M15.5 Flashcards

1
Q

What is the function of the combustion chamber?

A

To produce a hot stream of gas for the turbines and jet nozzle

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2
Q

What are the main two components of a combustion chamber?

A

The casing and the flame tube

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3
Q

What are the two primary conditions necessary for correct and safe combustion?

A

The correct ratio of fuel and air mixture and the correct air velocity

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4
Q

What is the ratio for a kerosene-air mixture?

A

15:1

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5
Q

What percentage of airflow is used in the primary combustion?

A

20%-30%

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6
Q

Where does the flame stabilise in the combustion chamber?

A

The primary combustion

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7
Q

What is the percentage split of the primary and secondary airflow in the combustion chamber?

A

20-30% in the primary and 70-80% in the secondary

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8
Q

What is the secondary airflow used for?

A

For cooling the combustion chamber inner wall via the dilution zone air holes

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9
Q

What are the three types of combustion chambers on gas turbine engines?

A
  • can-type
  • can-annualar
  • annualar
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10
Q

Why is there interconnection tubes on a multiple-can type combustion chambers?

A

Because only two combustion chambers have igniter plugs and they help equalise pressure between cans

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11
Q

Why is the can-annular combustion chamber better than the multiple can-type combustion chamber?

A

Because its smaller, lighter, and stronger

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12
Q

What is the name for the special small gas turbine engine annular combustion chamber?

A

The reverse flow combustion chamber (airflow direction in the flame tube)

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13
Q

On an annular combustion chamber where are the fuel nozzles and igniter plugs located?

A

The outer wall of the combustion case

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14
Q

What is the rear flange of the inner wall used for?

A

To attach the nozzle guide vanes to the high pressure turbine and to support the flame tube

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15
Q

What is the front of the inner wall flange for?

A

It is the seal surface of the compressor discharge pressure seal

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16
Q

What are the last stator vanes of the high pressure compressor often known as?

A

Exit guide vanes

17
Q

Why is there openings on the outer wall of the combustion chamber?

A

For bleed air from the last compressor stage is fed to the aircrafts pneumatic system

18
Q

Where are the igniter bosses located?

A

Slightly behind the row of fuel nozzles

19
Q

What is the dome section used for?

A

To connect the inner linner with the outer liner and houses the swirl vanes

20
Q

What is the secondary airflow cooling system in the combustion chamber known as?

A

Film cooling

21
Q

What are the two ways of cooling of a combustion chamber?

A

Film cooling and using a thin coating of ceramic