Aircraft Assembly Flashcards

1
Q

involves the joining of various components and
structures that form an entire aircraft

A

Aircraft assembly

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2
Q

generally refers to the positioning and alignment of an aircraft’s major sub-assemblies to
produce a synergistic design.

A

rigging

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3
Q

five major stresses to which all aircraft are subjected

A
  • Tension
  • Compression
  • Torsion is the stress that produces twisting.
  • Shear
  • Bending stress
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4
Q

is the stress that resists a force that tends to pull something apart

A

Tension

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5
Q

is the stress that resists a crushing force.

A

Compression

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6
Q

occurs to thin sheet materials when they are subjected to end loads and to ties if
subjected to compressive forces.

A

Buckling

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7
Q

is a phenomenon that occurs in a member that is under compression with sufficiently short length to prevent instability

A

Crippling

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8
Q

is the stress that resists the force tending to cause one layer of a material to slide over an adjacent layer.

A

Shear

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9
Q

is a combination of compression and tension.

A

Bending stress

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10
Q

Major categories of aircraft

A

airplane, rotorcraft, glider, and
lighter-than-air vehicles.

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11
Q

the main structure or body of the fixed-wing aircraft. It provides space for cargo, controls, accessories, passengers, and other equipment

A

Fuselage

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12
Q

A —— is a rigid framework made up of members, such as beams, struts, and bars
to resist deformation by applied loads.

A

truss

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13
Q

The truss-framed fuselage is generally
covered with _______.

A

fabric

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14
Q

The ________ fuselage relies largely on the strength of the skin or covering to carry the primary loads.

A

monocoque (single shell)

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15
Q

The true monocoque construction uses _____, ______, ________ to give shape to the fuselage

A

formers, frame assemblies, and bulkheads

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16
Q

A heavy frame to contain pressures or
fluids or to disperse concentrated loads.

A

Bulkhead

17
Q

This construction is a modification to the monocoque type wherein the skin is stiffened by
longitudinal elements. (stiffeners, stringers, longeron).

A

Semi-monocoque Type

18
Q

The principal longitudinal member of
the fuselage that helps the skin support primary
bending load.

A

Longeron.

19
Q

Longitudinal member in the fuselage (or
spanwise member in the wing) to transmit skin
loads to body frames or wing rib.

A

Stringer.

20
Q

A metal part, other than flat sheet, used
in framing of a structure to provide rigidity

A

Stiffener.

21
Q

prevent stress concentration

A

Rounded corners

22
Q

fitted to pressurized aircraft must
withstand both the loads of pressurization and impact loads from bird strikes. They are constructed from toughened glass panels attached to each side of a clear vinyl interlayer.

A

Flight Deck Windows

23
Q

They are designed to be fail-safe and normally have two panes of acrylic plastic mounted in an airtight rubber seal fitted into a metal window frame. If one pane fails the other will prevent loss of cabin pressure

A

Passenger Cabin Windows