Fundementals Flashcards

(51 cards)

1
Q

What is acceleration due to gravity

A

9.8 m/s2

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2
Q

Force formula

A

Mass x acceleration

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3
Q

Weight formula

A

Mass x acceleration due to gravity

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4
Q

Newton conversion

A

Kg x m/s2

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5
Q

GTE Working cycle

A
  1. Induction
  2. Compression
  3. Combustion
  4. Exhaust
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6
Q

Work done formula

A

Force x distance

SI Unit = Joules

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7
Q

Power formula

A

Work / Time

SI Unit = Watts

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8
Q

What are the 2 types of mechanical energy

A

Potential and kinetic

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9
Q

What is potential energy

A

Energy a body has due to a virtue of position

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10
Q

What is kinetic energy

A

Energy a body has by virtue of motion

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11
Q

Newtons first law

A

Law of inertia

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12
Q

Newton’s second law

A

Acceleration produced in a mass by a force acting on it directly proportional to the force and inversely proportional to the mass

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13
Q

Newton’s third law

A

Every action has an opposite and equal reaction

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14
Q

What is the brayton cycle

A

Working cycle of GTE

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15
Q

What is a piston engine peak pressure

A

Excess of 1000psi

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16
Q

Within the Brayton cycle what increases

A

Velocity of air & Pressure energy

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17
Q

What happens during combustion in regards to volume and pressure

A

Pressure of air doesn’t rise during combustion however volume does

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18
Q

What is isobaric heating

A

Heating at constant pressure

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19
Q

What’s the difference between piston engine and GTE working cycle

A

Piston is intermittent whereas GTE is continuously

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20
Q

How is energy converted back to kinetic energy

A

High velocity jet efflux

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21
Q

What’s the function of aircraft engines

A

Creates necessary movement on aircraft which is thrust

Supplies hydraulic power , electric power , bleed air for pneumatic system

22
Q

2 types of engines

A

Piston engine and Gas Turbine

23
Q

Advantage of piston aircraft

A

More efficient

24
Q

Disadvantages of piston aircraft

A

Performance decreases as altitude increases

Too large for aircraft as ratio of weight to power decreases

25
What is Jet Propulsion
Force to move aircraft forward
26
How does a reaction engine work
Use newtons law of motion
27
What’s needed to accelerate air
Pressure needs to be increased
28
What are the 4 types of Gas Turbine
1. Turbojet 2. Turbofan 3. Turboprop 4. Auxiliary Power Unit
29
What is bypass ratio
Air coming into fan duct vs air into core
30
How can you identify a turbojet engine
No fan in front of
31
How can you identify a Turbofan aircraft
Fan in front
32
How can you identify a Turboprop aircraft
Propeller in front of
33
When is a turbojet engine used
High speed aircraft
34
Disadvantage with turbojet engine
Very loud and inefficient
35
What is turbofan engine a combination with of
Combines advantages of turbojet & turboprop
36
Turbofan engine is what kind of engine
Twin or triple spool
37
What is total thrust in turbofan engines
Thrust developed by core engine + Fan
38
Advantage and disadvantage of turboprop engines
Efficient but not at high speeds
39
In a turbofan how much thrust does the fan produce
More then 80% of total thrust
40
Turbofan bypass ratio
Between 4:1 & 9:1
41
Aircraft engine bypass ratio
90:1
42
Advantage of aircraft engine in terms of fuel
Use 20% less fuel then high bypass engines
43
2 types of engine construction
Modular and non-modular
44
What is modular construction
Engine can be separated into sub major modules
45
What is non-modular construction
Weight saving construction but complicated to repair and difficult to access parts
46
What’s aluminium alloy used for
Low loaded parts of fan module such as gearbox housing & fan stator castings
47
Where is ceramic alloy used
Heat and corrosion protection such as combustor and HP turbine
48
Where is steel alloy used
N1 drive shaft Engine bearings Main structural frames on engines Intermediate case & turbine exhaust
49
Where is cobalt alloy used
High heat resistance when stator in first stage of high pressure turbine
50
Where is Titanium alloy used
High centrifugal force areas such as LP compressor & front stage of HP compressor
51
Where is nickel base alloy used
High centrifugal loads at high temperatures HP Compressor & combustion section for high and low pressure turbines