FSI LOGO Revision 1.0

Transcription

1 FSI LOGO Revision 1.0

2 HELICOPTER OPERATIONS

3 MODERN HELICOPTERS

4 MODERN HELICOPTERS

5 MODERN HELICOPTERS

6 MODERN HELICOPTERS

7 HUMS Ground Station Overview Health and Usage Monitoring System Ground Station Help System Pre-Flight Procedures Initializing a DTMU Card Post-Flight Procedures Downloading a DTMU Card Downloading from Other Sources Maintenance Debrief Rotor Tuning Procedures Vibration Diagnostics Mechanical Diagnostics Strip Chart Data Analysis Operation Explorer Generic Trending Reports Data Export Administration User Security Configure Tasks Configure Menu Aircraft Configuration Data Management.

8 Operators Off Shore Air Taxi Corporate Military State Government State Police Air Ambulance Fire Fighting SAR

9 Specialty Helicopter S-92 Rescue Hoist

10 Specialty Helicopters

11 Specialty Helicopters

12 Specialty Helicopters

13 Specialty Helicopters

14 Specialty Helicopters

15

16 HELICOPTER STRUCTURES S-76 C++

17 Aircraft Zones

18 Cockpit / Cabin Zone 1

19 Tailboom / Landing Gear Zone 2 Tailboom Fire Bottles AC Junction Box RCCB s DC Junction Box Landing Gear

20 Tail Rotor Pylon Zone 3 Tail Rotor Horizontal Stabilizer Tail Rotor Gearboxes Tail Rotor Driveshafts

21 Powerplant Zone 4 Allison 250-C30 TurboMeca Arriel 1S1 / 2S1 Pratt & Whitney PT6B-36B

22 Main Rotor / Flight Controls Zone 5 Flight Controls M/R Hub & Blades Main Transmission Hydraulics

23 Aircraft Systems Electrical Power Fuel Hydraulics Landing g Gear Flight Controls Powertrain Rotors Powerplant Floats Autopilot

24 TYPES of HELICOPTER ROTOR SYSTEMS Conventional, Tandem and Counter, Rotating Rotor Systems

25 Conventional Helicopter

26 Rotorhead Components Control Horn Pitch link MRB Swashplate Mast

27 Rotorhead Components

28 Drive system (Conventional)

29 Engine Inlet

30 BARRIER FILTER

31 ENGINE INSTALLATION

32 ENGINE INSTALLATION

33 MAIN GEAR BOX AND ROTOR HEAD ASSEMBLY

34 Accessory Gearbox

35 Tail Rotor Drive Shaft

36 INTERMEDIATE GEAR BOX

37 Tail Rotor Assembly

38 ROTOR BRAKE

39 TORQUE COMPENSATION

40 LATERAL LEAD

41 STABILATOR AIRFLOW - HOVER

42 STABILATOR AIRFLOW - INFLIGHT

43 TAIL PYLON AERODYNAMICS

44 NOTAR NOTAR

45 NOTAR

46 Helicopter Controls Cyclic

47 PITCH FLIGHT CONTROLS BLOCK DIAGRAM

48 ROLL FLIGHT CONTROLS BLOCK DIAGRAM

49 Helicopter Controls Collective

50 COLLECTIVE FLIGHT CONTROLS BLOCK

51 Yaw Pedals Helicopter Controls

52 YAW FLIGHT CONTROLS BLOCK DIAGRAM

53 FLIGHT CONTROLS SYSTEM COMPONENTS

54 TAIL ROTOR CONTROL CABLES

55 HYDRAULIC SYSTEM COMPONENTS

56 Tandem Helicopter

57 TANDEM ROTORS

58 Drive system (Tandem)

59 Combining Transmission Transmission i

60 Accessory Module Accessory Modules

61 Tandem Helicopters Hover Turn Sideward

62 COUNTER ROTATING

63 TYPES OF ROTOR SYSTEMS

64 ROTOR SYSTEMS Lynx A Star A Star

65 Fully Rigid BK-117

66 Semi-Rigid Bell Jet Ranger

67 Fully Articulated S-76

68 Fully Articulated MRB Damper Reservoir Bifilar Vibration Absorber Elastomeric Bearing Control Horn Damper

69 Elastomeric Bearings Droop Stop

70 Spindles ¾ Steel Bolt Outer Race Plastic Collar Inner Race

71 INSPECTION OWL

72 FLOATS

73 Floats

74 Floats

75 Float Bottle

76 Float Bottle

77

78 Inflated Floats

79 Floats

80 FlightSafety International MAIN ROTOR BLADE CONSTRUCTION

81 FlightSafety International BLADE INSPECTION METHOD (BIM)

82 FlightSafety International Blade Construction

83 FlightSafety International Blade Construction

84 FlightSafety International Blade Construction

85 FlightSafety International Blade Construction

86 FlightSafety International Blade Construction

87 FlightSafety International MEASURED STATION STA STA STA STA STA STA (SEE NOTE 4) ZONE 1 ZONE 2 ZONE 3 ZONE 4 15" 12" 9" 6" 0" D C B A D C B A 15" 12" 9" 6" 0" D C B A D C B A 10" BLADE STA NOTES 1. REINFORCED PLASTIC (0.090) INCORPORATES 6. ALL SHEET METAL CALLOUTS DEICING BLANKET. ARE 6061-T6 ALUMINUM ALLOY, QQ-A COMPOSITE MADE FROM GLASS FABRIC AND A -BASIC SKIN (0.063) REDUCED GRAPHIC PLIES, BONDED WITH ADHESIVE TO INCH THICKNESS. RESIN. B EXAMPLE -BASIC SKIN (0.063) REDUCED TO 3. INCORPORATES BIM BLANKET INCH THICKNESS. DAMAGE 10 INCHES TO FRONT 4. REPAIRS INBOARD OF ZONE 1 (STATION 60.0) 7. ON TIP CAP OF TRAILING EDGE AT BLADE DO NOT NEED TO BE RECORDED. REPAIRS STA IS IN ZONE 3C. IN THIS AREA WILL NOT AFFECT CHORDWISE 8. CRACKS ARE USUALLY FOUND AT OR SPANWISE BALANCE. HOLES 4 AND 5; 1/2 INCH OUTBOARD OF HOLE 6; BETWEEN HOLES 6 AND 7, 1 5. HELICOPTERS WITH BLADES SERIAL NOS INCH AFT OF HOLE 6. A TO A WILL HAVE A NOTCH IN TRIM TAB.

88 FlightSafety International ERROSION

89 FlightSafety International ERROSION

90 MRB Skin Disbond

91 Trailing Edge Delamination

92 Tail Rotor

93 TRB Spar Delamination

94 TRB Spar Delamination

95 Tail Rotor Failure

96 Blade Damage

97 Completed Repair

98 Sikorsky k X-2 THE FUTURE

99 PROTOTYPE HELICOPTER Sikorsky k X MPH Fly by Wire Twin Rotors Pusher Propeller

100 THE FUTURE AUTO PILOT Oil Rig Landings SAR Grids FLY BY WIRE Flight Controls

101 TRAINING TOPICS Rotorcraft Aerodynamics Rotor Systems Structures Rotor Blades Flight Controls Hydraulics Floats Hoists

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110 THE END Fred Banke FlightSafety International