aircraft construction Flashcards

1
Q

pratt truss parts and loads

A

vertical member: compressive load
diagonal member: tension/compressive load
longerons: just struts

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2
Q

warren truss unique points

A

has no vertical pieces (except at 2 ends)

longerons connected only to diagonal members

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3
Q

monocoque is only effective for

A

small diameter fuselage

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4
Q

difference between monocoque and semi monocoque

A

monocoque has thicker skin

semi-monocoque has additional structures

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5
Q

monocoque consist of

A

stressed skin
formers
bulkhead

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6
Q

semi-monocoque consist of

A
outer skin
frames
stringers
longerons
bulkheads
floor beam
shear ties
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7
Q

outer skin, frames, stringers placement

A

outer skin: covers frames & stringers

frames: goes around the fuselage
stringers: longitudinal members

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8
Q

purpose of winglet

A

extra lifting area

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9
Q

purpose of ailerons

A

control aircraft movement about the longitudinal axis (rolling)

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10
Q

purpose of slats

A

increase lift at low speeds

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11
Q

purpose of flaps

A

enable aircraft to operate at lower speed for landing and takeoff

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12
Q

purpose of rudder

A

controls the movement about the vertical axis of the aircraft

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13
Q

purpose of elevators

A

control pitch or movement about the lateral axis of aircraft

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14
Q

primary structures points

A

failure may affect structural integrity and safety of aircraft (most impt)

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15
Q

secondary structures points

A

designed to have safe separation and will not affect ops of aircraft (2nd)
can continue to fly safely

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16
Q

tertiary structure points

A

failure will not significantly affect ops of aircraft

17
Q

metal alloys that are used to build aircrafts

A

Al Alloys - fuselage
Titanium alloys - main landing gear beams
Stainless steel - engine mounts, firewall
Monel (Nickel-Copper alloy) - landing gear

18
Q

longeron and bulkhead placement

A

longeron: like stringer but longer
bulkhead: like frames but at front or back of fuselage

19
Q

what is shear tie and what does it do

A

plates with holes

transfers weight from frame and floor beam to the skin

20
Q

wing structure

A

spars: perpendicular to fuselage
ribs: parallel to fuselage that have holes (like rib cage)
stringers: beams that go through ribs to stiffen the wing

21
Q

primary & secondary flight control surfaces

A

primary: ailerons, rudder, elevators
secondary: flaps, slats, spoilers

22
Q

power plant structure

A

pylon, nacelle, firewall, engine mount