P Gas Turbine Principles Flashcards

1
Q

What is the equation for thrust?

A

Thrust = Mass x Velocity

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2
Q

What is the equation for total thrust?

A

Total = Fan + Core

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3
Q

What is the Brayton cycle?

A
  • Intake
  • Compression
  • Combustion
  • Exhaust
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4
Q

What are the names of the 5 engine modules?

A
  1. Intake
  2. Compressor
  3. Combustor
  4. Turbine
  5. Exhaust
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5
Q

What is the relationship between thrust and TAS?

A

As TAS increases:

  • Thrust lost due to momentum drag increases
  • Thrust gained from ram effect increases

Overall thrust is fairly constant with TAS

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6
Q

Which 3 factors effect thrust?

A
  • Altitude
  • Speed
  • Ambient temperature
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7
Q

What ambient conditions provide the worst thrust?

A

Hot and humid due to less dense air

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8
Q

What happens above M0.4?

A

Engine benefits from ram effect increasing thrust

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9
Q

How does engine bleed effect thrust?

A

Reduces - takes mass flow from just before the combustor and reduces thrust

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10
Q

How does intake heating reduce thrust?

A

Reduces the air density and therefore the mass flow of air

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11
Q

Where is maximum thrust produced?

A

On the ground

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12
Q

What is thermal efficiency?

A

Describes the efficiency with which fuel is converted into kinetic energy - determined by combustion temperature and pressure ratio

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13
Q

Reassure ratio calculated?

A

The difference in pressure between input pressure (P1) and compressor outlet pressure (P3)

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14
Q

What is propulsive efficiency?

A

Efficiency with which kinetic energy is translated into propulsive force

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15
Q

How does a FADEC determine thrust?

A
  • Compares intake pressure an exhaust outlet pressure
    Or
  • Uses N1, which is the speed of the fan displayed as a percentage
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