1A

The thrust of a jet engine is directly proportional to the

The compressor shaft rotates on

In a pure jet engine, the rate of pressure rise is greatest at the

A DC started motor disconnects due to

For aircrat design purposes, output of a turbo-shaft engine is measured in

A direct drive turboprop engine

If a helicopter rotor /engine RPM gauge shows split reading, the likely cause is

The centrifugal type compressor produces a compression ratio

A free turbine aircraft engine is most likely to be used on a

A free turbine turbo-prop engine has

A full flow oil system

A directive drive turbo-prop engine

A gas tubine's propulsion force is produced by

A modular constructed gas turbine engine means that

A twin spool engine has

Advantage of flow type fuel system over pressure type fuel system is

An aircraft flying at 800mph would typically use a

An annular combustion chamber consists of

During normal running conditions

Engines having two independent moving systems are

Gas turbines work on the

How are the combustion chambers cooled

How is fuel flow varied in a variable displacement pressure type pump

In a ducted fan engine, the fan is driven by the

In a flow type fuel system, fuel shutoff is done by

In a gas turbine engine, the mass airflow is

In a pure jet engine the rate of pressure rise is greatest at the

In a single spool gas turbine engine thr compressor rev/min is

In a turbine engine used to drive a propeller, the power from the engine is

In a twin spool engine

In the HEIU, the discharge resistors

Normal gas turbine engine starting sequence is

Oil systems consists of

On a gas turbine engine, what is the fan driven by

On a twinrotor fan engine, the high pressure turbine drives

On a twin spool engine, the HP compressor is driven by

One stage of a turbine is

Operation of an engine at a fixed RPM at takeoff (sea-level) causes

Piston engines work on the

Power is adjusted in a gas turbine engine by

Power is adjusted in a variable pitch turboprop aircraft by

Propelling nozzle provide

Reverse thrust can only be selected when the throttle is

Swirl vanes at the inlet of a combustion chamber

The annulus of an axial compressor case is

The basic gas turbine engine cycle is

The bleed valve on a engine at a start up is

The centrifugal compressor produces a compression ratio

The cycle of a gas turbine engine is

The energy remaining in the exhaust or a turbo-shaft engine is

The fan on a turbofan engine is turned by

The fuel flow transmitter is downstrem of

The gas tubine cycle is a

The high bypass duct

The HP compressor is powered by

The inlet of a turbo fan is

The largest pressure change in air passing through an engine occurs in the

The majority of power in a free turbine engine is used to

The majority of the output power from a turbofan is in the form of

The purpose of a high bypass ducted fan engine is to

The purpose of the LP fuel pump is to

Thrust is generated in a turboprop system by

Thrust of a jet turbine engine is directly proportional to the

Turboprop shaft bearings are

What does a 'stage' consist of

What drives the high pressure compressor

What is an engine stage

What is the pressure increase over one stage of a centrifugal compressor

What is unit of measurement of EGT

What percentage of air passing through combustion section is burned

When the air iss blocked in the HP compressor

Which of these statements is true regarding the Brayton cycle