11.3 Fuselage Construction And Sealing Flashcards

1
Q

What are the three aircraft fuselage construction?

A

Truss type (Pratt or Warren), Monocoque type, Semi-monocoque type

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2
Q

What is a truss?

A

A form of construction in which several members are joined to form a rigid structure

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3
Q

When was Pratt truss used?

A

Early aircraft with wooden longerons as the main longitudinal structural members

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4
Q

In warren truss construction, how are the longerons connected?

A

They are connected with diagonal members

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5
Q

What are the similarities between Pratt and warren type?

A

Both have longerons, both have horizontal and vertical strut members

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6
Q

What are the differences between the Pratt type and warren type?

A

Pratt types diagonal stays are cable so they only take tensile loads, warren types diagonal stays are solid metal

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7
Q

What loads do truss take

A

Tensions and compression

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8
Q

What is stressed skin fuselage?

A

When loads are are carried in the exterior skin of a fuselage

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9
Q

How and why is an aircraft pressurised

A

Air is pumped into the cabin after take off and a difference in pressure between the inside and outside the cabin. This is regulated and maintained to ensure passengers have enough oxygen to breathe and move around the cabin without breathing apparatus

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10
Q

What can lead to metal fatigue on the aircraft cabin ?

A

The difference in air pressure inside and outside the cabin, and the cycling from pressurised to the unpressurised fuselage can lead to metal fatigue

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11
Q

What happens when an aircraft fuselage is pressurised and what is done to solve this?

A

Causes significant stresses on the structures which causes fatigue over cycles. To address this problem, semi monocoque fuselages were developed to take other stresses off of the fuselage

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12
Q

What are attached to the fuselage?

A

Wings, stabilisers, engine pylons and landing gears

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13
Q

What are pressurised joints used for?

A

Creating pressurised joints to make a “wet area” safe or for leak free joints

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14
Q

In the area of component attachment, why must the structure be reinforced?

A

To ensure all loads are transmitted from these attached assemblies to the fuselage

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15
Q

What are typical seals?

A

Faying seals, fillet seals

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16
Q

Where is a faying seal added?

A

Where there is a jiggle or overlap in material to provide a pressurised seal

17
Q

What is a fillet seal used for?

A

When two pieces of metal are joined together

18
Q

Why must cables running through pressure bulkheads be sealed?

A

To create an air tight seal