RARE-EARTH PERMANENT MAGNETS VACODYM VACOMAX ADVANCED MATERIALS THE KEY TO PROGRESS
CONTENTS page 1. Introduction 4 2. Product Range 6 3. Applications 9 4. Materials and Magnetic Properties 14 4.1 Characteristic Properties 14 4.2 Material Grades 18 4.3 Temperature Dependence and Magnetic Losses 39 4.4 Magnetization of RE Magnets 4 5. Corrosion Behaviour, Surface Protection and Coatings 42 5.1 Corrosion Behaviour 42 5.2 Surface Protection 43 5.3 Types of Coating 44 5.4 Description of the Coatings 44 6. Forms of Supply 48 6.1 Types of Magnetization 48 6.2 Dimensional Tolerances 48 7. Glueing RE Magnets 51 8. Integrated Management System 51 8.1 Quality Management 51 8.2 Technial terms and Conditions of Sale 52 8.3 Environmental and Safety Management 53 9. Safety Guidelines 54 1. Appendix: 55 1.1 Technical Principles and Terms 55 1.2 Conversion Table Celsius Fahrenheit 57 11. Ductile Permanent Magnet alloys and Magnetically Semi-hard Materials 58 2
RARE-EARTH PERMANENT MAGNETS VACODYM VACOMAX VACUUMSCHMELZE GmbH & Co. KG (VAC) is one of the world s leading producers of special metallic materials with exceptional physical properties and resulting products. The company has a staff of approximately 3., is represented in 4 countries spread across all continents and currently achieves a turnover of more than 27 million. The headquarters, including operational headquarters of VAC is in Hanau, Germany. The company also has production plants in Slovakia and China. 3
1. INTRODUCTION In addition to permanent magnets, the product range includes soft magnetic materials, semi-finished products and parts, inductive components, magnetic shieldings and various other materials with special physical properties. Apart from the rare-earth permanent magnets, the spectrum includes, ductile permanent magnets and magnetically semi-hard materials. The latter are characterized by low-cost forming capabilities and adjustable permanent magnet properties. We have been working on the magnetic properties of special metallic materials and their applications for over 7 years. In 1973 we had already started producing permanent magnets on a rare-earth-cobalt base using powder metallurgical methods. By finding optimum solutions in close cooperation with our customers we have contributed strongly to the widespread use of this new material group available under the trade name VACOMAX. VACODYM * is our trade name for neodymium-iron-boron magnets. VACODYM has been produced on an industrial scale since 1986. Our materials have the highest energy density available to date. All processing steps from melting the alloy under vacuum through to coating the finished parts are performed at our works ensuring optimum material properties throughout the entire production process. As market leader in Europe today, we belong to the worldwide top-ranking producers of rare-earth permanent magnets. The magnetic properties are largely determined by the prematerial and the production process. Magnets can be produced in three different ways. These three methods are identified by the letters HR, TP, or AP in the alloy code. HR (high remanence) refers to the isostatically pressed magnets, as in the past. In the die pressed design we differentiate between TP (transverse pressed) and AP (axial pressed). Details on the available forms of supply are given in Section 6. Intensive development work has continually adapted our range of VACODYM alloys to the demands of the market. The focus being on the magnetic properties and especially on improving corrosion resistance, which was realized in the newly developed 8-Series consisting of VACODYM 837, = registered trademark of VACUUMSCHMELZE *) = licensor NEOMAX Co. Ltd. (Japan) 4
854, 863, 872 and 89. This new series of alloys and the 6-Series consisting of VACODYM 633, 655, 669, 677 and 688 already successfully launched on the market magnets particularly suitable for use in motor applications are available. These can be used under normal ambient conditions without any extra surface coating. For systems we developed a group of alloys for application temperatures up to 15 C the so-called 7-Series of VACODYM 722, 745, 764 and 776, which are characterized by particularly high remanence in-duction values. If the best possible corrosion resistance is an additional issue the high remanent qualities of VACODYM 837 and 854 from the 8-Series are a further option. Economic production processes, modern inspection techniques and a certified quality management system complying with DIN EN ISO 91, ISO TS 16949 and DIN EN ISO 141 are as much a matter of course as staff training sessions and an active environmental protection policy. By continuing to build on our long established foundations, we aim to remain your reliable and competent partner. Fig 1: Development of energy densities (BH) max of permanent magnets and their potential. 8 7 (BH) max [kj/m 3 ] Future possibilities of new materials 6 5 4 (BH) max = 485 kj / m 3 (Theoretical limits NdFeB) NdFeB 3 2 Sm 2 Co 17 1 Steel AlNiCo SmCo 5 Ferrite 188 19 192 194 196 198 2 22 24 26 Year 5
2. PRODUCT RANGE The product range of our rare-earth magnets covers a carefully balanced program of materials with different magnetic properties. As a result, it is relatively easy to select a material suitable for any specific application. VACODYM is the permanent magnet material offering the highest energy densities currently available. The excellent magnetic properties of this material group can be traced to the strongly magnetic matrix phase Nd 2 Fe 14 B featuring very high saturation polarization and high magnetic anisotropy. A ductile neodymium-rich bonding phase at the grain boundaries provides these magnets with good mechanical properties. Fig. 2 gives an overview of the typical properties of our VACODYM-magnets. VACOMAX is our permanent magnet material of rare-earths and cobalt. These magnets feature especially high coercivities with simultaneously high saturation and excellent temperature and corrosion stability. In Fig. 3 the typical demagnetization curves of VACODYM and VACOMAX are compared with the classical permanent magnet materials AlNiCo and hard ferrite. VACUUMSCHMELZE has many years of experience in the production of permanent magnets and the design of magnetic circuits. Alongside analytical processes, we utilize sophisticated computer programs to analyze and design magnet systems. These include 2D- and 3D-field calculations with finite element methods. Their use has substantially shortened the design phase of assemblies. As a result, besides single magnets, we are supplying an increasing number of finished magnet assemblies to customer s specifications. Detailed information on these is given in our PD-4 leaflet. Fig. 2: 1,5 Remanence B r and coercivity H cj of transverse field pressed VACODYM magnets 1,45 1,4 1,35 745 TP 764 TP 837 TP 854 TP VACODYM remanence, Br (T) 1,3 1,25 1,2 633 TP 776 TP 655 TP 863 TP 669 TP 872 TP 89 TP 1,15 677 TP 1,1 688 TP 1,5 1, 8 12 16 2 24 28 32 coercivity, H cj (ka/m) 6
Fig. 3: Typical demagnetization curves of VACODYM and VACOMAX in comparison with AlNiCo and Ferrite at room temperature The use of soft magnetic materials as system components, e.g. VACOFLUX and VACOFER, enables us to meet customers specifications at a high quality level. In many cases optimum assembly and magnetization of the systems is only possible when the magnets and the other system components are sourced and put together at the magnet producer. by strong magnetic fields parallel (axial field for AP-grades) or perpendicular (transverse fields for TP-grades) to the direction of pressing depending on the geometry of the part. Isostatically or transverse-field pressed parts have an approximately 5 8% higher remanence compared to axial-field pressed magnets. Magnets made of VACODYM and VACOMAX are produced powder metallurgically by sintering. The main processing steps are given in Fig. 4. Depending on size, shape, tolerances, batch size and magnetic requirements, the parts are either cut from isostatically pressed blocks or are diepressed. When diepressing, the powder particles are aligned 7
Melting of the Alloy under Vacuum Crushing Milling Alignment in Magnetic Field isostatic Pressing die pressed Transverse Field (TP) Axial Field (AP) Sintering, Annealing Machining, Coating Magnetizing Fig. 4: Production steps of rare-earth magnets 8
3. APPLICATIONS Compared to conventional magnet materials, such as AlNiCo or hard ferrite, magnets of VACODYM and VACOMAX display a number of excellent magnetic properties. Users benefit immensely from their merits: Energy densities up to tenfold those of AlNiCo and hard ferrite not only enable a reduction in magnet volume (see Fig. 5), but also the miniaturization of systems and whole subassemblies, saving the costs for return paths, coils etc. Existing magnet systems can be improved in many cases. In general, when using VACODYM or VACOMAX we recommend the previous systems to be re-designed. New design ideas can be utilized and new fields of applications are opened: MOTORS AND GENERATORS Servomotors, DC motors, linear motors and heavy-duty motors (e.g. motors for ships propulsion and wind turbine generator systems) utilize predominantly VACODYM magnets. In the case of high temperatures VACOMAX is the material of choice. A further important application is small power and fractional horsepower motors, e.g. bell type armature and dental motors. Assemblies for motors Rotor of a servomotor Fig. 5: Example illustrating the volume reduction achieved with VACODYM and VACOMAX: each magnet is designed to produce a field of 1 mt at the reference point P = 5 mm from the surface of the pole 9
