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
What are the 2 types of wing?
- Low wing | - High wing
26
What is the key disadvantage of a high wing?
Reduced visibility into the turns when banking
27
Where does a spar run from?
Root to tip
28
Where do ribs run from?
Leading edge to trailing edge
29
What do stringers do?
Combine with ribs to share loads and transfer loads to spars
30
What is the centre wing box?
Part of the fuselage which provides the attachment points for the wings
31
What is the wing box?
Main structural component of the wing
32
What does the wing box house?
Mounting points to support hinge points and actuators for control surfaces
33
How is the vertical stabiliser attached to the aircraft?
3 or 4 lugs and pins
34
What can cause catastrophic vertical stabiliser failure?
Excessive application/deflection of the rudder
35
The advantage and disadvantage of a T tail?
- Predictable flight characteristics | - Prone to deep stall
36
What does the pylon do?
Attaches the engine to the wing
37
How are weight/thrust forces carried?
Strut braces
38
What is a fuse pin?
A bolt designed to break at a given load
39
Why are fuse pins used for the engine pylon?
Allow the engine to separate without causing excess damage to the wing