Fortron PPS for Thermoplastic Composites Celanese PPS-014 AM 10/13

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1 Fortron PPS for Thermoplastic Composites 2013 Celanese PPS-014 AM 10/13

2 Contents Introduction to Ticona Fortron PPS Chemistry Properties Applications Fortron PPS Composites Background Processing Options Properties Applications Summary 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 2

3 Celanese Maintains Leading Position in Engineered Materials Service temperature High-Performance Polymers (HPP) (TI 1 > 150 C) Engineering Polymers (ETP) (TI C) Engineering Polymers LCP Vectra /Zenite PPS Fortron PCT Thermx PET Impet PBT Celanex PBT Alloy Vandar TPC-ET Riteflex POM Hostaform /Celcon UHMW-PE GUR Long Fiber and Continuous Fiber Reinforced Thermoplastics* LFRT Celstran, Factor Compel Basic Polymers Amorphous Partially crystalline CFR-TP Celstran Tapes, Rods and Profiles TI 1 = Temperature Index * with Matrix Polymers: PP, PA, PPS, PBT, POM and others on request 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 3

4 Fortron PPS Summary Structure and Properties Semicrystalline T g 85 C, T M 285 C Density 1.35 g/cm³ Inherently Flame Retardant: UL94-V0, LOI > 45 n Chemical Resistance Dimensional Stability Fuels, oils, solvents Water-glycol Polyphenylenesulfide (PPS) Poly(thio 1,4 - phenylene) Easy to Process Injection molding Extrusion 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 4

5 Fortron PPS Semi-crystalline thermoplastic polymer, perfectly suited for parts that have to withstand the high mechanical and thermal requirements which require A high melting point range between 280 and 290 C Inherently flame resistant Excellent resistance to chemicals, oils and fluids An ideal alternative to conventional materials such as thermosetting polymers and metals High hardness and stiffness and superb long-term creep under load properties Ease to injection mold, blow mold and machine Weight reduction combined with high dimensional stability 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 5

6 Fortron PPS Has No Known Solvent Below 200 C Chemical resistance with minimal attack or swelling even at elevated temperatures Resists: acids/bases ph 2 to 12 Resists: strong bleaches Resists: auto fluids coolants, transmission & brake Resists: gas & alternate fuels (methanol, ethanol) Resists: hydrolysis 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 6

7 Fortron 0214C1 Matrix Material for Composites Linear, unmodified PPS polymer High molecular weight / high viscosity: 140 pa s For extrusion and injection molding applications Specified for aircraft applications In use at Airbus and Boeing VIAM qualification Federal state unitary enterprise All Russian Scientific Research Institute of Aviation Materials Tested in regards to flammability, smoke density and smoke toxicity: ABD0031 FAR/JAR New: DIN 5510 and ISO Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 7

8 Fortron PPS 0214C1 Smoke Density Tested with 2 mm Plaques Smoke density according to Airbus Standard ABD0031 Non-flaming Max. Value: 0, Average: 0 DS 4 min: 0; ABD and FAR Passed Flaming Max. Value: 32 (6 min.), Average: 23 (6 min) DS 4 min: 15; ABD and FAR Passed Tox-Test (ABD0031): ABD / FAR passed Value Max. Value in ppm Hydrogen Cyanide HCN: NF: 0 F: Carbon Monoxide CO: NF: 0 F: Nitrous Gases NO-NO 2 : NF: 0 F: Sulfur Dioxide/Hy. Sulfide SO 2 -H 2 S: NF: 0 F: Hydrofluoric Acid HF: NF: 0 F: Hydrochloric Acid HCl: NF: 0 F: Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 8

9 Fortron 0214C1 Flammability Tested With 2 mm Plaque Vertical Burning Test 12 s ABD0031 Total burn time: 12 s Flame extinguish time: 0 s No. of particles: 0 Ignited particles: 0 Total burn length: 5 mm Vertical Burning Test 60 s ABD0031 Total burn time: 60 s Flame extinguish time: 0.6 s No. of particles: 2.4 Ignited particles: 1.4 Total burn length: 44 mm 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 9

10 Internal UL Flammability Testing Material Part Thickness Unaged Sample Rating Aged Sample Rating Unfilled Fortron PPS Control 3.0mm (0.12 ) V-0* V-0* 1/32 V-0 V-2 1/64 V-2 V-2 Unfilled PEEK Control 3.0mm (0.12 ) V-0* V-0* 1.5mm (0.059 ) V-0* V-0* 1/32 No V-Rating V-2 1/64 No V-Rating No V-Rating Thin PEEK samples failed to achieve a V-Rating because of long burn times and cotton ignition Thin PPS parts have V-0 equivalent burn times but molten polymer drips can ignite the cotton = V-2 Rating *Data as reported by Underwriters Laboratory 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 10