AUTOMOTIVE ENGINEERING AND SENSORS Sensors to measure engine, gear and wheel rotary speed (e.g. ABS systems), accelerations (e.g. ESP, airbag) or positions (e.g. throttle valve, injection systems, camshaft, crankshaft, fuel gauges) are equipped with VACOMAX or VACODYM magnets, depending on the requirements for temperature and corrosion stability. Sensor for electronic vehicle stabilization program (ESP) Sensor (module in plastic housing with customer specific connectors) module cap: inner (with magnet) and outer view Producer: Robert Bosch GmbH VACODYM magnets, in particular, should be considered for actuators in engine management, small motors (e.g. steering boost), generators and for noise reduction. Synchronous motors as main drives in electro and hybrid vehicles are also equipped with VACODYM magnets. MRI (MAGNET RESONANCE IMAGING) In precise analysis equipment in medical engineering more and more permanent magnet systems with high remanent VACODYM grades are used besides superconducting and other electrically excited systems. The main advantages are the very low energy consumption, savings in weight and a maintenance-free construction. Synchronous coupling with VACODYM-magnets MAGNETIC COUPLINGS Magnetic couplings are preferred in automation and chemical processing technology as they ensure a permanent hermetic separation of different media. Owing to increased temperature requirements, VACOMAX magnets are used for numerous applications. VACODYM is recommended for lower application temperatures. Field line characteristic (Finite elements calculation) 1
A dipole with a diameter of 1.5 m is the heart of a particle detector named Alpha Magnetic Spectrometer (AMS). It is manufactured from approx. 5 rectangular magnets made of VACODYM 51 HR and operates successfully aboard the ISS space station since 1998. 11
BEAM GUIDING SYSTEMS, WIGGLERS AND UNDULATORS Permanent magnetic beam guiding systems require very little maintenance and no power supply. Systems using VACODYM or VACOMAX magnets have proved imperative in all applications where high field strengths have to be achieved in special reaction chambers, e.g. in sputtering devices, travelling wave tubes, wigglers, undulators and multi-pole devices as well as particle detectors. To meet these requirements, we produce defined and carefully balanced compatible sets of magnets exhibiting magnetic properties to tight tolerances, such as the angle between the preferred magnetic direction and the geometry of the parts. Economic manufacturing processes are available to produce parts with a large volume, in particular, we can produce large magnet cross sections with pole surfaces up to approx. 11 cm 2. 15 m long undulator system with magnets of VACODYM and polepieces of VACOFLUX for the TESLA Test Facility at DESY in Hamburg. 12
PERMANENT MAGNET BEARINGS Different magnetic bearing principles have been developed for turbo-molecular pumps, centrifuges etc. These employ ring magnets magnetized in either axial or radial direction. The material is selected according to customer s specifications. HOLDING SYSTEMS Clamping plates and vibration dampers for machine tools are one of the main fields of application for holding systems. These normally require maximum holding forces and call for VACODYM. We supply ready-to-use holding assemblies with pot-shaped iron return passes as well as single magnets. MEASURING INSTRUMENTS In this field the applications range from electronic scales through pulse meters to NMR-analysis equipment. Depending on the construction principle systems using armatures or rotors fitted with VACODYM or VACOMAX magnets are selected. SWITCHES AND RELAYS For the widely varying designs of Hall switches, polarized relays, revolution counters etc., magnets or magnet assemblies incorporating VACODYM or VACOMAX are used depending on the specification. Mass spectrometer from INFICON GmbH with magnet assembly made of VACOMAX 13
4. MATERIALS AND MAGNETIC PROPERTIES 4.1 CHARACTERISTIC PROPERTIES Table 1: CHARACTERISTIC PROPERTIES OF VACODYM AT ROOM TEMPERATURE (2 C) Pressing Material Code 1 ) Remanence Coercivity direction 1) Coding based on IEC 644-8-1, the magnetic values usually exceed the IEC values B r B r H cb H cb typ. min. typ. min. Tesla kg Tesla kg ka/m koe ka/m koe HR VACODYM 722 HR 38/87,5 1,47 14,7 1,42 14,2 915 11,5 835 1,5 VACODYM 745 HR 37/111,5 1,44 14,4 1,4 14, 1115 14, 165 13,4 VACODYM 51 HR 36/95,5 1,41 14,1 1,38 13,8 98 12,3 915 11,5 VACODYM 633 HR 315/127,5 1,35 13,5 1,29 12,9 14 13,1 98 12,3 VACODYM 655 HR 28/167 1,28 12,8 1,22 12,2 99 12,4 925 11,6 VACODYM 677 HR 24/223 1,18 11,8 1,12 11,2 915 11,5 85 1,7 TP VACODYM 745 TP 355/111,5 1,41 14,1 1,37 13,7 19 13,7 135 13, VACODYM 764 TP 335/127,5 1,37 13,7 1,33 13,3 16 13,3 15 12,6 VACODYM 776 TP 35/167 1,32 13,2 1,28 12,8 12 12,8 97 12,2 VACODYM 837 TP 335/127,5 1,37 13,7 1,33 13,3 16 13,3 11 12,7 VACODYM 854 TP 31/167 1,32 13,2 1,28 12,8 12 12,8 97 12,2 VACODYM 863 TP 295/2 1,29 12,9 1,25 12,5 995 12,5 95 11,9 VACODYM 872 TP 28/223 1,25 12,5 1,21 12,1 965 12,1 915 11,5 VACODYM 89 TP 25/263 1,19 11,9 1,15 11,5 915 11,5 865 1,9 VACODYM 633 TP 35/127,5 1,32 13,2 1,28 12,8 12 12,8 97 12,2 VACODYM 655 TP 28/167 1,26 12,6 1,22 12,2 97 12,2 925 11,6 VACODYM 669 TP 255/2 1,22 12,2 1,17 11,7 94 11,8 875 11, VACODYM 677 TP 24/223 1,18 11,8 1,13 11,3 915 11,5 86 1,8 VACODYM 688 TP 225/262,5 1,14 11,4 1,9 1,9 885 11,1 83 1,4 AP VACODYM 745 AP 325/111,5 1,34 13,4 1,31 13,1 125 12,9 97 12,2 VACODYM 764 AP 35/135,5 1,3 13, 1,27 12,7 995 12,5 955 12, VACODYM 776 AP 28/167 1,26 12,6 1,22 12,2 965 12,1 915 11,5 VACODYM 837 AP 3/135,5 1,3 13, 1,26 12,6 995 12,5 95 11,9 VACODYM 854 AP 275/167 1,26 12,6 1,21 12,1 965 12,1 95 11,4 VACODYM 863 AP 25/2 1,21 12,1 1,17 11,7 925 11,6 875 11, VACODYM 872 AP 235/223 1,17 11,7 1,13 11,3 89 11,2 845 1,6 VACODYM 89 AP 21/263 1,11 11,1 1,7 1,7 845 1,6 795 1, VACODYM 633 AP 28/135,5 1,26 12,6 1,22 12,2 965 12,1 915 11,5 VACODYM 655 AP 255/167 1,2 12, 1,16 11,6 915 11,5 865 1,9 VACODYM 669 AP 225/2 1,16 11,6 1,12 11,2 885 11,1 82 1,3 VACODYM 677 AP 215/223 1,13 11,3 1,8 1,8 86 1,8 85 1,1 VACODYM 688 AP 2/262,5 1,8 1,8 1,3 1,3 83 1,4 77 9,7 14
Energy density Temperature coefficient Density Max. 2-1 C 2-15 C continuous Temperature H cj (BH) max (BH) max TK (B r ) TK (H cj ) TK (B r ) TK(H cj ) T max 2) min. typ. min. typ. typ. typ. typ. typ. ka/m koe kj/m 3 MGOe kj/m 3 MGOe %/ C %/ C %/ C %/ C g/cm 3 C F 875 11 415 53 38 48,115,77 7,6 5 12 1115 14 4 5 37 47,115,73 7,6 7 16 955 12 385 48 36 45,115,79 7,5 6 14 1275 16 35 44 315 4,95,65,15,55 7,7 11 23 167 21 315 4 28 35,9,61,1,55 7,7 15 3 223 28 27 34 24 3,85,55,95,5 7,7 19 37 1115 14 385 48 355 45,115,73 7,6 7 16 1275 16 36 46 335 42,115,7,125,59 7,6 1 21 167 21 335 42 31 39,11,61,12,55 7,6 14 28 1275 16 36 46 335 42,11,62,12,54 7,6 11 23 167 21 335 42 31 39,15,6,115,53 7,7 15 3 2 25 315 4 295 37,1,56,11,51 7,7 17 34 223 28 3 38 28 35,95,53,15,49 7,7 19 37 2625 33 27 34 25 31,9,5,1,46 7,7 22 43 1275 16 335 42 35 39,95,65,15,57 7,7 11 23 167 21 35 39 28 35,9,61,1,55 7,7 15 3 2 25 29 36 255 32,85,57,95,51 7,7 17 34 223 28 27 34 24 3,85,55,95,5 7,7 19 37 2625 33 25 32 225 28,8,51,9,46 7,8 22 43 1115 14 34 43 325 41,115,73 7,6 8 18 1355 17 325 41 35 38,115,69,125,58 7,6 11 23 167 21 35 38 28 35,11,61,12,55 7,6 15 3 1355 17 325 41 3 37,11,62,12,54 7,6 12 25 167 21 35 38 275 35,15,6,115,53 7,7 16 32 2 25 28 35 25 32,1,56,11,51 7,7 18 36 223 28 26 33 235 3,95,53,15,49 7,7 2 39 2625 33 235 29 21 26,9,5,1,46 7,7 23 44 1355 17 35 38 28 35,95,64,15,57 7,7 12 25 167 21 275 35 255 32,9,61,1,55 7,7 16 32 2 25 255 32 225 28,85,57,95,51 7,7 18 36 223 28 24 3 215 27,85,55,95,5 7,7 2 39 2625 33 225 28 2 25,8,51,9,46 7,8 23 44 2) The maximum application temperature is governed by the layout of the system. The approx. values given refer to magnets operating in working points of B/μ o H = -1 (max. energy product). Users are recommended to consult VAC on any application of VACODYM involving temperatures above 15 C. 15
