Aircraft Anatomy Flashcards

1
Q

Wing- Spar?

A

the main load bearing structural member and provide a lot of strength

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2
Q

Wing - Ribs?

A

What the skin is attached to. They provide the wing cross-sectional shape and transfer loading from the skin to the spars

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3
Q

Wing - stringers?

A

They take bending loads and prevent the skin from buckling.

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4
Q

Skin

A

often made from composite materials such as glass or carbon fibre or some metals.

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5
Q

Spoilers?

A

Spoils lift on upper surface of the wing to provide more weight on wheels - shorter landing distance

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6
Q

Winglets?

A

Reduces air spilling from the lower to upper surface, reducing induced drag

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7
Q

Types of wing anti-icing?

A

Pneumatic, electro-thermal or bleed air operated

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8
Q

Vertical stabilizer?

A

Acts to return the aircraft to its original position following a disturbance in yaw without pilot input.

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9
Q

Horizontal stabiliser?

A

Acts to return the aircraft to its original position following a disturbance in pitch without pilot input.

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10
Q

Two main types of engine?

A

Piston, Gas turbine

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11
Q

Purpose of the propeller?

A

To convert rotational motion of engine to a linear force (thrust).
It does this by accelerating air rearward

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12
Q

Types of fuselage?

A

Truss, monocoque, semi-monocoque

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13
Q

Characterisitcs of truss?

A

Strength comes from frame works

Members on tension and compression

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14
Q

Characteristics of Monocoque?

A

Skin carries structural load, for lighter aircraft

Small dents or stresses can cause complete failure

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15
Q

Characteristics of Semi- Monocoque?

A

Skin fastened to sub-structure
Load shared between structure and skin
Modern method

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16
Q

Why are AC windows small?

A

Aircraft windows are small to maximise the area of the fuselage structure between them which maximises the strength of the airframe. Larger windows could blow out under cabin pressurisation.

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17
Q

What makes up a landing gear?

A

Tires
Brakes
Shock absorbers

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18
Q

Purpose of LDG gear?

A

Support the aircraft on the ground
Absorb loading from landing and braking
Give minimum rolling friction during take-off
For a given strength be light and produce minimum drag

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19
Q

Two LDG gear configs?

A

Tricycle & taildragger

Taildraggers have limited ground visibility

20
Q

Benefits of retractable LDG?

A

Reduced form & interference drag

Used when aerodynamic gains outweigh cost and weight

21
Q

Type of power associated with helicopters?

A

Shaft power

22
Q

What is an airship?

A

A lighter than air aircraft, which can navigate through the air under its own propulsion.

23
Q

What were the historical uses for airships?

A

Transoceanic luxury travel
Freight & mail transportation
Political propaganda
Bombers in WW1

24
Q

Future uses for airships?

A

Freight and logistics
Scenic tourism
Surveillance
Mass transport to remote areas

25
6 Primary aircraft instruments?
``` Attitude Indicator Airspeed Indicator Altitude Indicator (Altimeter) Direction Indicator Vertical Speed Indicator Turn Co-ordinator (Balance) ```
26
Purpose of primary instruments?
Primary instruments are the most safety critical instruments that are used to determine exactly what the aircraft is doing in the air.
27
Types of pressure related to ASI & Alt?
ASI - Dynamic pressure | Alt - Static pressure
28
Secondary instruments?
Engine Temperature and Pressures Engine RPM Fuel gauges Navigation Instruments (VOR/DME/GPS/NDB)
29
Why are engines important?
Engines provide a force that is typically used to provide thrust for for forward motion or direct lift to counter gravity
30
Five engine considerations?
``` Lightweight Small (minimise drag) Powerful (rapid climb) Reliable Repairable ```
31
4 Major types of engines
Piston Engines Gas Turbine Engines Rocket Engines Electric Engines
32
Piston engine configurations?
Radial Inline Inverted Inline Horizontally opposed
33
Radial engines
Large size, more drag Douglas DC3 North-American T-6 Texan
34
Inline Engine
When air-cooled, furthest back cylinder gets too hot | Dehavilland tiger moth, gipsy moth
35
Horizontally opposed engines
Cessna 172 By having the pistons oppose each other, any forces are cancelled out, and the weight is evenly distributed. Having a wider engine with less cylinders on either side means that air cooling is feasible without the drag of radial engines.
36
Rotary engines
Fixed crankshaft & rotating cylinders Gyroscopic forces difficult to control Sopwith Snipe
37
Pros and cons of piston engines
Cheap to buy & maintain Efficient at low alt Hard to get right mix at high alt Needs a prop, limits top speed
38
Wankel engine
Lightweight, compact, reliable, vibrationless, high power to weight ratio inefficient at low rpm due to unburnt fuel Used in light aircraft & UAV
39
Four different gas turbine engines
Turbojet, Turbofan, Turboprop, Turboshaft
40
Turbojet
Fuel inefficient since thrust just comes from exhaust Used for supersonic More efficient at higher alt
41
Turbofans
Engine feeds power back to fan, as well as compressors - fan also provides thrust Low bypass - military jets like F-35 High bypass - like Boeing 787
42
Turboprop
Engine powers a shaft that transforms rotational power to the propeller to create propulsion
43
Turboshaft
Uses a free power turbine to power a shaft
44
Main disadvantage of gas turbine
Cost of purchasing & maintaining | Inefficiency at low alt (relative)
45
Rocket engines
Light compared to other engines | Least efficient, in fuel use
46
Electric engines
Convert electrical to mechanical energy Very efficient Limited by ability to store & obtain electric power