11 Fortron PPS Dimensional Stability Extremely low moisture absorption 0.02% Minimal effect of temperature CLTE 19 x 10-6 / C (6165A4) Precision molding Low shrinkage - 0.3% (6165A4) Creep resistance For Precision Parts Even at Elevated Temperatures 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 11

12 Low PPS Water Absorption Results in Dimensional Stability (%) PPS PEI PEEK 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 12

13 Top Fortron PPS Segments Semicon Industrial EE & Sensors Fibers Automotive Composites 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 13

14 Fortron PPS Automotive: Under the Hood Throttle Body 1140L4 Inlet Tank for CAC 1140L4 Water Pump 6165A6, 1140L6 Crankshaft Flange 4332L6 Water Pump Impeller 1140L Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 14

15 Fortron PPS Automotive: Fuel Applications Fuel Injection Rail Fortron PPS was selected for: Resistance to all sorts of fuels including autooxidized fuels up to 120 C Excellent mechanical and impact strength at elevated temperatures Inherently flame resistant (UL 94 V-0) Lower specific gravity than metal Simplified fabrication by eliminating secondary operations Fuel Pump Parts 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 15

16 Fortron 1140L4 Water Pump Impellers The challenge: Improve pump efficiency Decrease water pump cost Improve fuel efficiency (Lower HP requirements) The innovation: Exotic blade shapes improve pump efficiency by 10-20% vs. sheet metal Fortron PPS has required chemical / hydrolysis resistance to OAT coolants Excellent fatigue properties withstand pressure cycles Excellent erosion resistance 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 16

17 Fortron PPS Industrial Gas Furnace Tray Chemical Metering Pump Washing Machine Light Fixture Medical Forceps Instant Hot Water Heater 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 17

18 Fortron PPS Extrusion: Film, Fiber, Netting, etc. Aircraft Composite Filter Netting High Tenacity Monofilament Stock Shapes CPI Filter 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 18

19 Fortron PPS for Thermoplastic Composites May Celanese PPS-014 AM 10/13

20 Why Thermoplastic Matrix Composites? Melt processible Can be reformed Near infinite shelf life No refrigeration needed Common generalized attributes: Good in fatigue Insensitive to moisture Tough Higher temperature Damage tolerant Excellent FST Good chemical compatibility in aircraft fluids 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 20

21 Why Thermoplastic PPS Composites vs. Thermoset Composites? Improved Properties Tougher, good fatigue performance 4x tougher than toughened epoxies Damage tolerant Insensitive to moisture High-temperature performance Very low flammability, smoke, toxicity Low residual stress in molded parts Excellent chemical resistance Improved Processing Eliminate bagging materials and labor May also eliminate kitting and debulking steps and equipment Eliminate autoclave possible Cost, space and bottleneck issues Rapid processing vs. thermosets Can be reformed Simple, longer lasting tool Fusion bonding eliminates fasteners and adhesives Reduces cost and weight Green processing Recyclable No VOCs in processing Less process scrap Fewer process energy requirements 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 21

22 Thermoplastic Composite Matrix Cost Advantage System Cost in % Processing Material The material cost for a thermoplastic matrix might be equal or even higher Lower cost for handling, processing, and assembly can lead to a substantial advantage in total cost 0 Conventional Thermoplastic Even the High Cost Thermoplastic Polymers Offer Improved Cost Savings vs. Epoxy Based Composites 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 22

23 Thermoplastic Composite Value Chain Raw Materials Intermediate Products Fabrication Processes End Users Fibers Film E Glass Fabric S2 Glass Prepreg Carbon/ Graphite Aramid/Kevlar Slurry Polymer Boron/Ceramic Resins Liquid PEEK PPS PEI Nylons PP Etc Dry Powder Hot Melt Comingle Tows Fabric Pultrusion Lamination Molding Oven Match Bladder Fiber Placement Filawinding AFP Sheets Rods Pipes/Tubes Beams Shapes Structures 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 23

24 Example for Value Chain in Aircraft Industries Plastic Pellets Film Producer Producer of Composites Thermo- Forming- Process Assembling Aircraft 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 24

