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Power and Work Formulae in Gas Turbine Engine

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30 Questions

What is the formula for power?

Power = Force × Distance / Time

If an engine requires 500 foot-pounds of work per minute, how much power does it require?

500 foot-pounds per minute

What is the unit of measurement for Power?

Foot-pounds per minute

If a 2500-lb engine is to be hoisted a height of 9 ft in 2 min, how much power is required?

1125 foot-pounds per minute

What is the formula for Work?

Work = Force × Distance

If the force required to hoist an engine is 2500-lbs, and the distance is 9 ft, what is the work done?

22500 foot-pounds

What is the formula for velocity?

Displacement / Time

What is acceleration defined as in physics?

A change in velocity with respect to time

What is the SI unit for acceleration?

Metres per second squared

What is velocity in the context of a gas turbine engine?

The flow velocity of the gas throughout the engine

What is the difference between the velocity of the two aircraft in the diagram?

Their directions are different

Why is velocity a vector quantity?

Because it has magnitude and direction

What is the main concept behind Newton's Third Law of motion?

Action and reaction forces are always equal and opposite in magnitude.

What is the result of accelerating a mass of air backwards in a jet engine?

An equal and opposite force is produced that moves the aircraft forward.

What is the main principle behind Bernoulli's Theorem?

As air velocity increases, pressure decreases.

What is the purpose of a venturi in relation to Bernoulli's Theorem?

To create a narrowing in a tube where air velocity increases and pressure decreases.

What happens to the pressure inside the balloon as it deflates, according to Newton's Third Law?

The pressure inside the balloon decreases, causing an equal and opposite force to react.

How do Newton's three laws of motion relate to each other?

They are inseparable and take place simultaneously.

What is the primary function of the compressor in a turbojet engine?

To compress air before combustion

What is the main advantage of turbojet engines in high-altitude operations?

Enhanced efficiency due to lower air density

What is the purpose of the turbine wheels in a turbojet engine?

To drive the compressor blades

What is the main difference between turbojet and turbofan engines?

Turbofan engines are designed for subsonic cruising speeds

What is the primary purpose of the bypass feature in a turbofan engine?

To allow for higher turbine temperatures

At what speed range is the turbojet or turbofan engine most widely used?

From 450 mph up

What percentage of thrust is produced by the fan in a high bypass fan engine?

Up to 80%

What is the characteristic fan ratio of an ultra-high bypass engine?

9:1 or greater

Which of the following engines is an example of an ultra-high bypass engine?

CFM LEAP

What is a characteristic of a ducted fan engine?

It uses a twin- or triple-spool configuration

What is the advantage of the turbofan engine?

Higher performance and better fuel economy than turbojets and turbo-props

What is the bypass ratio of the P&W 1000G geared fan engine?

12.5:1

Study Notes

Power and Work

  • Power formula: P = F × D / t, where P = Power in foot-pounds per minute, F = Force, D = Distance/Displacement in feet, t = Time in minutes
  • Power can also be related to velocity: P = F × V, where V = Velocity

Velocity

  • Velocity formula: V = D / t, where V = Velocity, D = Displacement, t = Time
  • Velocity is a vector quantity
  • Important in a gas turbine engine, particularly in controlling engine operating temperatures and resultant thrust

Acceleration

  • Defined as a change in velocity with respect to time
  • Typical units: feet per second per second (fps/s), miles per hour per second (mph/s), and meters per second squared (m/s²)

Newton's Third Law

  • "For every action, there is an equal and opposite reaction"
  • Illustrated through the example of a deflating balloon, where the air escaping the balloon creates an equal and opposite force that propels the balloon forward
  • Applies to all forms of jet propulsion, including turbojet engines

Bernoulli's Theorem

  • States that as air velocity increases, pressure decreases, and as velocity decreases, pressure increases
  • Illustrated through the example of a venturi, where air velocity increases as it passes through a narrowing in a tube, resulting in decreased pressure

Turbojet Engine

  • Uses the acceleration of airflow throughout the engine to produce thrust
  • Well-suited for high-speed, high-altitude operations
  • Basic operating principles:
    • Air enters through an inlet duct and is compressed
    • Fuel is added and ignited in the combustor section
    • Heat generated by combustion causes compressed air to expand and flow towards the rear of the engine
    • Air exits the engine at a much higher velocity than the incoming air, producing thrust

Turbofan Engine

  • Developed for subsonic cruising speeds
  • Has become the most popular power plant for commercial and business jets
  • Greater propulsive power at higher subsonic cruising speeds
  • Replaced the turbojet engine due to its higher efficiency

Turbofan/Bypass Engines

  • Consists of a multi-bladed ducted propeller driven by a gas turbine
  • Produces most of its thrust from the fan (up to 80%)
  • Fitted to large commercial jets

Ultra-High Bypass Engine

  • Has a fan ratio of 9:1 or greater
  • Requires a larger fan diameter and a geared fan
  • Examples: CFM LEAP, RR Trent 1000, P&W 1000G geared fan
  • Produces up to 90% of its thrust from the fan

This quiz covers the formulae for power and work in the context of gas turbine engine, including the substitution of work formula into power formula.

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