Power Points Flashcards

1
Q

Purpose of thrust reversals

A

Increase aircraft stopping power with a significant increase In weight

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2
Q

Benefits of thrust reversals

A
  • Aid in braking and directional control during landing
  • Back aircraft out of parking spots
  • aid in emergency landing and takeoffs
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3
Q

4 methods if thrust reversal

A
  • hot jet
  • cold jet
  • hot and cold jet
  • revrse pitch propellers
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4
Q

2 types of operation thrust reversals

A

Mechanical
- clamshell
Areofynamic
- cascade vanes

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5
Q

Thrust reversals safe guards

A
  • can’t be selected until throttle at idle
  • not normally selected until weight on wheels is activated
  • engine power can’t be increased until thrust reversals are fully deployed
  • automatically return to idle if forward thrust is selected while TR are deployed
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6
Q

3 purposes of drive train system

A

Reduce speed
Increase torque
Provide drive for accessories

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7
Q

Components mounted on accessory gearbox

A
  • starter motor
  • fuel pump
  • FCU
  • oil pump
  • generator
  • Tachometer generator
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8
Q

Function of accessory gearbox

A

Provide mounting face and a means of drive for those components essential to start, sustain, monitor

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9
Q

Turbojet noise supressors

A

Corrugated

Lobe type nozzle

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10
Q

How do turbo jet noise reduction nozzles work

A

Changes the jet pattern reducing noise level

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11
Q

Modular alignment methods

A
  • spline drive
  • serrated drive
  • keys and keyway
  • off set bolt holes
  • dowels
  • witness marks
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12
Q

3 reasons for post maintenance activites

A

Prevent corrosion
Control deterioration
Eliminate physical damage

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13
Q

Oil pressure system components

A
Tank
Pump
Filter
Relief valve
Oil jets
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14
Q

Oil scavenge components

A
Strainer
Scavage pump
Oil cooler
Tank
Centrifugal breather
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15
Q

Low pressure air uses [5]

A

Customer services
Cooling HP compressor
Cooling and pressurisation of bearings
Cooling accessories

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16
Q

3 effects from icing

A

Decreased performance
FOD
Compressor surging/stalling

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17
Q

3 methods of ice prevention

A

Hot air
Electric heating
Hot oil

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18
Q

4 engine starting systems

A

Motor
Fuel sys
Ignition sys
Control sys

19
Q

5 types of starters

A
Electric 
Air turbine
Air impingement 
Gast turbine starter
Cartridge type
20
Q

Fire prevention methods [5]

A
Fire zones
Fire resistant materials
Explosion proof electrical equipment 
Drainage for leaks
External cooling and vents
21
Q

Fire extinguishing components

A
Discharge handle/buttons
Fire bottles 
Explosive cartridges 
Discharge nozzles 
Discharge indicators
22
Q

Fire discharge indicators

A

Electronic indicators
Skin panel indication (disks)
Mist smell
Indicators pins

23
Q

What cascade vanes do

A

Redirect escaping exhaust gasses forward

24
Q

Fuel flow measured in

25
Braking force of thrust reverses
Proved 20% braking force under normal conditions
26
How Turbo fans dampen noise
Insulating blankets/ absorbing material
27
Define ram effect
Result of forward movement which cuases a pile up of air in the inlet. This increases the pressure therefore increases thrust
28
Second operation of air inlet
Provide uniform supply of air to the compressor
29
Shape of subsonic inlets and why
Divergent. Increase pressure and slow down velocity
30
Inlet FOD protection
Inlet screens Vortex dissipator Partical seperators (helicotpers)
31
Engine monitoring things
- EPR - Compressor and turbine speeds (RPM) - Torquemeter - turbine discharge pressure - EGT
32
EPR indicates...
Indicates the amount of thrust the engine produces
33
Turbine discharge pressure gage indicates..
Amount of pressure aft of last turbine stage
34
Torque meter indicates
Amount of torque produced to drive prop or rotor
35
EGT indicates
Temp at turbine section
36
2 types of compressor cleaning
Fluid | Abrasive grit
37
Compressor bleed air HP (jeppeson)
Cabin pressurisation, anti icing, pneumatic engine starting.
38
Compressor stall caused by
Imbalance between inlet velocity and compressor rotational speed. When compressor blade AoA exceeds critical AoA
39
Compressor mid band shrouds purpose
To make them more resistant to bending forces created by airstream
40
Adv of centrifugal compressor
``` Simplicity Low cost Low weight Low starting power requirements Good operating efficiency ```
41
Dis adv of axial flow compressors
``` High weight High starting power Low pressure rise per stage Expensive Difficult to manufacture ```
42
Combustion section elements:
Combustion chamber Fuel injection sys Ignition sys Fuel drainage sys
43
Purpose of swirl vanes
To slow air down so the flame can propagate properly. Fast airflow cuases flame outd
44
Disadvantage of tailpipe
Reduces efficiency due to heat and duct friction losses