Table 2: CHARACTERISTIC PROPERTIES OF VACOMAX AT ROOM TEMPERATURE (2 C) Material Remanence Coercivity Code 1 ) B r B r H cb H cb H cj typ. min. typ. min. min. Tesla kg Tesla kg ka/m koe ka/m koe ka/m koe VACOMAX 24 HR 1,12 11,2 1,5 1,5 73 9,2 6 7,5 64 8, 2/64 VACOMAX 225 HR 1,1 11, 1,3 1,3 82 1,3 72 9, 159 2, 19/159 VACOMAX 225 TP 1,7 1,7 1,3 1,3 79 9,9 72 9, 159 2, 19/159 VACOMAX 225 AP 1,4 1,4,97 9,7 76 9,6 68 8,5 159 2, 17/159 VACOMAX 2 HR 1,1 1,1,98 9,8 755 9,5 71 8,9 995 12,5 18/1 VACOMAX 17,95 9,5,9 9, 72 9, 66 8,3 1195 15, 16/12 VACOMAX 145 S,9 9,,85 8,5 66 8,3 6 7,5 199 25, 14/2 1 ) Coding based on IEC 644-8-1, the magnetic values usually exceed the IEC values Table 3: CHARACTERISTIC PROPERTIES OF VACODYM AND VACOMAX AT ROOM TEMPERATURE (2 C) Material Curie- Specific Specific Thermal Coefficient of thermal Young s Bending Compressive Vickers- Stress temp. electr. heat con- expansion modulus strength strength hardness crack resistance ductivity 2-1 C resistance II c c K IC C mm 2 /m J/(kg K) W/(m K) 1-6 /K 1-6 /K kn/mm 2 N/mm 2 N/mm 2 HV N/mm 3/2 VACODYM 31 37 1,1 1,7 35 55 5 15 4 9-2 14 17 12 4 6 125 5 7 8 18 VACOMAX Sm 2 Co 17 8 85,65,95 3 5 5 15 8 12 1 14 14 17 8 15 4 9 55 75 3 6 VACOMAX SmCo 5 7 75,4,7 3 5 5 15 4 1 1 16 1 13 9 18 6 11 5 7 4 8 16
Energy density Temperature coefficient Density Max. 2-1 C 2-15 C continuous temperature (BH) max (BH) max TK (B r ) TK(H cj ) TK (B r ) TK(H cj ) T 2 ) max typ. min. typ. typ. typ. typ. typ. kj/m 3 MGOe kj/m 3 MGOe %/ C %/ C %/ C %/ C g/cm 3 C F 24 3 2 25,3,15,35,16 8,4 3 57 225 28 19 24,3,18,35,19 8,4 35 66 215 27 19 24,3,18,35,19 8,4 35 66 2 25 17 21,3,18,35,19 8,4 35 66 2 25 18 23,4,21,45,22 8,4 25 48 18 23 16 2,4,21,45,22 8,4 25 48 16 2 14 18,4,14,45,15 8,4 25 48 2 ) Prior to using VACOMAX above 2 C we recommend customers contact VAC. Table 4: Material INNER MAGNETIZING FIELD STRENGTH OF VACODYM AND VACOMAX ka/m H mag min. koe VACODYM 25 31 VACOMAX 225 365 46 VACOMAX 24 2 25 VACOMAX 145/17/2 2 25 17
4.2 MATERIAL GRADES VACODYM and VACOMAX are anisotropic materials with a reversible permeability µ rev < 1.1 at the working point. The exact value depends on the material grade and the magnet geometry. VACODYM and VACOMAX do not feature open porosity, i.e. the pores are not connected to one another. Therefore both materials can be utilized for vacuum applications. The following pages show demagnetization curves of different grades at various temperatures. Additionally, the typical irreversible losses are given as a function of temperature at different loadlines. These charts are based on HR- or TP-grades. Axial field pressed magnets have slightly reduced losses under comparable conditions. The measured curves refer to magnets whose minimum dimensions are >1 mm perpendicular to the direction of magnetization and > 5 mm parallel to it. Smaller dimensions may deviate from the curves shown. 18
4.2.1 SINTERED MAGNETS ON A Nd-Fe-B BASE VACODYM 722 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 722 HR -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 -,5 2 C 6 C 8 C 1 C 12 C 1,2 1,,8,6 12 1 8 6 J,B,4 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 19
VACODYM 745 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 745 HR -,5-1, -1,5-2, -4, 2 C 6 C 8 C 1 C T 1,6 1,4 1,2 1,,8 kg 16 14 12 1 8 J,B 12 C,6,4 6 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 745 AP -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 -,5 2 C 6 C 8 C 1 C 1,2 1,,8 12 1 8 J,B 12 C,6,4,2, -,2 -,4 -,6 6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 2
VACODYM 764 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 764 TP -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 1,2 12 J,B -,5 2 C 6 C 8 C 1 C 12 C 1,,8 1 8 15 C,6,4 6 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 764 AP -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 2 C 6 C 8 C 1 C 12 C 1,,8 1 8 15 C,6,4,2, -,2 -,4 -,6 6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 21
VACODYM 776 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 776 TP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6 18 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 776 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6 18 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 C 2 VACODYM 776 TP -5 B/μ H = -,5-1 -2-1 22
VACODYM 51 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 51 HR -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 -,5 2 C 6 C 8 C 1 C 1,2 1,,8 12 1 8 J,B,6 6 12 C,4,2 4 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 23
VACODYM 633 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 633 HR -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 1,2 12 J,B -,5 2 C 6 C 8 C 1 C 12 C 1,,8 1 8 15 C,6,4 6 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 633 AP -1, -1,5-2, -4, -,5 2 C 6 C 8 C 1 C 12 15 C T 1,6 1,4 1,2 1,,8,6,4,2, -,2 -,4 -,6 kg 16 14 12 1 8 6 4 2-2 -4-6 J,B -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 24
VACODYM 655 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 655 HR 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6 18 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 655 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6 18 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 25
VACODYM 669 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 669 TP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 8 C 1 C 12 C 15 C 18 C 1,,8 1 8 21 C,6,4,2, -,2 -,4 -,6 6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 669 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 8 C 1 C 12 C 15 C 18 C 21 C 1,,8,6,4 1 8 6 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 26
VACODYM 677 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 677 HR 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 1 C 12 C 15 C 18 C 1,,8,6 1 8 6 21 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 677 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 1 C 12 C 15 C 18 C 1,,8,6 1 8 6,4 4 21 C,2, -,2 -,4 -,6 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 27
VACODYM 688 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 688 TP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 12 C 15 C 18 C 21 C 1,,8,6 1 8 6 24 C,4,2, -,2 -,4 -,6 4 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 688 AP -,5 2 C -1, -1,5-2, -4, 12 C 15 C 18 C 21 C 24 C T 1,6 1,4 1,2 1,,8,6,4,2, -,2 -,4 -,6 kg 16 14 12 1 8 6 4 2-2 -4-6 J,B -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature 28
VACODYM 837 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 837 TP -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 1,2 12 J,B -,5 2 C 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6,4 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 837 AP -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 2 C 6 C 8 C 1 C 12 C 15 C 1,,8 1 8,6 6,4 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 2 C 25 VACODYM 837 TP -5 B/µ H = -,5-1 -2-1 29
VACODYM 854 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 854 TP -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 2 C 1,2 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 18 C 1,,8 1 8,6 6,4 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 854 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 6 C 8 C 1 C 12 C 15 C 18 C 1,,8 1 8,6 6,4 4,2 2, -,2-2 -,4-4 -,6-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 2 C 25 VACODYM 854 TP -5 B/µ H = -,5-1 -2-1 3
VACODYM 863 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 863 TP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 8 C 1 C 12 15 C 18 C 1,,8 1 8 21 C,6,4,2, -,2 -,4 -,6 6 4 2-2 -4-6 -2 koe - 18-16 -14-12 -1-8 -6-4 -2 -,8-8 ka/m -14-12 -1 H -8-6 -4-2 B/ μ o H VACODYM 863 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 8 C 1 C 12 C 15 C 18 C 1,,8 1 8 21 C,6,4,2, -,2 -,4 -,6 6 4 2-2 -4-6 -2 koe - 18-16 -14-12 -1-8 -6-4 -2 -,8-8 ka/m -14-12 -1 H -8-6 -4-2 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 2 C 25 VACODYM 863 TP -5 B/ H = -,5-1 -2-1 31
VACODYM 872 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 872 TP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 1 C 12 15 C 18 C 1,,8,6 1 8 6,4 4 21 C,2, -,2 -,4 -,6 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 B/ μ o H VACODYM 872 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 kg 16 14 12 J,B -,5 1 C 12 15 C 18 C 1,,8,6 1 8 6,4 4 21 C,2, -,2 -,4 -,6 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2 ka/m -14-12 -1-8 -6-4 -2 H -8 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 2 C 25 VACODYM 872 TP -5 B/ H = -,5-1 -2-1 32
VACODYM 89 Typical demagnetization curves B(H) and J(H) at different temperatures B/ μ o H VACODYM 89 TP -1, -1,5-2, -4, T 1,6 1,4 kg 16 14 2 C 1,2 12 J,B -,5 12 15 C 18 C 21 C 1,,8 1 8,6 6,4 4 24 C,2, -,2 -,4 -,6 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2-8 ka/m -14-12 -1 H -8-6 -4-2 B/ μ o H VACODYM 89 AP 2 C -1, -1,5-2, -4, T 1,6 1,4 1,2 1,,8 kg 16 14 12 1 8 J,B 12 15 C 18 C 21 C,6 6,4 4 24 C,2, -,2 -,4 -,6 2-2 -4-6 -,8-2 koe - 18-16 -14-12 -1-8 -6-4 -2-8 ka/m -14-12 -1 H -8-6 -4-2 Typical irreversible losses at different working points as a function of temperature irreversible losses (%) Temperature 5 1 15 2 C 25 VACODYM 89 TP -5 B/ H = -,5-1 -2-1 33
4.2.2 SINTERED MAGNETS ON A Sm 2 Co 17 BASE VACOMAX 24 Typical demagnetization curves B(H) and J(H) at different temperatures Typical irreversible losses at different working points as a function of temperature 34
VACOMAX 225 Typical demagnetization curves B(H) and J(H) at different temperatures AP Typical irreversible losses at different working points as a function of temperature 35
