Power plant chapter 3

Question 1

Name the major components in a gas turbine engine?

Answer 1

1.Air inlet
2.compressor section
3.combustion section
4.turbine section
5exhaust section
6.gearbox and accessory section

Question 2

What determines the amount of airflow through a turbine engine?

Answer 2

The forward speed of the aircraft, compressor speed, and air density.

Question 3

Name the two types of compressors commonly used in turbine engines?

Answer 3

Axial and centrifugal flow compressors.

Question 4

Name two different methods for attaching turbine engine rotor blades to the rotor desk?

Answer 4

Dovetail-type root

Bulb-type root

Fir tree-type root

Question 5

What is a split compressor system?

Answer 5

Also called duel or twin spool compressors, these are connected to the turbine section with two rotor shafts, one inside the other.

Question 6

What are the different types of combustion chambers used in turbine engines?

Answer 6

Can,annular,can-annular, and reverse flow annular.

Question 7

What prevents the combustion chambers form burning?

Answer 7

Cooling air along the inside of the liner.

Question 8

What is the purpose of the interconnecting tubes attached between can type combustion chambers?

Answer 8

For flame propagation during start.

Question 9

What functions do axial flow turbine nozzles perform?

Answer 9

They direct the mass airflow to drive the turbine rotor at a specific angle.

Question 10

How is thermal stress relieve on a turbine disc?

Answer 10

By directing bleed air on to the face of the disk, or by grooves been cut in the disk.

Question 11

What are carbon seals used for in turbine engines

Answer 11

They are used as oil seals for the rotor shaft bearings.

Question 12

What is shaft horsepower?

Answer 12

It is an indication of the torque developed by a turboprop or turboshaft engine.

Question 13

What is the purpose of an APU?

Answer 13

They provide ground electrical and pneumatic powered for aircraft systems when the engines are not running. Pneumatic power can be used for engine starting, ground heating or air conditioning, and anti-icing. Many APU’s may also be used as an emergency source of in-flight electrical power.

Question 14

Name the main components of a typical APU?

Answer 14

A small power turbine for power and bleed air, and an electrical generator.

Question 15

When is the greatest demands placed on an APU?

Answer 15

When supplying bleed air.

Question 16

How is an APU generally started?

Answer 16

With its own electrical starter and battery power.

Question 17

Where does an APU get its fuel supply?

Answer 17

From one of the aircraft’s main fuel tanks.

Question 18

At what speed does a gas turbine APU operate and how is this speed maintained?

Answer 18

At or near it’s rated speed regardless of electrical or pneumatic loads imposed. The APU fuel control automatically adjust the fuel flow to maintain beat rated speed.

Question 19

What is used to prevent a heavily loaded APU from the exceeding its maximum EGT?

Answer 19

A load control valve modulates the pneumatic load to maintain EGT’s within limits.

Question 20

How is an APU shut down and why is this procedure used?

Answer 20

After the APU is unloaded by closing the bleed air valve, it is run for specified amount of time to allowed the EGT to cool and stabilize. This cool down period Is typically three minutes. If a heavily loaded APU is abruptly shut down without any cooling down period, Damage could occur as a result of thermal shock.

Question 21

What powers the variable inlet guide vanes used on some APUs to regulate compressor intake airflow?

Answer 21

Fuel pressure.

Question 22

What is fan blade shingling?

Answer 22

It is the overlapping of the mid span shrouds of the fan blade.

Question 23

When a Turbofan or turbojet engine is shut down, what should a mechanic listen for during coastdown.

Answer 23

Any rubbing sound or other unusual noises from the engine.

Question 24

Explain the main difference and advantage of Turbofan over turbojet engines?

Answer 24

A Turbofan engine uses a fan to bypass some air around the engine core and to provide thrust. The advantage is that this provides additional thrust without increasing fuel flow.