25 Station 1: Film Production Fortron PPS Pellets Starting Product: PPS Pellets Temperature stability High level of hardness and impact strength Excellent resistance to chemicals Broad temperature range Inherent flame resistance Film Production Station 1 Lipp-Terler GmbH in Gaflenz near Linz, Austria. The pellets are converted into films with a thickness of 50 to 200 µm. The film leaves the special plant in rolls of 100 kg in a flawless state, crystal clear and with the required characteristics with regard to strength and dimensional stability Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 25

26 Station 2: Composite Production Fortron PPS Film e. g. Carbon Fiber Starting Product: Basic Matrix of PPS / Carbon Fiber Fabric Laminate Production Station 2 Ten Cate Advanced Composites BV, Nijverdal, Netherlands. The carbon fiber fabric and PPS film are bonded together in a press, under high pressure and high temperature, into high-strength, dimensionally stable and resistant composites in the desired layer thickness Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 26

27 Station 3: Thermoforming Positive Form Composite Plate Starting Product: Composite plates in the required size Negative Form Shaping Station 3 Fokker Special Products, Hoogeveen, Netherlands. The composite plates are preheated and subsequently shaped into the desired form under pressure and high temperature Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 27

28 Station 4: Assembly Front Wing Portion Starting Product: Front wing portion (Weight of the parts is 20 percent less than aluminum) Assembly Station 4 Airbus The completed construction element is mounted at the intended location Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 28

29 Technology Breakthrough: Fixed Wing Leading Edge Airbus Welded structure Low weight and low cost monolithic design 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 29

30 Fortron PPS Success in the Aviation Industry Safe, efficient, environmentally friendly Modern design Licensed for aircraft construction New applications from Fortron PPS 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 30

31 Thermoplastic Composite Processing Technologies Pultrusion Continuous laminating Compression molding Thermoforming Automated tape laying/fiber placement Bladder molding 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 31

32 Process Cost vs. Part Complexity for Continuous Fiber Reinforced Parts Part Complexity Continuous Molding Pultrusion In-Situ Filament Winding, Tape Placement Sheet Forming: Stamping, Roll Forming Diaphragm Forming Prepreg Molding Compression Molding, Autoclave Relative Cost Source: Composite Market Reports 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 32

33 Continuous Fiber TPC Processes Rods/Profiles/Sheets Pultrusion Continuous/Semi-continuous molding Batch molding (press, autoclave) Tubes/Pipes Fiber/Tape placement (In situ) Table roll/oven molding (2 Step) Table roll/bladder molding (2 Step) Complex Geometries (draws, bends, etc.) Automated tape lay-up/fiber placement Mold processing (compression, bladder) Diaphragm, matched metal, thermoforming/folding, et al 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 33

34 Additional Thermoplastic Composite Manufacturing Processes Automated Dynamics Fiber Placement Lingol Thermoforming FiberForge Compression Molding 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 34

35 Advantages of Thermoplastic Composite Automation Processes Accurate fiber placement at any angle Material savings Labor savings Quality improvement Automatic debulking Reduced manufacturing space Reduced assembly costs 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 35

36 Environmental Attributes for Thermoplastic Composites Reduced Energy Requirements Reduced Scrap and Reusability/Repairability Reduced VOCs and Toxic Cure By-Products 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 36

37 Reduced Scrap and Reusability/ Repairability Thermosets Prepreg Shelf Life Scrap Ends in Landfill Rework can be Difficult Thermoplastics No Prepreg Shelf Life All Scrap can be Reused e.g., Pelletized for Injection Molding Rework is easier since Thermoplastics can be Melted and Reformed 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 37

38 Reduced Process Energy Example for TP vs TS Composites Thermosets Assemble part in tool Match Mold Process Cycle (1+ hours) Cool, removal Thermoplastics Assemble part in tool Stamp /Thermoform Cycle (minutes) Subsequent part can be stamped immediately Additional Savings: No Need for Prepreg Freezers Reduced Facility HVAC Costs Energy Required Per Part Can Be Less Than a Factor of 10 for TP vs. TS with Match Metal Molding of Simple Parts 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 38

39 Reduced VOCs and Toxic Products Thermosets Prepregs usually Contain Solvents (VOC s) for Tackiness Cure By-Products can be Complex Organic Compounds Halogenated Additives Are Typically Used to Reduce Flammability But Toxicity is Increased Thermoplastics Prepregs Do Not Contain Solvents No Cure By-Products No Halogenation Necessary for Most High Performance Thermoplastics Excellent FST Performance 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 39

40 Thermoplastic Composite Properties Tg, C High Load Continuous use Temperature, C Approx. Resin Cost, $/lb Approx. Carbon Reinforced prepreg Cost, $/lb Fortron PPS PEI PEEK Fortron PPS High-Performance, Low-Cost Solution 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 40

