L13-14 - Turbines Flashcards

1
Q

Why does the area increase in a turbine?

A

Becasue the temp and pressure decrease, so dpes the density, and so to keep flow velocity low the area must increase.

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2
Q

What does a turboine stage consist of?

A

A stage and then a rotor.

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3
Q

What provides power?

A

The change in whirl velocity?

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4
Q

How large is the change in whirl velcity in a turbine compared to a compressor?

A

Much larger.

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5
Q

How hot do combustion gases reach?

A

1750-2000K

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6
Q

What drastically effects the lifespan of turbine blades?

A

Creep, combination of stress and temperature

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7
Q

What are the three types of turbine blades, crytal wise?

A

Equiaxed - roughly even crystal sizes throughout, good mechanical properties in all directions.
Directional solidication - Elongated crystals with great longtiudinal strength.
Single crystal - Excellent mechanical properties and temlerature resistance due to no creep.

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8
Q

What is the Reynolds analogy?

A

Links coeffient of skin friction to heat transfer.

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9
Q

Does laminar or turbulent flow have higher heat transfer?

A

Turbulent flow increases heat transfer. Thefore ideally the gas flow in laminar and the cooling flows are turbulent.

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10
Q

What are the cooling requirements for Nozzle guide vanes?

A

These see higher temps than rotor blades, and lower stress. Will suffer oxidation if not cooled properly.

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11
Q

What are the cooling requirements for rotor blades?

A

Slightly cooler however high stress presenting creep as an issue.

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12
Q

What are the two types of cooling options?

A

Internal cooling

Barrier Cooling

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13
Q

What are the typed of internal cooling?

A

Impingement cooling - Tubes of high pressure air blowing on inside of blade.
Passage cooling - Cool air path inside blade

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14
Q

What is the type of barrier coating most commonly used?

A

Film cooling, blowing cold out out of the blade to create a cooler boundary layer.

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15
Q

What order is the cooling process achieved?

A

Internal cooling followed by film cooling as the coolant cannot extract anymore heat from the blade yet is still cooler than the combustion gases.

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16
Q

What are the negatives of complex cooling?

A

Cost of manufacturing
More high pressure air required by compressor
Film cooling disrupts boundary layers and can increases losses.

17
Q

What percentage of compressor air used for cooling?

A

6-10%