Gasturbine Performance Deel 3
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Questions and Answers

What is a property of a TAPS combustion chamber?

  • Combustion takes place at the stoichiometric ratio.
  • Mixing of fuel and air takes place before atomization. (correct)
  • Through holes in the casing cooling air is supplied.
  • When atomizing the fuel all nozzles are used.

One of the prohibited areas in the fuel metering graph is labelled as 'Stall Area'. In this area the fuel-air ratio increases too much. As a result, the ...

  • air expands too much in the turbine (correct)
  • air ignites too early in the combustion chamber
  • flame is extinguished
  • TIT becomes too high

The principle of propulsion by aircraft gas turbines is the increase of the … of the air.

  • density
  • pressure
  • temperature
  • velocity (correct)

How many times does the piston move up during the thermodynamic cycle of a 4-stroke engine?

<p>2 (B)</p> Signup and view all the answers

Molecules of an ideal gas …

<p>have zero volume (C)</p> Signup and view all the answers

In a petrol engine whose thermodynamics is described by the Otto-cycle, the ignition is:

<p>isochoric (C)</p> Signup and view all the answers

Due to the divergence of a turbofan inlet, the (1) … of the air (2) …

<p>(1) temperature (2) increases (C)</p> Signup and view all the answers

I Enthalpy and total enthalpy have the same value in a gas flow with zero velocity II Temperature and total temperature have the same value in a gas flow with zero velocity

<p>(I) right (II) right (A)</p> Signup and view all the answers

Applying the First Law of Thermodynamics to the combustion chamber means:

<p>Δ𝐻 = 𝑄 (A)</p> Signup and view all the answers

What can be determined in a p-V diagram from the area encircled by the Brayton-cycle?

<p>Specific work (C)</p> Signup and view all the answers

If we consider the losses in the combustion chamber, then the total temperature immediately after the combustion chamber is … when we don’t consider losses.

<p>as high as (A)</p> Signup and view all the answers

(I) When cruise altitude increases the thrust decreases (II) When cruise altitude increases the specific thrust increases

<p>(I) right (II) right (A)</p> Signup and view all the answers

What percentage of the air flows through the core of a turbofan with a BPR of 4?

<p>20% (A)</p> Signup and view all the answers

What type of mounting is shown in the picture?

<p>An axial firtree (B)</p> Signup and view all the answers

In the compressor the absolute velocity in the rotor (1) … and in the stator (2) …

<p>(1) increases (2) decreases (C)</p> Signup and view all the answers

The picture shows a velocity triangle at which (1) … can occur. This is caused by a too (2) … axial velocity.

<p>(1) stall (2) low (D)</p> Signup and view all the answers

The function of the VSVs is to prevent stall in the …

<p>LPC (C)</p> Signup and view all the answers

Not every component of a gas turbine has as many stages. Rank the following components to an (average) increasing number of stages!

<p>radial compressor; turbine; axial compressor (B)</p> Signup and view all the answers

During which phase of flight is Active Clearance Control of interest?

<p>Cruise (B)</p> Signup and view all the answers

What is NOT a function of the air surplus that is fed to the combustion chamber?

<p>To ensure complete combustion of the fuel in the primary (D)</p> Signup and view all the answers

If the RPM increases, and the airflow increases with 10%, the fuel flow increases with …

<p>more than 10% (C)</p> Signup and view all the answers

What component is part of FADEC?

<p>ECU (A)</p> Signup and view all the answers

What is prevented by the use of a drain point?

<p>The build-up of static charge that might cause a spark (D)</p> Signup and view all the answers

If the ambient temperature increases the (1) ... rotates. This (2) ... the fuel flow.

<p>(1) 3D-cam; (2) decreases (A)</p> Signup and view all the answers

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