Exhaust Flashcards

1
Q

What is the purpose of an exhaust?

A

Conduct gas flow away from the turbines and clear of the aircraft surface.

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2
Q

What is the purpose of an exhaust in Turbojets, Turboprops and Turboshaft?

A

Turbojet: Produce thrust
Turboprop: Produce some thrust
Turboshaft: Acts as a diffuser

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3
Q

What are the major components in an Exhaust?

A

Exhaust Unit:
- Tail cone
- Exhaust cone
- Exhaust fairing/strut

Exhaust Duct
Exhaust Nozzle

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4
Q

What are exhaust components typically made from?

A

Nickel or titanium due to high temperatures

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5
Q

What are the two ways that the heat from the exhaust is insulated from the aircraft structure

A
  • Passing ventilating air
  • Insulation blanket made up of a core of fibrous material wrapped in a dimpled stainless steel outer skin.
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6
Q

How does the exhaust work on Turboshafts helicopters

A

The nozzle forms a divergent duct to diffuse air
- Does not increase thrust

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7
Q

What are the two types of Turbofan exhausts?

A

Ducted and Unducted

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8
Q

How does a ducted turbofan exhaust work?

A

Takes fan airflow and directs it to a common exhaust where the core flow and fan flow mix

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9
Q

How does an unducted turbofan exhaust work?

A

Has two separate nozzles (one for core, one for fan).
- Both flow to ambient air through separate nozzles.
- Handles high amounts of airflow
- Converging nozzle exhaust produces 15-20% thrust

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10
Q

In a turboprop, what is another word for exhaust duct?

A

Tailpipe

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11
Q

What does a turboprop tailcone and struts do to the airflow?

A

Imparts an axial flow onto the air, straightening it.

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12
Q

What percentage of thrust is produced from a turboprop exhaust?

A

10-15%

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13
Q

On a turboprop, is the fwd section of the tailpipe connected to the exhaust?

A

No
- Fwd section is funnel shaped and surrounds the exhaust but DOES NOT CONTACT (Annular gap).

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14
Q

Where is the rear section of the exhaust connected to on Turboprops?

A

Connected to the airframe by two support arms, one on each side.
- Support arms are connected to the wing in a way to compensate for heat expansion.

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15
Q

What is the insulating blanked on a turboprop tailpipe made of?

A

Stainless steel on the outside and fiberglass on the inside
- Used when the exhaust is located some distance from an aircraft structure.

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16
Q

What is Turbine Discharge Pressure?

A

Total pressure discharge in an LP turbine in a dual spool axial engine

17
Q

Where is the Turbine Discharge Pressure measured from in the exhaust?

A

Immediately aft of the turbine and fwd of the exhaust flange
- Pressure probes inserted.

18
Q

In large engines where its not practical to measure temperature at the turbine inlet, where is temperature measured?

A

EGT is measured on the turbine outlet

19
Q

What is the purpose of an Exhaust Cone (tailcone)

A

Form a divergent duct to reduce the velocity to Mach 0.5 and increase the pressure.

20
Q

What is the purpose of an Exhaust Duct?

A

The convergent duct is used to accelerate the gas to Mach 1 (Chocked Nozzle)
- Usually fixed geometry on subsonic aircraft

21
Q

When is a Convergent-Divergent (C-D) Nozzle used?

A

To help produce thrust when the exhaust velocity is higher than Mach 1.
- Best suited for supersonic aircraft due to higher pressure ratios in exhaust.

22
Q

What is the use of an afterburner limited by?

A

Fuel consumption

23
Q

What are some additional components that are needed to make an afterburner?

A
  • Flame stabilizer
  • Flame holder
  • Fuel manifold
  • Igniters
  • VARIABLE AREA EXHAUST NOZZLE
24
Q

When energy and mass are added to fuel an afterburner, what must the exhaust nozzle do?

A

Widen to allow more fuel

25
Q

In a low bypass turbofan, what is the purpose of the fan air in an afterburner?

A

Provides more oxygen to the exhaust for burning.

26
Q

How is heat managed in an afterburner exhaust?

A

Using a special liner around the nozzle that is cooled with air
- Operates like a Single Can Combustion Chamber

27
Q

What is the purpose of Thrust Vectoring?

A

Directs thrust other than parallel to the longitudinal axis of the plane
- Used to change direction of the aircraft or VTOL
- Up to 20 degrees maneuverability

28
Q

How can Thrust Reversers be actuated?

A

Pneumatically or Hydraulically

29
Q

When are thrust reversers used?

A

On larger aircraft when braking cannot stop the aircraft alone

30
Q

What is the typical thrust production of a thrust reverser?

A

40-50% rearwards thrust

31
Q

What is the Braking force percentage of thrust reversers in normal runway conditions and icy/wet runway conditions?

A
  • 20% in normal conditions
  • 50% in wet or icy runways
32
Q

What are the two main types of thrust reversers?

A
  • Mechanical blockage (clamshell or inverted cone) - Ducted turbofan
  • Aerodynamic blockage (Cascades and blocker doors) - Modern
33
Q

What are the requirements when designing a thrust reverser?

A
  • Light
  • Strong
  • Handle high temperatures
  • Fail safe
34
Q
A