4.2.3 SINTERED MAGNETS ON A SmCo 5 BASE VACOMAX 2 Typical demagnetization curves B(H) and J(H) at different temperatures HR Typical irreversible losses at different working points as a function of temperature 36
VACOMAX 17 Typical demagnetization curves B(H) and J(H) at different temperatures Typical irreversible losses at different working points as a function of temperature 37
VACOMAX 145 Typical demagnetization curves B(H) and J(H) at different temperatures Typical irreversible losses at different working points as a function of temperature 38
4.3 TEMPERATURE DEPENDENCE AND MAGNETIC LOSSES The magnetic properties of permanent magnets are governed by the application temperature. The typical demagnetization curves of VACODYM and VACOMAX at different temperatures are shown on the relevant alloy pages (see pages 19-38). When selecting a material and the dimensions of a magnet, the characteristic magnetic values and the temperature dependence must be considered (see section 1.1 of appendix Technical Principles and Terms ). The temperature dependence of the demagnetization curves causes changes in the flux density, commonly referred to as magnetic losses. These losses fall into two main categories: Reversible losses and irreversible losses. The latter result from demagnetization of small areas of the magnet in opposing fields and/or a rise in temperature, as well as changes in the micro-structure. Reversible changes in the flux density are attributed to the temperature dependence of the saturation polarization and are solely a function of alloy composition. They are described by the temperature coefficient of the remanence; the mean value for each material is given in Table 1 and 2, resp. If an application calls for temperature compensation, we recommend the use of a magnetic shunt made of THERMOFLUX. This achieves temperature coefficients l TC l <.1%/K in systems with slightly reduced flux values in the range from 2 to 1 C. Irreversible losses owing to demagnetization processes are dependent on the load line of the magnet and the maximum application temperature. The typical irreversible losses to be expected for the various material types at different load lines B/µ o H are given in the applicable data sheets. Irreversible changes can largely be avoided by means of a stabilization process (aging). To obtain the optimum stabilization conditions for each application users should contact VAC. As a rule, it is adequate to heat the magnets to slightly above the maximum application temperature for approximately one hour. This pre-treatment achieves good stabilization but at the expense of the flux density which is reduced accordingly by the irreversible changes. The losses caused by magnetization reversal in small areas of the magnet can be eliminated by remagnetization. The maximum continuous application temperatures are primarily restricted by the reduction in the magnetic properties (see Tables 1 and 2). To avoid undesired irreversible changes in the microstructure which cannot be remedied by remagnetization, VACODYM magnets must not be heated to above 35 C and VACOMAX magnets not above 4 C. Chemical reactions with the immediate atmosphere or contact materials (e.g. glues) must be prevented. This applies especially to reactions with potential hydrogen production (see section 5.1). Radioactive radiation for a longer time can cause irreversible magnetic losses. VACOMAX can be used at temperatures down to that of liquid helium. When using VACODYM below approx. 15 K our technical staff should be consulted. 39
4.4 MAGNETIZATION Full magnetization is the precondition for achieving the typical magnetic values that are listed in Table 1 resp. 2 for the various materials. The required minimum field strengths of the inner magnetizing field H mag are obtained from the magnetization behaviour of the material in question. They are shown in Table 4, page 17, and in Fig. 6. To achieve the internal magnetizing field H mag, the given external field H ext must be increased by the value of the demagnetizing field H a which is determined by the working point: l H ext l = l H mag l + l H a l (See Section 1.1 of appendix Technical Principles and Terms.) Due to the high coercivities of VACODYM and VACOMAX the magnets can also be magnetized outside the system. As a result, handling the magnets and assembly of systems is more difficult but the actual magnetization is far easier. With VACODYM 51, 722/745 and also VACOMAX 24, care must be taken to ensure that the working point of the magnet is sufficiently above the knee of the B(H) -demagnetization curve (see section 1.1 of appendix Technical Principles and Terms ). Prior to magnetizing VACODYM and VACOMAX in a system we advise users to contact VAC. Magnets made of VACODYM and especially of VACOMAX can only be completely reversed in exceptionally high magnetic fields (> approx. 12 koe). Fig. 6: Demagnetization curves of VACODYM and VACOMAX as a function of magnetization field strenght H mag. The magnetization behaviour of VACODYM and VACOMAX of the SmCo 5 type (Figs. a and b) is based on the so-called nucleation mechanism. This easy magnetization is only possible from the thermally demagnetized state. The pinning mechanism is characteristic for the VACOMAX type Sm 2 Co 17 (Figs. c and d). VACOMAX 24 is very easy to magnetize compared with VACOMAX 225. This is achieved by a special heat treatment. a) Magnetizing field strength (ka/m) 4
Magnetizing field strength (ka/m) Magnetizing field strength (ka/m) Magnetizing field strength (ka/m) 41
5. CORROSION BEHAVIOUR, SURFACE PROTECTION AND COATINGS 5.1 CORROSION BEHAVIOUR Due to their strongly negative electrochemical standard potential (E = 2.2 to 2.5 V) rare-earth (RE) elements belong to the group of non-precious and thus highly reactive elements. Their chemical reactivity is similar to that of alkaline earth metals, like magnesium. Under normal conditions, the RE metals react slowly. Under conditions at higher temperatures and the presence of water or humidity, the reaction is more rapid, RE-hydroxide is formed and hydrogen is set free. The released hydrogen can then react with the free RE metal forming RE metal hydrides. By adding an adequate amount of more noble elements such as, for example, cobalt, the reaction with water can be almost suppressed. The reaction rate is negligible. This is the back-ground to VACOMAX (SmCo 5 or Sm 2 Co 17 ) only exhibiting a slight surface discolouration when exposed to high humidity (e.g. >8 % relative humidity) and increased temperature (e.g. >8 C). No significant amount of corrosion products was measured even after long exposure (e.g. >1 h). 95 % humidity and 2.6 bar). This in turn leads to a high corrosion rate and debris, which is neodymium hydroxide, and also to magnet dust (loose Nd-Fe-B grains). Sections 5.2 to 5.4 describe means of protecting these materials effectively in corrosive operating conditions. The second generation of VACODYM materials such as for example the 6-series and 8-series alloys no longer feature this corrosion mechanism. Additions of carefully selected suitable materials (including cobalt) to the neodymium-rich phase have improved their corrosion behaviour and systematically stopped intergranular corrosion in a warm, humid atmosphere. The corrosion behaviour of such VACODYM alloys is similar to that of pure iron materials (steel). In the HAST test even after several weeks exposure the corrosion rate can hardly be measured. There is merely a dark grey shimmer to the material surface. In cases where the humidity turns to condensation, VACO- DYM materials gradually begin to rust, similarly to parts made of iron (red rust). Here the corrosion products are mainly non-magnetic metal oxides or hydroxide. In applications where dew formation occurs regularly (condensation), and/or the parts are to be used in water or other corrosive media, we recommend coating. The situation is in general different with Nd-Fe-B magnets. The individual magnet grains are held together mechanically and fixed to each other by the so-called neodymium-rich phase. This phase represents up to 5 % of the total volume of the material and from a chemical point of view behaves like pure neodymium. As a result, a relatively rapid intergranular decomposition of the magnet (see Fig. 7) sets in under high humidity and temperature (e.g., in the so-called HAST Highly Accelerated Stress Test acc. IEC 68-2-66 at 13 C / 42
