15.6* Flashcards

1
Q

Where is the highest heat to metal contact in the engine?

A

1st stage HP turbine

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2
Q

What are the different types of turbine blades called?

A

Impulse and impulse reaction

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3
Q

What 3 factors contribute to turbine creep?

A

Time
Temperature
Centrifugal force

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4
Q

How is vibration reduced in LP turbine blades?

A

Use of shrouds

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5
Q

What causes stress rupture cracks in the turbine section?

A

Metal fatigue and corrosion

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6
Q

When does the active clearance control systems operate on engines fitted with hydro mechanical fuel control systems?

A

During climb and cruise

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7
Q

What type of duct does a nozzle guide vane form with adjacent vanes?

A

A convergent (nozzle) duct

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8
Q

What are the methods used to cool NGV’s and HP turbine blades?

A

1st stage of nozzle and blades use convection, impingement and film
2nd stage nozzle uses convection and impingement
2nd stage blades use convection

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9
Q

What method is used to cool the LP turbine blades?

A

LP turbine blades are not normally cooled

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10
Q

What is the most common method of attaching turbine rotor blades?

A

Fir tree root

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11
Q

What advantage does the axial flow turbine have over the radial flow turbine?

A

They can be built with as many stages as required and they allow for very high flow rate

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12
Q

What is the purpose of the turbine?

A

To create torque used to drive the compressor

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13
Q

What is the primary air sources for a passive clearance control system?

A

HPC air for the HPT
Fan air for LPT

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14
Q

On engine shut down what is the contraction sequence of the turbine in the casing?

A

The rotor shrinks faster due to reduction in centrifugal force then the casing shrinks faster due to it’d thinner material

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15
Q

On what stages of a turbine would open turbine blades normally be found?

A

On the HP turbine stages

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16
Q

What is the form of a turbine stage?

A

A stator (nozzle guide vane) followed by the rotor