41 Fortron PPS Carbon Fiber Composite Properties Thermo-Lite 1466P Physical Property Data Fiber Type AS-4 Resin Type PPS Fiber Weight % 66±3 Resin Weight % 34±3 Fiber Volume % 59±3 Resin Volume % 41±3 Fiber Areal Weight 150 g/m 2 Total Areal Weight 227 g/m 2 Density 0.58 lb/in 3 (1.61 g/cm 3 ) Thickness/Ply (0.14 mm) Tape Width 12 (30.5 cm) Mechanical Property Data 1 Laminate Property Fiber Orientation Test Data Tensile Strength Ksi (MPa) (2,045) (50) Tensile Modulus Msi (GPa) (127) (8.8) Compression Strength Ksi (MPa) (1,117) Compression Modulus Msi (GPa) (118) Flexural Strength Ksi (MPa) (1,672) Flexural Modulus Msi (GPa) (112) Shear Strength (4 Point) Ksi (MPa) (77) 1 Typical mechanical properties at room temperature, dry condition 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 41

42 Fortron PPS Carbon Fiber Composite Properties Thermo-Lite 4268P Physical Property Data Fiber Type E-Glass Resin Type PPS Fiber Weight % 68±3 Resin Weight % 32±3 Fiber Volume % 53±3 Resin Volume % 47±3 Fiber Areal Weight 260 g/m 2 Total Areal Weight 382 g/m 2 Density lb/in 3 (2.0 g/cm 3 ) Thickness/Ply (0.19 mm) Tape Width 12 (305 mm) Mechanical Property Data 1 Laminate Property Fiber Orientation Test Data Tensile Strength Ksi (MPa) (1,118) ± (135) (46) Tensile Modulus Msi (GPa) (44) ± (14.5) (13.8) Open Hole Tensile Strength Ksi (MPa) 0 / ±45 / (207) Open Hole Tensile Modulus Msi (GPa) 0 / ±45 / (18.6) Compression Strength Ksi (MPa) (1,111) Compression Modulus Msi (GPa) (41) Open Hole Compression Strength Ksi (MPa) 0 / ±45 / (304) Open Hole Compression Modulus Msi (GPa) 0 / ±45 / (23.5) In Plane Shear Modulus (Iosipescu) Ksi (MPa) (61) In Plane Shear Modulus (Iosipescu) Msi (GPa) (5.5) Flexural Strength Ksi (MPa) (1,201) Flexural Modulus Msi (GPa) (43) Shear Strength (4-point) Ksi (MPa) (63) 1 Typical mechanical / physical properties 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 42

43 Fortron PPS Carbon Fabric Composite Physical Property Data Physical/Thermal (nominal values) T300 5HS/pps with double sided Amcor foil Mass of fabric 8.26 oz/yd g/m 2 Mass of fabric + resin oz/yd g/m 2 Resin content by volume 50 % 50 % Resin content by weight 43 % 43 % Moisture pick up 0.1 % 0.1 % Ply thickness In 0.31 mm Specific gravity 96.7 lb/ft g/cm 3 Tg (DSC) (amorphous) 194 F 90 C Tg (DSC) (crystalline) 248 F 120 C TM 536 F 280 C High Quality prepreg made by film infusion of fabric Excellent wetout of fabric by resin Reproducible and uniform No shelf life * TenCate CETEX Data CETEX is a registered trademark of TenCate Advanced Composites, BV 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 43

44 Fortron PPS Carbon Fabric Composite Mechanical Property Data* Mechanical Properties 73 F (23 C)/50% RH 7781/PPS Tensile strength warp 49.3 ksi 340 MPa Tensile strength weft 48.3 ksi 333 MPa Tensile modulus warp 3.1 Msi 22 GPa Tensile modulus weft 2.9 Msi 20 GPa Compression strength warp 61.6 ksi 425 MPa Compression strength weft 42.8 ksi 295 MPa Compression modulus warp 3.7 Msi 26 GPa Compression modulus weft 3.5 Msi 24 GPa Flexural strength warp 74.2 ksi 511 MPa Flexural strength weft 56.6 ksi 390 MPa Flexural modulus warp 3.3 Msi 23 GPa Flexural modulus weft 2.9 Msi 20 GPa In plane shear strength 11.6 ksi 80 MPa In plane shear modulus ksi 3714 MPa Open hole tensile strength 23.0 ksi 158 MPa Open hole compression strength 26.5 ksi 183 MPa Compression after impact 24.8 ksi 171 MPa Bearing strength yield 46.1 ksi 318 MPa Bearing strength ultimate 74.8 ksi 516 MPa * TenCate CETEX Data 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 44

