training notes turbine engine

7/18/2019 Training Notes Turbine Engine

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:LSCTPICITY AND MAGNETISM

ENGINE IN5TALLA7I0!



SECTION-1, FIG. PAGE-".



„».,



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 ' —



&\~&\-_-. 1 - - , j , . t

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



\



SECTION - 18

ENGINE CONTROL AND INSTRUMENTS



AXIAL FLOW COME

SECTIOH-2. FIGURE PAGE-2



i



c^«r

I s -

«k



"UJ



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



w

///



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



O/f



*

."si's:1-1"

= =-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 —~



w



i'e



SECTION - 9

THRUST AUGMENTATION



( I

i

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