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FLIGHT

v

LENGTH

..

..

8lin.

ROLi*

(to airscrew rear cone)

HEIGHT

..

45in.

TACHOMETER DRIVE

AUXIIJARY GEARBOX DRIVE

CONSTANT SPEED UNIT MOUNTING FACE

WIDTH

DRY WEIGHT

. . 29.5in.

2,0901b.

INTERCOOLER

INDUCTION TRUNK. DELIVERING TO CYLINDER BLOCKS

WET CYLINDER INERS

MAX. B.H.P.

..

2,220

HONEYCOMB BLOCK

FRONTAL AREA

Bare engine . .

7.9 sq.ft.

Installed (Spitfire XIV) 11 sq. ft.

INTER-STAGE COOLANT CONNECTIONS TO AIRCRAFT RADIATORS

INTER-STAGE COOLING PASSAGE -

ACCELERATOR PUMP

INIECTOR

NOZZLE

INJECTOR FUEL NOZZLE

TURBULENCE SPIDER

SUPERCHARGER IMPELLERS

THREE-BARREL THROTTLE ENTHY

SUPERCHARGER CHANGESP6ED

|NTERCOOLER

COOLANT PUMP

SCAVENGE OIL FILTERS

FOUR

UNIT

ROLLS-ROYCE BENDIX-STROMBERG INJECTOR TYPE CARBURETTOR

This special copyright Flight drawing by Max Millar iays bare thecomponent arrangement andstructural design of the engine, to beautiful piece of work be illustrated more effectively, and, further to emphasise this point, the reader may refer between the & follow thedisposition of the various units.

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