45 T300 3K Carbon Fabric/Fortron PPS Composite Property Data* C 23 C 80 C Tensile Strength Compressive Strength Flexural Strength In Plane Shear Open Hole Tensile Open Hole Compressive Compression After Impact Values are in ksi Warp direction data Average values - Tested per Mil-R-17 * TenCate CETEX Data Steady and Stable Across Use Temperature 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 45

46 T300 3K Carbon Fabric/ Fortron PPS Composite Property Data* * TenCate CETEX Data Tensile Modulus, msi Compressive Modulus, msi Values are in msi Warp direction data Average values - Tested per Mil-R-17 Flexural Modulus, msi -55 C 23 C 80 C In Plane Shear Modulus, msi Steady and Stable Across Use Temperature 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 46

47 Working Together in the Aviation Industry 2013 Celanese PPS-014 AM 10/13

48 Technology Validation Carbon/PPS: Fokker 50 Undercarriage Door Final step in a dedicated 10-year program Press-formed ribs and spars Welded assembly Qualified carbon / PPS material Certified by the Airworthiness Authorities Flown on a KLM aircraft for 3.5 years 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 48

49 Technology Breakthrough: Fixed Wing Leading Edge Airbus A /600 Welded structure Low weight and low cost monolithic design Strong partnering with Airbus UK and TenCate Technology is now state of the art current application Airbus A Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 49

50 Metal Substitution with Linear PPS Composite Resulted in 20 50% Lighter Components KB WP: 18m, 2.5 tons Main Ribs (L&R) Keel Beam Application Multi-technology concept Panels and spars Thermoset Prepreg lay-up TP ribs and angles Aluminum and titanium brackets 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 50

51 A330/340 Family: Common Aileron A318 A319 A320 A321 A A A A Parts per Airframe A A Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 51

52 Airbus A /600 Aileron Thermoplastic Composite Parts Edge Ribs Main Ribs Edge Rib Leading Edge Ribs, Angles & Panels 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 52

53 Airbus A /600 Thermoplastic Composite Components Part Description: Panel of the Pylon Forward Second Structure 22 per Aircraft Dimensions: Material: L = mm W = mm Thickness 2.8 mm Double-Curvature Shape PPS / Carbon Fiber Bronze Mesh Top-layer for EMI Shielding 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 53

54 Leading Edge Airbus A380 8 assemblies / wing Wing length: 26 meters 16 segments, 52-meter length 400 kg total weight 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 54

55 Weight Reduction The Vision Fortron PPS in Aircraft Interior 46% Lighter Seat Parts Due to Metal Substitution Aluminum Fortron 280 g 150 g Product innovations for Composites 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 55

56 Weight Reduction The Vision Linear PPS for Aircraft Interiors Fortron PPS is the prime candidate for several aircraft interior efforts Applications include seat frames, brackets, beams, ducts Lower cost vs. PEI and PEKK 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 56

57 240 CETEX Parts in Ailerons Common Aileron for A Family 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 57

58 Summary Fortron PPS is a demonstrated, producible, low-cost, highperformance thermoplastic for composite applications Aircraft interior and exterior applications Down hole applications Corrosion resistant environments High-temperature usage The low-cost, green alternative Industrial thermoplastics composites manufacturing is a demonstrated production process Proven success in aerospace Ticona technical personnel will work with you to meet your composites needs 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 58

59 Disclaimer This publication was printed on 1 October 2013 based on Celanese s present state of knowledge, and Celanese undertakes no obligation to update it. Because conditions of product use are outside Celanese s control, Celanese makes no warranties, express or implied, and assumes no liability in connection with any use of this information. Nothing herein is intended as a license to operate under or a recommendation to infringe any patents. Copyright 2013 Celanese or its affiliates. All rights reserved. Contact Information Americas 8040 Dixie Highway, Florence, KY USA Product Information Service t: t: Customer Service t: t: e: info-engineeredmaterials-am@celanese.com Europe Am Unisys-Park 1, Sulzbach, Germany Product Information Service t: +(00) t: +49-(0) e: info-engineeredmaterials-eu@celanese.com Asia 4560 Jinke Road, Zhang Jiang Hi Tech Park Shanghai PRC Customer Service t: f: e: info-engineeredmaterials-asia@celanese.com 2013 Celanese PPS-014 AM 10/13 Fortron PPS for Thermoplastic Composites 59

60 Thank you. For more information: celanese.com/engineered-materials 2013 Celanese PPS-014 AM 10/13