8XX 6XX Weight loss VACODYM 7XX Exposure time (days) Fig. 7: Weight loss of VACODYM magnets in a HAST-Test similar to IEC 68-2-66 (13 C; 95 % relative humidity; 2.6 bar in vapour) 5.2 SURFACE PROTECTION Permanent magnets made of VACODYM and VACOMAX can be used in normal ambient conditions (such as room temperature, humidity up to 5 %, no condensation) without special additional surface protection. However, the magnet surface has to be coated for many applications. There are three main reasons for this: CORROSION PROTECTION RE-permanent magnets are frequently exposed to chemically aggressive media such as acids, alkaline solutions, salts, cooling lubricants or harmful gases and have to be protected. In the case of VACODYM high humidity, dew formation or sweat is already sufficient to cause corrosion. We therefore recommend to handle VACODYM-magnets with suited gloves on principle. PROTECTION AGAINST MAGNETIC PARTICLES VACODYM and VACOMAX are sintered materials, thus it cannot be excluded that magnetic particles are found on the surface. In certain applications (e.g. systems with small working air gaps) loose magnetic particles may affect the function and/or destroy the magnet assembly. Coating ensures that the magnets can be cleaned thoroughly and will be free of all deposits. HANDLING PROTECTION Magnets are frequently mechanically stressed during assembly or operation in an assembly. In some circumstances, this may lead to chipping, sharp edges are a particular risk. Each application of VACODYM and VACOMAX must be chekked as to whether coating is necessary and how the surface is to be protected. We have tested the behaviour of our permanent magnets under widely varying conditions and will be pleased to advise you on the appropriate coating for your application. 43
5.3 TYPES OF COATINGS The coatings can be divided into two basic groups: metallic and organic. To meet special requirements and on request, double coatings of metal/metal & metal/varnish and a number of special coatings are available. METALLIC COATINGS As a rule, galvanic processes are used for metallic coating. Apart from our standard nickel or tin coating, on request we offer double coating nickel + tin. In addition IVD (Ion Vapour Deposition)-Aluminium coating is also possible. When selecting the type of metallic coating, the possibility of galvanic element formation in the assembly must be taken into account, as long as dew formation cannot be excluded. ORGANIC COATINGS For this case we offer different spray coatings with excellent corrosion protection characteristics. Cost-effective alternatives to metallic coatings are especially aluminium spray coatings as well as the newly developed VACCOAT epoxy resin coating. 5.4 DESCRIPTION OF THE COATINGS The majority of all applications are covered by our coatings galvanic tin, galvanic nickel, electro-painting and IVD aluminium coating as well as the recently introduced VACCOAT spray coatings introduced. The properties of the coatings complement one another. All galvanic coating processes and the spray coatings are applied at VACUUMSCHMELZE. The described properties can only be achieved in a carefully controlled system which takes into consideration the microstructure of the magnets, the mechanical processing/machining, cleaning and coating. IVD aluminium coating is performed by a subcontractor selected and qualified by VAC with great care. Appropriate quality assurance measures ensure continuity of quality in series production. Using the latest automating technology, all other coatings are applied by VAC in-house cost-effectively and with high reproducibility as well as quality. GALVANIC TIN Galvanic tin coating provides good corrosion protection against atmospheric influences, humidity as well as weak acids and alkaline solutions. The tin coating applied at VAC is dense and free of interconnected pores. The typical coating thickness range for magnets is 15 3 µm. The finish of tin coating is silvery-white and slightly glossy. No phase transitions occur between 4 C and the melting point of 232 C. The deposition process is optimized by VAC for RE magnets especially to preclude hydrogen damage to the surface of the magnet during coating positively. Small parts can be coated economically in a barrel. Larger parts are galvanized in a rack. The decision on which method to use is governed by the weight of the part and/or the geometry (typical nominal values: <25 g barrel; >25 g rack). The special merits of tin coatings are their high resistance to environmental influences (e.g. 85 C/85 % relative humidity) as generally specified for electronic applications. Tin is highly ductile and is almost free of internal stresses over a wide coating thickness range, moreover the process is highly reliable. There is no risk of cracking or flaking. Mechanical stress does not lead to chipping but merely to deformation of the tin coating so that the magnetic material is still protected safely. After thorough cleaning the tin coating is free of all residues and thus provides an ideal surface for many adhesives. 44
GALVANIC NICKEL Galvanic nickel coatings can be used as an alternative to tin or as double coating in combination with tin. On VACODYM, its protection is superior to a comparable coating thickness of tin. The minimum coating thickness that we recommend for protection against corrosion is 1 µm for nickel coating in comparison with 15 µm for tin coating. Galvanic nickel coatings are hard, abrasion-proof and can be cleaned without difficulty and without residues. Therefore these coatings have prevailed today, especially for clean room applications. VAC has a special nickel coating process which supplies optically attractive semibright coatings. Compared with customary bright nickel methods, such as are frequently used for rare earth magnets, our process has the following advantages: a) The coatings have high ductility and therefore show a clearly lower tendency to mechanical damage in the edge area on impact of shock. This leads to more reliable production both in the plating process and during assembly. Even parts of 5 g in weight can still be coated by barrel plating with suitable geometry. Coating in a rack is possible for heavier parts. b) When glued, clearly better adhesive strengths are achieved than with bright nickel coating because of the increased surface roughness. c) The process exhibits a very homogenous coating thickness distribution over a wide current density range, so that the so-called dog-bone-effect (excessive coating build-up in the edge/corner area) is minimized. Dimensional tolerances for thin flat parts of ±5 µm (including machining) can thus be achieved reliably in production (comparable with galvanic tin coating). d) The risk of stress cracks under thermal loading is low. The reasons for this are the better ductility as well as the extremely low internal stresses of the coating. All these properties make galvanic nickel a universal coating for RE permanent magnets covering many applications. DOUBLE COATING NICKEL + TIN Especially high corrosion resistance is attained when tin coating is applied on top of a layer of nickel. The lifetime of this double coating under environmental test conditions (e.g. 85/85 test) is twice that of nickel or tin coatings of the same thickness. The surface properties are equivalent to those of tin coating. IVD ALUMINIUM IVD (= ion vapour deposition) aluminum ensures excellent corrosion protection both in a humid climate and in exposure to salt spray. The cathodic protection by the aluminum coating enables, for example, continuous use in water. Further, owing to the electrochemical protection provided by the aluminium small imperfactions in the coating do not affect the corrosion resistance in any perceivable way. Since aluminum can be used in principle up to approx. 5 C, all applications of RE permanent magnets are thus covered. The corrosion resistance of this coating is improved further by subsequent surface passivation. Because of the high ductility of the coating, mechanical loads only cause deformation of the coating similar to that with tin, without the protective effect being impaired by damage to the coating. In comparison to electroplated zinc layers, which are also used as cathodic protection for Nd-Fe-B, the IVD-aluminium has the following advantages: extremely high temperature resistance no hydrogen embrittlement during coating process no formation of loose white rust in corrosive atmosphere very good HAST resistance. Small parts (up to 25 g) are coated in a cost effective barrel process. Heavy parts are handled as rack goods. Processincluded contact marks are prevented by special handling. 45
