S Aircraft Construction Flashcards

1
Q

3 main aircraft sub assemblies

A

Fuselage
Wings
Empennage

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2
Q

5 attachment methods?

A
  1. Riveting
  2. Welding
  3. Bolting
  4. Pinning
  5. Adhesives
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3
Q

What is the name of a joint which connects 2 panels together using rivets?

A

Doubler joint

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4
Q

What is a method of ensuring bolts do not come loose?

A

Wire locking

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5
Q

Can composite materials be riveted?

A

No

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6
Q

How do we attach composite materials?

A

Composite fastener

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7
Q

What isa longeron?

A

Main longitudinal load bearing member of the fuselage

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8
Q

What are stringers?

A

Run longitudinally, bonded to the skin, help withstand buckling

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9
Q

What are formers/frames?

A

Define the shape and provide skin attachment points

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10
Q

What doos the aircraft skin do?

A

Provides aerodynamic shape as well as withstanding tension and compression stresses

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11
Q

What is a bulkhead?

A

Provide structural partitions inside the fuselage and give structural support

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12
Q

What is a firewall?

A

Fire resistant bulkhead installed between engine compartment and the rest of the airframe structure

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13
Q

What are intercostels?

A

When weaker areas around the windows and doors are reinforced with frames and stringers

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14
Q

What is a machined structure?

A

A single piece of material effectively carved with components included in its shape, removing the need for joints

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15
Q

Why are most fuselage sections circular?

A

Eliminating corners helps ensure laminar flow

Circular cross section can more easily withstand loads imposed by pressurisation

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16
Q

What is a double bubble structure?

A

Intersecting circles tied together by the fuselage floor

17
Q

What shape are unpressurised aircraft?

A

Don’t have to be circular, can vary more widely

18
Q

3 advantages of an oval fuselage?

A
  • Lower manufacturing cost
  • Greater capacity
  • Better options for cargo
19
Q

Where is the pressure hull located?

A

Between the forward and rear pressure bulkheads

20
Q

What is the pressure bulkhead pressurised to?

A

Between 8 and 9psi

21
Q

What is axial stress?

A

Stress acting along the longitudinal axis

22
Q

What is hoop stress?

A

Stress that acts radially across the fuselage structure

23
Q

When do axial and hoop stresses occur?

A

Cyclic stresses - every time the cabin is pressurised

24
Q

What are 3 types of wing design?

A

Cantilever
Semi-cantilever
Externally braced

25
Q

What are the 2 types of wing?

A
  • Low wing

- High wing

26
Q

What is the key disadvantage of a high wing?

A

Reduced visibility into the turns when banking

27
Q

Where does a spar run from?

A

Root to tip

28
Q

Where do ribs run from?

A

Leading edge to trailing edge

29
Q

What do stringers do?

A

Combine with ribs to share loads and transfer loads to spars

30
Q

What is the centre wing box?

A

Part of the fuselage which provides the attachment points for the wings

31
Q

What is the wing box?

A

Main structural component of the wing

32
Q

What does the wing box house?

A

Mounting points to support hinge points and actuators for control surfaces

33
Q

How is the vertical stabiliser attached to the aircraft?

A

3 or 4 lugs and pins

34
Q

What can cause catastrophic vertical stabiliser failure?

A

Excessive application/deflection of the rudder

35
Q

The advantage and disadvantage of a T tail?

A
  • Predictable flight characteristics

- Prone to deep stall

36
Q

What does the pylon do?

A

Attaches the engine to the wing

37
Q

How are weight/thrust forces carried?

A

Strut braces

38
Q

What is a fuse pin?

A

A bolt designed to break at a given load

39
Q

Why are fuse pins used for the engine pylon?

A

Allow the engine to separate without causing excess damage to the wing