Exam 1 Flashcards

0
Q

Needs necessary for engines for modern military applications such as multi role aircraft

A

Drag of the engine
High specific thrust
Short takeoff and vertical landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
1
Q

What are the advantages of turbine engines over rockets, ramjets, and pulse jets?

A
  • can operate without forward momentum

* do not need to carry an oxidizer

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

How can missile firing and operating the aircraft at high angles of attack effect the engine

A

Can stall the compressor blades

Surge

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What percent of the fuel burned in the combustion section of a turbine engine is used to drive the compressor?

A

66%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Disadvantage of interstage bleeds vs the advantage of variable stators during turbine engine part speed operation

A

When using the bleeds energy is wasted through the work done to compressor air, air that is not used for combustion

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Advantages of using a multiple chamber combustor system

A
  • reduces time to maintain combustor
  • can accommodate larger combustors for better emissions
  • testing during development is simpler using only one chamber
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Regarding military engines and being able to cope with missile plume ingestion, what are some conditions that might cause extinction of hue flame in the combustor?

A
  • momentary increase in inlet mass flow and temp

* secondary effect of depletion of oxygen

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What is the main purpose of the rotating turbine blades?

A

Drive the compressor
Accessory gearbox
Power the prop/rotor blades/fan

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What are the consequences with new technology that allows for turbine blades to withstand more heat

A
High temps in turbines
Less cooling air
Smaller compressor
High % of fuel used for thrust
Lower TSFC
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What is the purpose of using bleed air on the turbine case?

A

Cooling turbine blades

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What tool is used in access ports in turbine engine casings that support health monitoring

A

Borescopes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What engine indicating probes are typically found in exhaust ducts

A

Thermocouples (EGT)

Pressure ratio probes (EPR)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Why are thrust reverses not typically used below 50 knots

A

Foreign object damage

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

What are the circumstances for which a pilot could accidentally over temp an engine during reverse thrust

A

On a non computer controlled engine

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

How does burning fuel in the afterburner increase thrust

A

Increase thrust by adding fuel to the exhaust gasses and igniting it

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What greatly affects operational noise levels of an aircraft

A

Engine design and airframe

16
Q

Emissions produced from a gas turbine engine are a direct result of what

A

The combustion process

17
Q

Why is the starter typically the basis design with regards to the accessory drive system

A

Starter often provides the highest torque that the drive system encounters

18
Q

What type of forces can ball bearings withstand

A

Radial and axial forces

19
Q

How does a labyrinth seal work?

A

Seal creates a resistance to airflow by forcing the air to transverse through a series of fins

20
Q

What is the correlation between the FMU and VIGVs

A

The FMU is a servo pressure source for a remote actuator to operate the VIGVs of the HP compressor

21
Q

How does fuel within the wing tanks rarely go below -35 degrees Celsius

A

Heating of he wing structure caused by the aircraft speed

22
Q

What is the function of a FOHE

A

Extract heat from the engine oil providing oil cooling and fuel heating

23
Q

Why is it that turboprops have spa separate oil reservoir that cannot be depleted by leakage from the basic oil system

A

So that the propellor pitch can be feathered if the engine has to be shut down inflight after loss of oil

24
Q

What is he correlation between FADEC and EEC

A

At the center of the FADEC is he EEC

25
Q

What does the FMU do with unwanted fuel and what are the consequences

A

Cycles it back through causing he fuel to heat up