ALUMINIUM SPRAY COATING VACCOAT The stove-enamel finish filled with aluminium flakes shows similar resistance to climatic or salt spray tests like IVD aluminium. Even magnets with a coating thickness of only 5 µm withstand longterm autoclave and salt spray tests. Compared to other spray coatings our new coating provides a superior edge protection. The coating is suitable for applications up to utilization temperatures of up to 18 C in continuous application. Due to the excellent hardness of this stove enamel finish (typical 6-8 H pencil hardness) Al-spray coating is not sensitive to mechanical damage. For parts > 1 g the coating is applied in an automatic spray coating machine which ensures high reproducibility and process safety as well compliance with strict dimensional tolerances. An automatically controlled and very cost-effective barrel-plating process is available for small parts. cured it can be a high-strength adhesive. A high-strength adhesive bond forms during stoving giving a shear strength of typically >15 N/mm 2. At the same time the system is protected effectively from corrosion by the coating. The attained corrosion protection is comparable to aluminium spray coating. The stoved coating has a pencil hardness of at least 4H and can be thermally stressed to approx. 2 C. Optically high-quality finish layers of between 5 µm and 4 µm can be applied in one operation. The coating colour is selectable (the standard colour is black). The coating is abrasion-resistant and exhibits very good electrical insulation behaviour. Similarly to aluminium spray coating the layers can be applied to the magnets either in a continuous automatic process or in a barrel-plating process. The Aluminium spray coating is also of great benefit in the coating of complete magnet systems. As a rule, any residual adhesive can be permanently covered by our spray coating. In contrast to IVD aluminium coating this coating is not electrically conductive. EPOXY SPRAY COATING VACCOAT This coating recently developed in-house sets new standards regarding corrosion protection, temperature resistance, coating application and the subsequent processing of coated magnets into systems. When cured VACCOAT 211 provides high-grade corrosion protection on VACODYM. At the same time when the coating film is not yet Micrograph of coverage with VACCOAT 147 at the edge of a magnet 46
TEMPORARY CORROSION PROTECTION/ SURFACE PASSIVATION To protect uncoated magnets temporarily, e.g. during transport or storage, we have developed a passivation method. This protects our RE-magnets, including the more corrosion sensitive VACODYM, sufficiently against temporary environmental influences such as a rise in humidity. With this standard procedure our magnets can be stored under normal ambient conditions providing condensation can be excluded. PROPERTY PROFILE OF DIFFERENT COATINGS Table 5 compares the properties of the most important coatings and should be used as a guideline when selecting surface protection for an application. It gives the minimum layer thickness of the various coatings and ensures adequate corrosion protection in the majority of applications. To meet more stringent requirements on corrosion protection, the layer thickness must be adjusted accordingly. Please note that improper handling may well harm the coating. Table 5: SURFACE COATINGS Surface Method Min. layer Colour Hardness Resistance Temperature Typical thickness for to range application corrosion examples protection tin (Sn) galvanic > 15 µm silver HV 1 1 ) humid atmosphere, < 16 C electric motors, bright solvents sensor technology mechanical engineering nickel (Ni) galvanic > 1 µm silver HV 35 1 ) humid atmosphere, < 2 C clean-rooms, semibright solvents, small-sized motors, cooling lubricants linear motors, UHV undulators Ni +Sn galvanisch Ni > 5 µm silver HV 1 1 ) humid atmosphere, < 16 C hot water meters, Sn > 1 µm bright solvents, use in fuel (biodiesel) cooling lubricants, salt spray test Aluminium IVD > 5 µm silver semibright HV 2 1 ) humid atmosphere, < 5 C electric motors, passivated (chromium VI salt spray test, sensor technology, free), yellow solvents aeronautic semibright applications (yellow chromated) aluminium automatic > 5 µm yellow > 4H 2 ) humid atmosphere, < 18 C electric motors, spray coating spray coating semibright spray test, generators, VACCOAT toxic gas test, sensor technology, 147 solvents linear motors, motorcars epoxy automatic > 1 µm black 3 ) 4H 2 ) humid atmosphere, < 2 C segmented magnet spray coating spray coating salt spray test, systems, electric motors, VACCOAT toxic gas test, linear motors, 211 solvents motorcars 1) Vickers hardness (nominal values) 2) Pencil hardness 3) other colours possible 47
6. FORMS OF SUPPLY 6.1 TYPES OF MAGNETIZATION Magnets made of VACODYM and VACOMAX can be supplied in the magnetized or non-magnetized state. Normally the poles are not marked. Owing to the magnetic anisotropy of VACODYM and VACO- MAX the parts are magnetized along certain preferred directions relative to the geometry of the part. The most common pole configurations are shown on the right. Our experts with in-depth know-how will be pleased to answer any questions on magnetization techniques. For the delivery of magnetized parts we have developed various packaging methods which can if necessary and in compliance with the rigorous IATA regulations be modified to meet individual customers requirements for airfreight. 6.2 DIMENSIONAL TOLERANCES The pole surfaces of die-pressed sintered magnets made of VACODYM or VACOMAX usually have to be ground. The tolerance after grinding is normally ±.5 mm; values of ±.2 mm are possible. The dimensions perpendicular to the direction of pressing are largely determined by the dies and do not normally require machining (netshape). Typical tolerances for the sides of die pressed parts are: Nominal dimensions perpendicular Tolerance (mm)* to the direction of pressing (mm) up to 7 ±,1...±,2 7 15 ±,15...±,3 15 25 ±,25...±,4 25 4 ±,3...±,6 4 6 ±,45...±,9 6 1 ±,8...±1,5 1 15 ±1,5...±2,5 * precise data on request Should these surfaces require machining the general tolerances to DIN EN 2768 mk can usually be met. For shaped parts with more complex geometry we usually give a maximum and a minimum envelope curve; the contour of the die-pressed part is within this curve. The length tolerances for parts cut from blocks (TP resp. HR quality) are ±.1 mm. On request even tighter tolerances can be met by grinding. If no tolerances are specified, we supply according to DIN ISO 2768 mk. Pole arrangements top view side view for rods: and rings: axial for rings: radial for rings: diametral for segments: diametral NETSHAPE PARTS By leaving out the grinding process, particularly competitvely priced magnets with a pole surface of up to approx. 6 cm 2 can be die-pressed. Perpendicular to the direction of pressing, these netshape magnets exhibit the tolerances as stated. In the direction of pressing due to special die-pressing and sintering methods, thickness tolerances of typically ±.2 mm are met at individually measured points without subsequent grinding. Preferred shapes are cuboids and segments with typical thicknesses in the range of 2.2 to 8. mm. Our experts will gladly assist in the layout of the magnet geometry and the tolerance of netshape magnets. 48
DIMENSIONS OF DIE-PRESSED VACODYM AP-MAGNETS (AXIAL-FIELD PRESSED) CRITERIA FOR ECONOMIC MAGNET GEOMETRIES Shape Type Sketch Dimensions Dimensions Remarks economic possible economic Ring AP D 12 mm D 18 mm only d 3 mm 1 mm T 7 mm thickness T ground (D-d)/2 = w 3 mm A <15 mm 2 d/d,6 D/1 T D/2 A <95 mm 2 Disk AP D 1 mm D 14 mm only D/1 T D/2 1 mm T 7 mm thickness T ground Cuboid AP L 12 mm L 15 mm only LxW 95 mm 2 LxW 15 mm 2 thickness T ground T 55 mm 1 mm T 7 mm T,15 (LxW) L/W 5 Re,1 (LxW) Loaf AP L 12 mm L 15 mm thickness W 5 mm 2 mm H 55 mm T and width W ground T,6 H 2 mm H 2 mm,5 L/W 5 Re,1 (LxW) Arc- AP L 12 mm L 15 mm thickness Segment W 5 mm 1,5 mm T 5 mm T and width W ground 2 mm T 2 mm ß 15 ß 8 W 7 mm,5 L/W 3 Re,1 (LxW) Shaped AP W 45 mm H, W 15 mm only Part H 35 mm A 15 mm 2 thickness T ground A 15 mm 2 1 mm T 7 mm W/H 3 1,5 mm T 3 mm T,1 A Re,1 A 49
DIMENSIONS OF DIE-PRESSED VACODYM TP-MAGNETS (TRANSVERSE FIELD PRESSED) CRITERIA FOR ECONOMIC MAGNET GEOMETRIES Shape Type Sketch Dimensions Dimensions Remarks economic possible economic Cuboid TP W 7 mm W 11 mm Thickness T (HR) 2 mm T 1 mm 1 mm T 14 mm cut or ground 1 mm H 55 mm TxW 13 mm 2 W/H 2,5 H 8 mm Re,1 (TxW) Ring TP 8 mm D 7 mm 6 mm D 12 mm only outer diameter D ground (diametral) d 3 mm d 1 mm (D-d)/2 = w 2 mm w 1,5 mm,1 d/d,65,1 d/d,8 3 mm H 55 mm 2 mm H 8 mm H 5w H 8w Disk TP 8 mm D 7 mm 5 mm D 12 mm only outer diameter D ground (diametral) 5 mm H 55 mm 2 mm H 8 mm H D/4 DIMENSIONS OF ISOSTATICALLY-PRESSED VACODYM HR-MAGNETS (UNTREATED, UNPROCESSED) CRITERIA FOR ECONOMIC MAGNET GEOMETRIES Shape Type Sketch Dimensions Dimensions Remarks economic possible economic Cuboid HR W 11 mm W 11 mm unprocessed with a T 25 mm T 8 mm 6 mm contour tolerance, A 7 mm 2 A 7 mm 2 R e approx. 5 mm Disk, HR D 7 mm D 9 mm unprocessed with a rod L 25 mm L 8 mm 6 mm contour tolerance Analogue shapes and dimensions also available in VACOMAX with moderate restrictions (appropriate to the magnet quality). 5
