旋翼机飞行手册 ROTORCRAFT FLYING HANDBOOK

时间：2011-04-05 11:32来源：蓝天飞行翻译 作者：航空 点击：次

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pinnacle, 10-8 shallow approach, 10-5 steep, 10-4 ARM 7-4 ASYMMETRICAL AIRFOIL 2-1 ATTITUDE INDICATOR 12-3 ATTITUDE INSTRUMENT FLYING 12-1 AUTOKINESIS 13-3 AUTOPILOT 5-10 AUTOROTATION 11-1 aerodynamics, 3-8, 16-1 during instrument flight, 12-19 from a hover, 11-4 power recovery, 11-3 straight-in, 11-2 with turn, 11-3 AXIS OF ROTATION 2-2
B
BASIC EMPTY WEIGHT 7-1 BERNOULLI’S PRINCIPLE 2-3 BLADE coning, 3-2 driven region, 3-9, 16-2 driving region, 3-9, 16-2 feather, 1-1 flap, 1-1, 16-6, 20-1 lead/lag, 1-1 reverse flow, 16-3 stall, 11-10 stall region, 3-9, 16-2 BLOWBACK 3-8 BUNTOVER 21-3
C
CARBURETOR 5-7 heat, 5-8 ice, 5-7 CENTER OF GRAVITY 7-2 aft CG, 7-2 forward CG, 7-2 lateral, 7-3, 7-7 CENTER OF PRESSURE 2-1, 16-5 CENTRIFUGAL FORCE 3-2, 3-8 CENTRIPETAL FORCE 3-8 CLUTCH belt drive, 5-4 centrifugal, 5-4 freewheeling unit, 5-4 sprag, 5-4 COANDA EFFECT 1-3 COCKPIT MANAGEMENT 20-1 COLLECTIVE CONTROL, GYROPLANE 17-2 COLLECTIVE PITCH CONTROL 4-1

COLLECTIVE PITCH/THROTTLE COORDINATION 4-2 COMPASS CORRECTION CARD 12-5 COMPASS DEVIATION 12-5 COMPASS ERRORS 12-4 COMPASS TURNS 12-17 CONFINED AREA OPERATIONS approach, 10-7 takeoff, 10-8 CONING 3-2 CONING ANGLE 18-1 CORIOLIS EFFECT 3-2 CORRELATOR/GOVERNOR 4-2 CREW RESOURCE MANAGEMENT 14-2 CYCLIC CONTROL, GYROPLANE 17-1 CYCLIC PITCH CONTROL 4-2

DATUM 7-3 DECISION-MAKING PROCESS 14-3 DENSITY ALTITUDE 8-1, 20-5 DIRECT CONTROL 15-2 DISC LOADING 2-4 DISSYMMETRY OF LIFT 3-6, 16-3, 20-1 DIVERSION 11-15 DRAG 2-5 form, 2-5 induced, 2-5 parasite, 2-6 profile, 2-5 rotor, 16-4 skin friction, 2-5 total, 2-6 DUAL ROTOR SYSTEM 1-1 DYNAMIC ROLLOVER 11-7

EFFECTIVE TRANSLATIONAL LIFT 3-5 ELECTRICAL SYSTEMS 5-8 EMERGENCIES aborted takeoff, 21-1 approach and landing, 21-3 autorotation, 11-1 buntover, 21-3 dynamic rollover, 11-7 ground resonance, 11-7, 21-3 instrument flight, 12-18 lift-off at low airspeeds and high angles of attack, 21-1 lost procedures, 11-16 low G conditions, 11-10 low rotor r.p.m. and blade stall, 11-10 mast bumping, 11-10 pilot-induced oscillation, 21-2 power pushover, 21-3 retreating blade stall, 11-6 settling with power, 11-5 systems malfunction, 11-11 vortex ring state, 11-5 EMERGENCY EQUIPMENT AND SURVIVAL GEAR 11-16, 21-4 ENGINE reciprocating, 5-1, 18-1
turbine, 5-1 ENGINE INSTRUMENTS 18-3 ENGINE STARTING PROCEDURE 9-2, 20-1 ENVIRONMENTAL SYSTEMS 5-10 EYE 13-1 cones, 13-1 rods, 13-2

FALSE HORIZON 13-3 FENESTRON TAIL ROTOR 1-2 FLIGHT AT SLOW AIRSPEEDS 20-12 FLIGHT CONTROLS 1-3, 4-1 antitorque pedals, 4-3 collective pitch, 4-1, 17-2 cyclic pitch, 4-2, 17-1 rudder, 17-2 swash plate assembly, 5-5 throttle, 4-1, 17-1 FLIGHT DIVERSION 11-15 FLIGHT INSTRUMENTS 12-1 airspeed indicator, 12-1, 18-4 altimeter, 12-2, 18-4 attitude indicator, 12-3 heading indicator, 12-3 magnetic compass, 12-4 turn-indicators, 12-4 vertical speed indicator, 12-2 FLIGHT MANUAL (See rotorcraft flight manual) FORCES IN A TURN 3-8 FOUR FORCES drag, 2-5, 16-4 lift, 2-3, 16-4 thrust, 2-5, 16-4 weight, 2-4 FREEWHEELING UNIT 5-4 FUEL INJECTION 5-8 FUEL SYSTEMS 5-6 FULLY ARTICULATED ROTOR 1-1, 5-4, 18-1

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