M15.1 Fundamentals Flashcards

1
Q

What is energy typically defined as?

A

Something that gives us the capacity to perform work.

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2
Q

How are work and energy measured?

A

In joules.

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3
Q

What are the two types of energy?

A
  • Potential
  • Kinetic
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4
Q

Define potential energy.

A

Energy at rest or energy that is stored.

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5
Q

Define kinetic energy.

A

Energy in motion.

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6
Q

What is Newton’s First Law of Motion also known as?

A

The law of inertia.

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7
Q

What does Newton’s Second Law of Motion express?

A

The interplay between force and motion.

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8
Q

What is the formula for Newton’s Second Law?

A

Force = Mass x Acceleration.

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9
Q

What is Newton’s Third Law of Motion also referred to as?

A

The law of action and reaction.

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10
Q

What does the Brayton cycle describe?

A

The thermodynamic cycle of a gas turbine engine that produces thrust.

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11
Q

What are the four stages of the Brayton cycle?

A
  • Intake (suck)
  • Compression (squeeze)
  • Expansion (bang)
  • Exhaust (blow)
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12
Q

What happens during the intake stage of the Brayton cycle?

A

Air enters at ambient pressure and at a constant volume.

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13
Q

What is isobaric heating in the Brayton cycle?

A

Heat is added to the air in the combustion chamber at constant pressure.

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14
Q

What are the four ideal changes of state?

A
  • Isobaric
  • Isochoric
  • Isothermal
  • Isentropic
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15
Q

Which changes of state are important for aircraft gas turbine engines?

A
  • Isobaric
  • Isentropic
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16
Q

What does force represent?

A

The intensity of a thrust or input.

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17
Q

What is the unit for force in the metric system?

A

Newtons (N).

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18
Q

What is work defined as?

A

When a force is moved through a distance, in the direction of the force.

19
Q

What are the two factors involved in calculating work?

A
  • Force
  • Movement through a distance
20
Q

What is the SI unit of work?

A

Joule (J).

21
Q

What does power involve in relation to work?

A

The rate of doing work over time.

22
Q

What is the SI unit of power?

23
Q

Define motion.

A

A continuing change of position or place.

24
Q

What is the difference between speed and velocity?

A

Speed does not include direction; velocity includes both speed and direction.

25
Q

What is acceleration defined as?

A

The rate of change of velocity.

26
Q

What are the two main types of aircraft engines?

A
  • Piston type engines
  • Gas turbine engines
27
Q

What is a key advantage of gas turbine engines over piston engines?

A

Can operate at very high altitudes.

28
Q

What type of engine produces thrust in aircraft?

A

Gas turbine engines.

29
Q

What are the types of gas turbine engines used on aircraft?

A
  • Turbojet engines
  • Turbofan engines
  • Turboprop engines
  • Turboshaft engines
30
Q

What is a significant disadvantage of turbojet engines?

A

High fuel consumption.

31
Q

What is the primary function of turbofan engines?

A

Produce thrust with better efficiency than turbojets.

32
Q

What is the advantage of turboprop engines?

A

Very fuel efficient at mid-range speeds.

33
Q

What is a turboshaft engine primarily used for?

A

To drive machinery instead of producing thrust.

34
Q

What are the main sections of a gas turbine engine?

A
  • Air inlet
  • Compressor section
  • Combustion section
  • Turbine section
  • Exhaust section
  • Accessory section
35
Q

What does the ‘cold section’ of a gas turbine engine refer to?

A

Parts from the inlets up through the compressors.

36
Q

What does the ‘hot section’ of a gas turbine engine refer to?

A

Areas past the compressors from the combustion chambers through the exhaust.

37
Q

What are the main sections of a turbine engine?

A

Combustion section, Turbine section, Exhaust section, Accessory section

The sections include the diffuser, combustor, Low-pressure Turbine (LPT), High-pressure Turbine (HPT), Turbine Exhaust Case (TEC), and main gearbox.

38
Q

What does the ‘cold section’ of a turbine engine refer to?

A

Parts of the engine from the inlets up through the compressors and/or diffusers

This section includes components that operate at lower temperatures compared to the hot section.

39
Q

What does the ‘hot section’ of a turbine engine refer to?

A

Areas past the compressors from the combustion chambers through the exhaust

This section involves components that operate at high temperatures.

40
Q

List the advantages of modular engine construction for the engine manufacturer.

A
  • The rotating module parts can be pre-balanced
  • Fewer spare engines are needed in stock
  • More flexibility when changes are made to individual engine parts
  • Main engine modules can be easily stored and transported

These advantages contribute to efficiency in manufacturing and inventory management.

41
Q

List the advantages of modular engine construction for the engine operator.

A
  • Modules can be removed and replaced with minimum disturbance to other nearby engine parts
  • No re-balancing is required after a module change
  • Most modules can be replaced while the engine remains on the aircraft
  • Less need for spare parts and modules can be easily transported

These benefits enhance maintenance efficiency and reduce downtime.

42
Q

What is a further advantage of the modular design in terms of repairs?

A

Replacement of a module is often considered a minor repair and not a shop repair

This allows maintenance to be performed by a maintenance organization rather than requiring an engine overhaul organization.

43
Q

What is the main design aim for engine materials?

A

Materials must be strong enough for their tasks, as light and cheap as possible

This balance is crucial for performance and cost-effectiveness in engine design.

44
Q

What are typical materials used in modern jet engines?

A
  • Aluminium alloy
  • Ceramic material
  • Composite material
  • Cobalt base alloy
  • Nickel base alloy
  • Corrosion resistant steel alloy
  • Titanium base alloy

These materials are selected for their specific properties suitable for high-performance engine components.