7. GLUEING RE MAGNETS The majority of RE magnets produced by VAC are assembled into magnet systems using adhesives. When selecting an adhesive the following should be considered: static and dynamic load thermal load (time-span/frequency/temperature range) thermal expansion of both partners size of glueing area corrosive load (resistance of adhesive to atmosphere and chemicals) quality of glueing surfaces (coating, roughness etc.) material matching regarding electrochemical potentials (corrosion due to voltaic cell formation) thickness of glueing gap In the following we offer some advice on adhesives and accumulated bonding methods for magnets based on the experience at VAC over the years: a) Adhesives with acid content must not be used with RE magnets, particularly not with VACODYM. Acidic products in connection with humidity lead to rapid decomposition of the magnet material at the interface adhesive/magnet and will damage the bond. Such adhesive must even be avoided when magnets are coated and especially if varnished. b) When bonding large surfaces with iron or other substrates the coefficients of thermal expansion of the RE magnet materials must be taken into account. In particular, in connection with VACODYM, which has a negative coefficient of thermal expansion (-1 x 1-6 /K) perpendicular to the direction of magnetization, and thus, as a rule, parallel to the bonding surface, stresses build up due to strains resulting from fluctuations in temperature which the bond must absorb. Our team of magnet experts will be pleased to advise you on this matter. c) When preparing the RE magnets for bonding, sand blasting should be avoided. This processing step might lead to a loosening of the microstructure on the surface of the sintered magnets. Our permanent magnets are supplied in the state ready for bonding. The passivation applied after cleaning provides a suitable base for most adhesives. However, if a pre-treatment step directly prior to bonding is considered important then we recommend users subsequently clean the bonding surface with a solvent, such as acetone or benzine. d) An adhesive selected for an uncoated magnet is not automatically suitable for a coated magnet. For surfaces which are particularly difficult to bond, e.g. nickel plating, the market offers tailor-made adhesives. With painted magnets care must be taken to ensure that the adhesive does not attack the painting or cause blisters. VAC have indepth experience with a large number of adhesives and the most commonly used surfaces, and will be pleased to help customers select the right adhesive for their application. 8. INTEGRATED MANAGEMENT SYSTEM Documentation of the quality, environmental and industrial safety management system in a corporate quality management system was integrated in the financial year 23. Currently it is based on the following set of standards: DIN EN ISO 91:2 ISO/TS 16949:22 DIN EN ISO 141:25 OHSAS 181:1999 ISO/IEC 1725:25 8.1 QUALITY MANAGEMENT Quality is an essential aspect of our corporate policy. In order to reliably realise the high quality of our products and services based on a quality management system certified in accordance with DIN EN ISO 91 and ISO/TS 16949 we set great store by close cooperation of all operational divisions. Further development of our Total Quality Management (TQM), introduced as early as 1994, has been continual, and it is orientated towards business excellence models and our corporate goals. 51
The most important target of all our quality managementrelated actions is fulfilling all customers expectations and great customer satisfaction, both internally and externally. To further optimise VAC-internal processes with the primary objective of further reducing costs the Six-Sigma analysis was introduced in all our operations in the fiscal year 22. We achieved the product quality demanded by our customers by the definition and implementation of targeted QM measures during product and process planning, strictly controlled raw material procurement and test sequences integrated in the process using a statistical process control (SPC). Compliance with relevant process feasibilities (cpkvalues) is a matter of course for us as is documenting the essential magnetic and geometric properties. For complexe tasks or for especially stringent requirements we define a quality assurance programme jointly developed with our clients. By qualified technical advice we help to design and realise quality and cost-effective products and services; at the request of our customers we also conclude quality assurance agreements (QAA). 8.2 TECHNICAL TERMS AND CONDITIONS OF SALE Like most other permanent magnet materials, sintered magnets of rare earth alloys are brittle. Although VACODYM is mechanically more stable than VACOMAX, for this material it is also impossible to exclude that magnets exhibit fine hair-line cracks or chipped edge defects. This does not significantly influence the magnetic or mechanical properties of the concerned parts. The exchange of critical samples has in serial production proved itself for the test and definition of the visual quality of magnets. Unless we have a special agreement with our customers, in our quality inspection we allow mechanical surface damages (flaking, edge and corner chippings) up to a total of max. 2% per pole surface. The permissible chippings are to be defined jointly with the customer or using critical samples for small magnets with a pole surface of <2 mm 2. Up to a third of the concerned cross-sectional area of fine hair-line cracks will not be rejected as long as the mechanical stability in accordance with the intended use is met. 52
Under normal manufacturing conditions, slight amounts of magnetic dust and material debris may adhere to finished, in particular to uncoated and magnetized parts. If this is not acceptable, a coating resp. individual packing is to be provided. The final inspection of our magnets and assemblies is normally based on a standardized fixed sampling rate. Unless otherwise agreed with customers we test to DIN ISO 2859-1, AQL.65 with the c = acceptance number. By consistently employing the latest quality assurance techniques we are frequently able to agree to even tighter tolerances on request. For instance, for products for the automotive industry an additional process capability value of c pk > 1.33 is specified for geometric characteristics. Acceptance conditions for special magnetic properties call for clearly defined test procedures and reference samples. A further prerequisite, in particular for VACOMAX, is that the parts are supplied in the magnetized state. With miniature magnets dimensions less than approx. 2 mm reduced magnetization is to be expected owing to surface effects and depending on the position of the working point. If you require more information, please contact us. 8.3 ENVIRONMENTAL AND SAFETY MANAGEMENT We are committed to protecting our environment and to using the available natural resources as economically as possible. This principle applies to our production processes as well as to our products. Already at the development stage of our products we take potential damage to the environment into consideration. It is our aim to avoid or reduce to a minimum any harmful effects our precautions frequently exceed those stipulated by law. VAC environmental management assures that the standard of EN ISO 141 is effectively put into practice. Technical and organisational means for this purpose are regularly audited and are subject to continuous improvement. A further goal in the design of our products, processes and workplaces is the health and safety protection of our staff and our partners based on OHSAS 181. Here the applicable laws, standards and regulations are taken into account together with state-of-the-art expertise on occupational medicine and industrial science. 53
9. SAFETY GUIDELINES FOR HANDLING MAGNETS MADE OF VACODYM AND VACOMAX Magnetized rare-earth magnets of VACODYM and VACOMAX exhibit high field and exert strong, attractive forces on iron and other magnetic parts in their vicinity. Consequently, they must be handled with care to avoid damage. Owing to their strong magnetic forces there is a risk of injury when handling larger magnets. They should always be manipulated individually or with the aid of jigs. We recommend protective gloves be worn as well as for handling of uncoated VACO- MAX and Ni-coated parts, especially for people with allergies to metals. The high fields can change or damage the calibration of sensitive electronic devices and measuring instruments. Please note that magnetized magnets must be kept at a safe distance (e.g. over 2 m) from pacemakers, computers, monitors and all magnetic data storage media (such as floppy disks, credit cards, audio and video tapes etc.). On impact rare-earth magnets may develop large sparks. Never handle them in an explosive atmosphere. Unprotected VACODYM and VACOMAX magnets must not be exposed to hydrogen. Its adsorption destroys the microstructure and leads to disintegration. The only effective protection is gas-proof encapsulation of the magnets. Machining magnets requires special safety precautions for the grinding slurry. Especially for VACOMAX legal regulations regarding the handling of Co-containing dust have to be observed. The EG Safety Data Sheets provide more comprehensive information on the safety aspects involved when handling VACODYM and/or VACOMAX magnets. 54
