Inlet Flashcards

1
Q

How does air enter engine

A

Via intake

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2
Q

2 parts of an intake

A

Intake nose & inlet duct

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3
Q

What is a divergent

A

Shape when inlet duct gets wider

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4
Q

What does a divergent do

A

Increase static pressure of air moving through the duct

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5
Q

What does intake nose do

A

Smoothens airflow

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6
Q

Why does all air enter the inlet from the front

A

Ram air effect at high speeds

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7
Q

What velocity to the ensure flow through compressor is smooth

A

0.4-0.7 Mach

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8
Q

What is a intake designed to do and how

A

Decelerate flow & convert kinetic energy into pressure energy

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9
Q

How is a subsonic air inlet shaped

A

To deliver air to front of compressor which gives even pressure distribution

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10
Q

What’s the consequences of poor air pressure and velocity

A

Compressor stall

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11
Q

What happens to ram pressure as ram velocity increases

A

Decreases

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12
Q

What happens to air while the aircraft is stationary

A

Air in duct is accelerated to velocity required by compressor

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13
Q

What does a rounded inlet lip do

A

Gives it a thicker radius which reduces risk of separation

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14
Q

At high speed what shape inlet lip do we want

A

Thin

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15
Q

What is a transonic duct practical speed

A

Up to Mach 1.5

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16
Q

What does a transonic duct use to decelerate supersonic airflow

A

Shock diffuser

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17
Q

What happens in a normal shockwave

A

Pressure and temperature increases while velocity decreases to subsonic

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18
Q

What is critical condition

A

Cross section of the inlet is sufficient to allow max airflow requirements of the engine

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19
Q

What is sub critical

A

The shockwave is detached from the lip and moves upstream which reduces Mach number

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20
Q

What is super critical

A

The shockwave is swallowed which makes the airflow in the inlet become supersonic which is unacceptable flow into the compressor

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21
Q

What is diffuser buzz or intake buzz

A

When extreme pressure fluctuations can severely damage the engine

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22
Q

What happens to kinetic energy in a supersonic inlet duct

A

Large amount of it turns into unusable heat

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23
Q

What happens in a oblique shockwave

A

Forced to change direction , the shockwave is inclined at oblique angle which is determined by upstream velocity

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24
Q

Disadvantage of shock diffuser in supersonic duct

A

Abrupt loss of efficient as Mach number increases such as 30% at Mach 2

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25
What does a oblique shock diffuser do
Reduces supersonic flow progressively by wing , in a series of oblique shock waves
26
In a normal duct what will an inefficiency of 1% do
Thrust loss between 1% and 4%
27
Efficiency of pilot design
96-99% efficient
28
Efficiency of wing root design
87-95% efficient
29
Efficiency of side design
80-89% efficient
30
Efficiency of turbo prop annular (Dart)
74-82% efficient
31
In a transonic duct what lip shape do you want
As thin as possible
32
In a variable intake what’s the maximum amount of shockwaves
4 , 3 oblique 1 normal
33
How can we prevent intake buzz
Bleed door
34
How do we cool the engine bay
With Air bled from ramps used for engine bay cooling
35
Problems with snow and ice
Cause turbulent flow which can stall
36
What anti ice system is used
Jet engines have thermal anti - ice systems
37
What are antennas heated with
Warm air
38
What’s the purpose of anti ice valves
Protect against over pressurisation
39
How are anti ice valves operated
Automatically via ice detection system or manually in flight deck
40
What happens to the air used for anti-icing
Ejected over board via small grills
41
What are the 2 methods of ice protection
Bleed air & electrical heating
42
How is the thermal anti ice valve energised
Engine anti-ice switch/ light
43
When does the amber light turn off
When LP sensor duct pressure is more then 5psi
44
Where is duct over pressure signalled to
EICAS/ECAM
45
Why is caution necessary when testing thermal anti Ice system on ground
Air is still hot no personnel should be in the area
46
Where is electrical ice protection employed
Turbo prop engined aircraft
47
Are mats supplied with AC or DC
Both
48
What’s the purpose of the continuously heated element
Prevent formation of ice on leading edge or aircraft engine air intake lip and propeller spinners
49
Where is a intermittently de-icing element located
Behind continuous heated element
50
What type of system is a continuous heated element
Anti - icing
51
What type of system is a intermittent heated element
De -icing
52
In an intermittently heated element why are they divided into separate segments
To ensure ice breaks away easily
53
What happens on the FAST cycle
ON/OFF for 2 minutes OAT between -6 & 10 degrees
54
What is the SLOW cycle
ON/OFF for 6 minutes OAT below -6 degrees
55
Why does the cycling light glow dim and bright
Indicate timer is rotating
56
What is a heated mat examined for
Splits , tears , wrinkling and discolouration which happens due to overheating security of the attachment or general condition
57
Where are anti-corrosion strips placed
Any sign of splitting or corrosion
58
When should you replace a heated mat
any damage which exposes the heated element
59
When does a continuity and resistance check need to be completed
Following any repair to heated mats , resistnace valves must be within limits
60
Why do we need to do insulation resistance checks
To determine any breakdown of insulation between heater mats Insulation resistance to earth must be checked
61
What should