Engines Flashcards

1
Q

Bernoulli theorem

A

Total energy made of 3 forms (potential, pressure/temp and kinetic)

Pressure and kinetic energy proportional

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2
Q

Piston engine process

A

Induction, compression, combustion (expansion) and exhaust

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3
Q

What is the compression ratio

A

Ratio to BDC and TDC (total vol / clearance vol)

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4
Q

Different colour smoke meaning

A

Blue = oil burn in cylinders
Black = carbon granules
White = water content

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5
Q

What does a supercharger do

A

Delivers more air to the engine cylinder, meaning more fuel, meaning a greater power output

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6
Q

Advantages of propellers

A

-Extra wing lift due to prop
-slip stream suppresses stall speed (good low speed characteristics)
-slipstream makes fin/rudder more effective

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7
Q

Disadvantages of propeller

A

Lack of airspeed and range due to limited revolution speed to ensure blade doesn’t become sonic

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8
Q

What decides the prop force

A

Output of engine and blade angle

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9
Q

3 restrictions on propellers

A
  1. Blade length
  2. Chord size (aspect ratio, centrifugal turning moments)
  3. blade interference (too many)
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10
Q

Why do blades have washout (twisted)

A

To maintain blade AoA and prevent it becoming sonic

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11
Q

Three reasons for critical engines

A

Asymmetric blade affect due to downgoing blade travelling faster

C of G position and blade distance greater on one engine

Slip stream of props

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12
Q

What is specific fuel consumption

A

Fuel used per hour / thrust of engine

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13
Q

Combustion cycle of jet engine

A

Induction, compression, combustion, expansion, exhaust

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14
Q

Why were jet engines introduced

A

-to fly at higher speeds
-more simplistic and reliable

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15
Q

Describe the process of a gas turbine

A

-air enters and compressed
-ignited in combustion chamber to form more energy
-expansion and passes across turbine
-exhausted through nozzle

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16
Q

Advantages of fuel injection

A

No vaporisation, uniform delivery, improved fuel/air ratio and instant engine response

17
Q

Compression ratio for gas turbine

A

Change in air pressure between inlet and outlet power of a compressor or system

18
Q

3 benefits of a bypass engine

A

-greater propulsive efficiency
-greater SFC
-less noise

19
Q

5 Advantages of a fan engine

A

-Smaller engine size
-better propulsive efficiency
-better SFC
-reduction in engine noise
-contamination effects reduced

20
Q

Why flat rate a fan engine

A

Give it a wide range of operation to keep it within mechanical limits

21
Q

EPR

A

Ratio of air pressure measurements

22
Q

Wet start

A

Failure to start after fuel delivery due to ignition problems

23
Q

Hung start

A

Ignition occurs but fails to reach self sustaining rpm (no starter motor)

24
Q

Hot start

A

Ignition and reaches self sustaining rpm but unstable combustion

25
Q

Surge

A

Reversal of air through the engine