Principles of Gas Turbine/Recip Operations
Gas Turbine/Reciprocating Engine Types
Hydraulic/ Electrical Systems
Fuel Systems/Lubricating Systems
Accessory/Start/MISC
100

This cycle consists of four events occuring simultaneously; intake, compression, combustion, and exhaust.

What is the Brayton Cycle
100

A simple engine best suited for high speed/high altitude flights. Example include to F-4.

What is a turbojet

100

Pressure change at any point in a confined incompressible fluid is transmitted throughout the fluid such that the same change occurs everywhere

What is Pascals law.

100

Thin film of lubricant that prevents metal to metal contact.

What is a squeeze film.

100

Two methods of accessories for gas turbine engines.

What are air or mechanically driven accessories. 
200

An opening that increase airflows velocity and decreases airflows pressure.

What is a Nozzle

200

Airflow that goes around a gas generator

What is Bypassed/Ducted air

200

Requires less current due to higher voltage and a ground neutral system.

What is AC power. 

200

Fuel commonly used aboard ships due to its high flash point and low volatility.

What is JP-5.

200

Most common type of starter used on small gas turbine engines.

What is a DC electric motor.

300

The increase in air pressure that occurs when an aircraft is moving through the air

What is RAM effect

300

Engine where the propelled provides the majority of the thrust and impacts a small amount of acceleration to a large mass of air.

What is a turboprop engine. 

300

Electromagnetic device that transforms direct current into alternating current.

What is an inverter. 

300

 The lowest temperature a combustible substance can ignite with a momentary application of a flame.

What is a flash point. 
300

Occurs when a compressor RPM stabilizes below normal and turbine temperature remains within limits.

What is a false start.

400

Indicator used by aircraft that rely on the propulsive power of exhaust from tubrojets/fans.

What is the Engine Pressure Ratio Gauge (EPR)

400

Major components of the propeller assembly.

What are the blades, hub, pitch change/dome assembly. 

400

 Routes power to equipment devoted to the aircrafts intended mission.

What is a primary bus.

400

 Thrust produced at the maximum continuous turbine temperature with a time limit.

What is the military rated thrust (MRT)

400

Term for when the engine is producing enough power to continue engine acceleration itself.

What is the self-accelerating speed. 

500

From the inlet to the burner this characteristic increases drastically before dropping and returning to 0 at the exhaust stage.

What is pressure.

500

Two ranges of operations of a turboprop engine (and what they mean).

Alpha (flight range), Beta (Ground operations)

500

Components of a hydraulic system. 

Reservoir, pump, check valve, pressure regulator, pressure relief valve, accumulator, pressure gauge, selector valve, hydraulic fuse, actuating cylinders, bypass filter.

500

Directs the flow of return oil into the fuel-oil heat exchanger to allow cooling to occur.

What is the oil temperature regulating valve. 
500

Three bleed systems of a dual-axial compressor engine.

What are the high pressure, low pressure, and inter-stage bleed air.