15.15 Power Augmentation Flashcards

1
Q

What are power augmentation systems used for?

A

To restore or boost power for improved performance

Without these systems, payload, fuel load, take-off, and climb performance would be affected.

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2
Q

What is a potential drawback of fitting larger engines for increased performance?

A

Increased weight, frontal area, and specific fuel consumption

This would consequently reduce the distance the aircraft could fly.

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3
Q

What factors affect the maximum power output of a gas turbine engine?

A

Density or weight of the airflow, air pressure, air temperature

If air pressure decreases or temperature increases, mass flow through the engine decreases.

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4
Q

List three methods to compensate for power loss in gas turbine engines.

A
  • Increasing the engine speed
  • Increasing the fuel flow
  • Increasing the air density
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5
Q

Why might increasing the engine speed not always be a viable option?

A

Due to mechanical limitations and over speed limits

Especially true for older engines.

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6
Q

How can air density be increased to compensate for power loss?

A

By cooling the air using water sprayed into the engine air intake

This cooling increases air density and decreases air temperature in the combustion chamber.

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7
Q

What is the effect of decreased combustor air inlet temperature?

A

More fuel can be burnt before reaching turbine inlet temperatures

This increases engine power and recovers power loss at low air densities.

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8
Q

Name a system used to augment engine power on turboprop and turboshaft engines.

A

Water methanol system

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9
Q

What is a common application of water injection systems?

A

Used on turbojets

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10
Q

What is the primary use of afterburners?

A

Used on military aircraft and was also used on Concorde

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11
Q

Which method is most suited for engines with centrifugal compressors?

A

Compressor Inlet Injection System

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12
Q

What is the disadvantage of using only water in the Compressor Inlet Injection System?

A

Water can freeze during flight at high altitudes

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13
Q

What is added to the water in the water/methanol mixture to prevent freezing?

A

Methanol

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14
Q

What is the typical mixture strength of water to methanol used?

A

Approximately 60% water to 40% methanol by volume

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15
Q

How does the water/methanol mixture affect compressor inlet air?

A

Reduces temperature, causing air density and thrust to increase

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16
Q

What does the Combustion Chamber Injection System primarily increase?

A

Mass flow through the turbine relative to the compressor

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17
Q

What is the result of reduced pressure and temperature drop across the turbine?

A

Greater pressure within the jet pipe, producing more thrust

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18
Q

What does the reduction in turbine gas temperature permit?

A

More heat to be added, resulting in a greater change of momentum to the gas flow

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19
Q

What does increased rotational speed in the combustion system provide?

A

Further additional thrust

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20
Q

What is the primary purpose of water/methanol injection systems?

A

To increase thrust for takeoff

21
Q

What is the term used for the maximum allowable thrust for takeoff when using water injection?

A

Wet thrust

22
Q

What conditions are required to obtain the wet thrust rating?

A

Predetermined turbine discharge pressure or engine pressure ratio for the prevailing ambient conditions

23
Q

What limitations are associated with the wet thrust rating?

A

Time-limited and altitude limitation

24
Q

Why are water injection systems not commonly used on turbine engines today?

A

Advancement in engine technology

25
Q

How does water injection compensate for reduced thrust on warm days?

A

By lowering the air temperature and increasing air density

26
Q

What component is actuated by the control shaft when the power lever is moved towards maximum power?

A

A microswitch in the fuel control

27
Q

What does the water injection speed reset servo do during water injection?

A

Resets the speed adjustment to a higher value

28
Q

What happens if the water injection system is not armed or if there is no water available?

A

Nothing happens when the water injection switch is switched on

29
Q

What is the role of methanol in water-methanol injection systems?

A

Acts as an antifreeze and contributes to thrust production in the combustion chamber

30
Q

Fill in the blank: Water injection systems are typically not used on _______ engines.

A

high bypass turbofan

31
Q

True or False: Water injection systems can be used at any altitude without limitations.

32
Q

What component increases the set speed during water injection?

A

Speeder spring

33
Q

What is the function of the shuttle valve in the water injection system?

A

Acted upon by water pressure during water injection

34
Q

What does the water injection speed reset servo displace to increase the force of the speeder spring?

A

A lever on the cam-operated lever linkage

35
Q

What is afterburning?

A

A method of augmenting the thrust of an engine to improve takeoff, climb, and combat performance in military aircraft.

36
Q

What are the advantages of afterburning over a larger engine?

A

It does not increase weight, frontal area, or overall fuel consumption.

37
Q

What is the maximum temperature reached by the engine during afterburning?

A

More than 1700 °C.

38
Q

How is fuel introduced in the afterburning process?

A

Fuel is introduced and burned between the engine turbine and exhaust nozzle using unburned oxygen in the exhaust gas.

39
Q

What is the purpose of the afterburning jet pipe’s larger area?

A

To obtain a reduced velocity gas stream.

40
Q

What type of nozzle is fitted to an afterburning jet pipe?

A

Either a two-position or a variable area propelling nozzle.

41
Q

What happens to the nozzle during non-afterburning operation?

A

The nozzle is closed.

42
Q

What prevents an increase in pressure in the jet pipe during afterburning?

A

The nozzle opens to provide an exit area suitable for the increase in the volume of the gas stream.

43
Q

What is the role of the flame stabiliser in afterburner operation?

A

To provide a region for turbulent eddies to assist combustion and reduce gas velocity for flame stabilization.

44
Q

What initiates combustion in the afterburner?

A

An igniter.

45
Q

What is the construction of the burner section in an afterburner?

A

Several circular concentric fuel manifolds supported by struts inside the jet pipe.

46
Q

What materials are used in the construction of the afterburning jet pipe?

A

Heat-resistant nickel alloy.

47
Q

What is the purpose of insulation in the afterburning jet pipe?

A

To prevent the heat of combustion from being transferred to the aircraft structure.

48
Q

Describe the construction of the propelling nozzle in an afterburner.

A

Similar material and construction as the jet pipe, often with two movable eyelids operated by actuators.

49
Q

Fill in the blank: The afterburning process involves the introduction and burning of fuel between the _______ and exhaust nozzle.

A

[engine turbine]