1. APPENDIX 1.1 TECHNICAL PRINCIPLES AND TERMS 1.1.1 HYSTERESIS LOOP The behaviour of a magnetic material in a magnetic field is characterized by the correlation between magnetic flux density (induction) B and magnetic field strength H (B(H) hysteresis loop). The same correlation can be described by the polarization J (J(H) hysteresis loop, Fig. I). The flux density B and the polarisation J are given by B = µ H + J. The first quadrant of the hysteresis loop describes the magnetization behavior of the material: when applying a magnetic field H the flux density B of a non-magnetized material varies along the virgin curve (cf. Fig. I). When all magnetic moments are oriented parallel to the external magnetic field, the polarization J is at its maximum value, the saturation polarization J s (J = J s = const.). The flux density B however, continues to increase linearly with the field strength H. The minimum field strength required to attain saturation polarization is referred to as the saturation field strength Hs. If in the magnetized state the magnetic field strength is reduced, the flux density changes in accordance with the hysteresis loop and at H = attains residual flux density (remanence) Br (intersection of the hysteresis loop with ordinate). In the strongly anisotropic RE permanent magnets described here the remanence Br is in the same order of magnitude as the saturation polarization J s : B r J s 1.1.2 DEMAGNETIZATION CURVE The second quadrant of the hysteresis loop describes the demagnetization behaviour of the material. The most important characteristic terms of permanent magnets which are operated exclusively in opposing fields (see working point for further details) are determined from the demagnetization curve. The most important characteristic terms of a permanent magnet are: Remanence This is obtained as described above from the intersection of the hysteresis loop and the ordinate (at H = we have B r = J r ). Coercivity The field strengths at which the flux density B or the polarization J reach zero are referred to as coercivities of flux density H cb or polarization H cj respectively (intersection of the hysteresis loop B(H) and J(H) with the abscissa). Energy Density The product of the related values from flux density B and field strength H can be attained from any point along the demagnetization curve (see Fig. II). This product represents the energy density and passes through a maximum value between remanence and coercivity, the maximum energy density (BH) max. As a rule this value is used to grade permanent magnet materials. Working Point The magnetic field originating from the poles of a permanent magnet has a demagnetizing effect as it is in the opposing direction to polarization J. The operational state of a permanent magnet is consequently always in the range of the demagnetization curve. The pair of values (B a,h a ) applying to the relevant operational state is referred to as working point P. The position of P depends on the geometry of the magnet or in magnetic circuits with soft magnetic flux conductors on the ratio of air-gap length to magnet length. P is obtained from the intersection of the working or shearing lines with the B(H) curve (see Fig. III). The best use of a permanent magnet in static systems is when the working point P lies in the (BH) max point. Shearing in the magnetic circuit should practically be selected so that the working point is just at this position or, preferably, just above it, i.e. is in slightly lower opposing field strengths. 55
For dynamic systems with changing operating straight lines (e.g. motors) shearing should be selected so that the permanent magnet s working point remains within the straight line range of the demagnetization curve. The reason is to ensure great stability from outside field and temperature influences (see Fig. III p. 57). The working point shifts to a higher opposing field strengths, e.g. from P 1 to P 2 if the air gap in a magnet system is increased. If the change is reversed the original working point P 1 can only be reproduced if P 2 is within the linear section of the demagnetization curve. However, if P 2, as shown in Fig. III, is below the knee of the demagnetization curve irreversible losses arise. The working point shifts to P 3 on an inner return path with a correspondingly lower flux density. The rise of this return path is referred to as permanent permeability. within the linear section of the demagnetization curve over the entire temperature range in which the magnet is to be used. A permanent magnet can be completely demagnetized by heating to temperatures above the Curie temperature Tc. After cooling to the initial temperature the old state of magnetization can be reproduced by magnetizing again providing heating has not caused changes in the microstructure. It follows that thermal demagnetization is only possible with magnets made of VACODYM. Here the Curie temperature is within a range where changes in the microstructure do not occur. In contrast thermal demagnetization may not be performed on VACOMAX because the range of Curie temperature in these alloys is substantially higher and at more than 7 C phase transitions occur which may destroy the permanent magnet properties irreversibly. 1.1.3 INFLUENCE OF TEMPERATURE The demagnetization curves of permanent magnets are temperature dependent. This dependence is characterized by the temperature coefficients of the remanent flux density TC(B r ) and the coercivity TC(H cj ): 1 db TK(B r ) = r 1 (%/K) dt B r 1 dh TK(H cj ) = cj 1 (%/K) dt H cj A change in temperature causes the working point to shift on the working line (see Fig. IV p. 57). As long as the working point stays within the linear region of the demagnetization curve, the changes in flux density are reversible, i.e. after cooling the flux density returns to its original value. In all other cases any change in flux density is irreversible (irreversible magnetic losses) and can only be cancelled out by remagnetization. 1.1.4 MAGNETIC SIZES AND UNITS The most important magnetic sizes, their units and conversions are as follows: Unit and SI-units 1 ) Conversion Symbol table flux density B T (Tesla) 1 T = 1 Vs/m 2 = 1 kg (Induktion) (Kilogauss) Polarization J T (Tesla) s. flux density B Magnetic field A/m 1 A/cm =,4 Oe strenght H 1,257 Oe (Oersted) Energy density kj/m 3 1 kj/m 3 =,126 1 6 MGOe (BH) max Max. energy product Magnetic Wb (Weber) 1 Wb = 1 Vs = flux 1 8 Mx (Maxwell) 1 ) Basic units in SI-systems: meter, kilogram, second, Ampere. The units Gauss, Oested or Maxwell in the conversation table refer to the cgsor Gaussian system with the basic units centimeter, gram and second. To avoid irreversible changes in the flux density through temperature fluctuations, the working point must remain 56
virgin curve Fig. I Fig. III Fig. II Fig. IV 1.2 CONVERSION TABLE CELSIUS FAHRENHEIT C F C F C F C F C F C F 2 : 4 5 : 122 12 : 248 19 : 374 26 : 5 33 : 626 1 : 14 6 : 14 13 : 266 2 : 392 27 : 518 34 : 644 : 32 7 : 158 14 : 284 21 : 41 28 : 536 35 : 662 1 : 5 8 : 176 15 : 32 22 : 428 29 : 554 2 : 68 9 : 194 16 : 32 23 : 446 3 : 572 3 : 86 1 : 212 17 : 338 24 : 464 31 : 59 4 : 14 11 : 23 18 : 356 25 : 482 32 : 68 57
11. DUCTILE PERMANENT MAGNET ALLOYS AND SEMI-HARD MATERIALS (MAGNETIC AND MECHANICAL PROPERTIES) Material CROVAC CROVAC CROVAC CROVAC MAGNETO- VACOZET SEMIVAC SENSOR- 12/16 16/16 12/5 16/55 FLEX 35U 258 9 VAC Main components FeCrCo CoFeV CoFeNi FeCrCoNiMo FeNiAlTi Variant isotrop anisotrop Forms of wire supply strip wire strip Remanence (T),85-,95,8-,9 1,15-1,25 1,1-1,2,8-,9 1,3-1,5,9-1,3 1,3-1,6 Coercivity (ka/m) 36-42 39-45 47-55 53-61 25-3 2,-3,2 4-1 1,5-2,6 Coercivity tolerance (ka/m) +/- 2 +/- 2 +/- 3 +/- 3 +/- 1,5 +/-,15 +/-,5 +/-,15 Energy density (BH) max (kj/m 3 ) 13 15 35 37 12 2,5 5 3 Density (g/cm 3 ) 7,6 8,1 8,1 7,85 7,65 Curie temperature ( C) 64 7 8 7 63 Max. application temperature ( C) 48 5 4 45 3 TK (BR) -25 C - 25 C (%/K),3 -,1 Therm. expansion (RT-1 C) (1-6/K) 1 11 11 El. resistivity ( mm 2 /m),7,65,15 Vickers hardness HV as rolled 33 48 4 soft annealed 23 hard treated 48 9 6 7 6 Tensile strenght RM as rolled (MPa) 115 185 17 soft annealed (MPa) 62 heart treated (MPa) 15 Elongation as rolled (%) 2 1,5 3 soft annealed (%) 2 heart treated (%),5 The elongation is given for AL5 (strips) rsp. AL1 (wire). The above mechanical properties are given as related values. A detailed description of these materials is included in our leaftet PD-3, which is available on request. 58
59
VACUUMSCHMELZE GMBH & CO. KG GRÜNER WEG 37 D-6345 HANAU / GERMANY PHONE +49 6181 38 FAX +49 6181 38 2645 INFO@VACUUMSCHMELZE.COM WWW.VACUUMSCHMELZE.COM VAC SALES USA LLC 2935 DOLPHIN DRIVE SUITE 12 4271 ELIZABETHTOWN KY / USA PHONE +127 769-1333 FAX +127 765 3118 INFO-USA@VACUUMSCHMELZE.COM VACUUMSCHMELZE SALES OFFICE SINGAPORE 3 BEACH ROAD #31-3 THE CONCOURSE SINGAPORE 199555 PHONE +65 6391 26 FAX +65 6391 261 VAC.SINGAPORE@VACUUMSCHMELZE.COM PD 2 - VACODYM/VACOMAX EDITION 27 Published by VACUUMSCHMELZE GmbH & Co. KG, Hanau VACUUMSCHMELZE 27. All rights reserved. As far as patents or other rights of third parties are concerned, liability is only assumed for products per se, not for applications, processes and circuits implemented within these products. The information describes the type of product and shall not be considered as assured characteristics. Terms of delivery and rights to change design reserved. ADVANCED MATERIALS THE KEY TO PROGRESS