Training Notes Turbine Engine

7/18/2019 Training Notes Turbine Engine

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:LSCTPICITY AND MAGNETISM

ENGINE IN5TALLA7I0!



SECTION-1, FIG. PAGE-".











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SECTION - 10

LUBRICANT AND LUBRICATING SYSTEM







r

•flTHE ROCKET ENGINE

(BIHE ENGINE







> r







SECTION - 11

COOLING, SEALING AND BLEED AIR SYSTEM









JL



:TION-I, FIG. PAGE-9





SECTION - 12

ICE PROTECTION SYSTEM









SECTION - 13

FIRE PROTECTION SYSTEM





w







42 FORWARD-FAM ENGIHE WI' • AND UNMIXED EXHA!

SECTIOH-1, FIG. PflC







j-iii

! i I





- rtdibdi





SECTION - 14

ELECTRICITY AND MAGNETISM



6







f ' —















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3 1





y [ I &1o !

t

J j"l

I







SECTION - 15

ENGINE IGNITION SYSTEM





ill

u) (

- s i -

pr V





i

i —4





SECTION - 16

ENGINE STARTING SYSTEM





















SECTION - 17

ENGINE INSTALLATION











SECTION - 2

ENGINE CONSTRUCTION









asa .;. "f







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SECTION - 18

ENGINE CONTROL AND INSTRUMENTS













AXIAL FLOW COME

SECTIOH-2. FIGURE PAGE-2













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VOLUME 2

FIGURES



SECTIOJJ-2, FIGURE PflGE-3















P I G . 2 - 1 2 A . O . A - H I



SECTION-2, FIGURE PAGB-6





-%^

T

JBRSE-FLOW COMBUi



CORRUGATED JOIN!

SPLASH COOLING STRIP

TRANSPIRATION COOLING

F I G . 2 - 2 0 FLAME TUBE COOLING METHODS

SECTION-2. FIGURE PAGE-9



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I G . 2 - 2 5 EXHAUST 1

HOLLOW INLET GUIDE

n o n - 2 . FIGURE PflGE-U



SECTION - 3

PROPELLER AND PROPELLER CONTROL SYSTEM

J f



SECTION - 1

PHYSICS AND GAS TURBINE ENGINE THEORY



SECTION OF A PROPI

T77TV™JLU\

r-V! V-l s

TVPICAL PROPELLER

IG-3.3 PITCH DISTHIB1

SECTION-3, FflGB-1



VELOCITY. THE ANGLB OF

BLADE IS THE SAME AS THE

FIG-3.7 AS THE ENGINE J

INCREASES FOR A GIVEN

FORWARD VELOCITY, THE

BLftDB DECREASES

SECTION-3. '



•17;

SCTION-3, PAGE-3



FIG-3. 14 T0RQU1

TWISTING HOHBMT THIBS°TODECREASE THE BLflDB ANGLE



3.17 STAGES IN THE PRODUCTION OF ft WOOD PROPELLEI



SPAR INTEGRAL WH . .

RETENTI ON NO COMP05IT1

CRITICAL RETENTION

INTEGRAL. DE ICING

HEATER DURABLEAN D EASILY REPAIRED

•JTEG BAL SEALED SH ELL TO SPAR CLOSURE





FIG-3 26 TYPICAL PROPELLER

HUBS FOB GBOUHD ADJUSTABLE

PROPELLERS

.28 TYPICAL SINGLE

; GOVERNOR FOR3E WEIGHT PROPELLER



I t H i



\\ _Jl_.

'EE-SPEED COHDITIt

)N-3, PflGE-9



i THE SOME POIHT

3N-1, FIG. PfiGE-1



iECTION-3. PAGE-K



SECTION-3. PfiGE-10



.BR REDUCTION GEAR

iECT10N-3. PfiGE-17





SECTIOH-3. PfiC



71







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= =-F +25523

srisi1, " , " ™ '

• 4 " - "

FIG . 1.5 IS(





EHG. OIL INLET j

:KEASE PITCH CHAMBER

m





7ION-3, PAGE-11



SECTION - 4

NOISE SUPPRESSION SYSTEM













m »P













SECTION - 6

AUXILIARY POWER UNIT

















D

- i !

l Tr

A









SECTION - 7

NIL



SECTION - 8

ENGINE FUEL CONTROL SYSTEM







SECTIOM-l. FIG. Pfl6B-5













If ,^i

K - 7

i

™(f-" - ' ^











-

ENGIHE HPM —~



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SECTION - 9

THRUST AUGMENTATION





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Training Notes Turbine Engine

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