M11c2

31問 • 4ヶ月前

ユーザ名非公開

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問題一覧

Aircraft fibreglass panels are protected against lightning strikes, partially by

bonding

System installation in an aircraft structure is provided by

brackets, reinforcements and cut-outs in the structure.

The radome is protected from lightning strike by

Diverter strips.

Ventilation to outside air is provided in a large transport aircraft fuselage structure in order to

relieve excess pressures and remove hazardous or foul smelling gases.

If an aircraft major structural element is replaced after a fixed number of flight cycles, this is known as

safe-life.

If an aircraft structure uses multiple load paths to ensure integrity, this design philosophy is known as

fail safe.

Damage tolerant structure is a structure where aeroplane damage is detected and repaired before

the strength is below a minimum level.

Exhaust gas deposits forming on areas of aircraft structure

can cause corrosion and must be removed with special solvents as recommended by the aircraft manufacturer.

The most common method of anodizing an aluminium alloy structural component is

sulphuric acid anodizing.

Fuselage formers are usually constructed of

pressed aluminium alloy sheet.

Stringers are usually constructed of

pressed aluminium alloy sheet.

Longerons are usually constructed of

pressed or rolled aluminium alloy.

The floor structure of a large transport aircraft passenger cabin is constructed of

beams, intercostals and composite/honeycomb sandwich panels.

A waffle doubler, bonded to the inside of a fuselage skin, performs the function of a

tear stopper.

An A symmetry check is carried out on aeroplane structure primarily

to check whether any distoration has taken place

The structure which carries flight, ground or pressure loads is called

primary structure

Damage to the nose cone of an aircraft is prevented during a lightning strike by

Bonding Strip

Composite materials are bonded by

special paint.

Most large transport aircraft skins are

2024.

oppose buckling in a semi-monocoque structure.

Stringers

The heat returned when the water vapour changes into a liquid is called

latent heat of condensation.

A method in which heat is transferred by vertical currents in a liquid or gas is

convection method.

The component that act as a reservoir for the refrigerant is

receiver/drier.

The actual height above sea level at which an aircraft is flying is called

aircraft altitude

The aircraft fuselage relies largely on the strength of the skin or covering to carry the primary stress is called

monocoque fuselage.

The colour used to identify the secondary structures is

Yellow or hatched.

The location identification system is used to pinpoint

the various locations in an aeroplane.

Pressurized aircraft cabin is affected by

Hoop stress.

The type of structure which carries only air or inertial loads is

tertiary

ATA zone 100 is

lower fuselage

The major zone number of landing gear is

700

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M6c1

M6c1

M6c2

M6c2

M6c3

M6c3

M6c4

M6c4

M6c5

M6c5

M6c6

M6c6

M6c7

M6c7

M6c8

M6c8

M6c9

M6c9

M6c10

M6c10

M6c11

M6c11

M7c1

M7c1

M7c2

M7c2

M7c3

M7c3

M7c4

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M10c1

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M7c5

M7c5

問題一覧

Aircraft fibreglass panels are protected against lightning strikes, partially by

bonding

System installation in an aircraft structure is provided by

brackets, reinforcements and cut-outs in the structure.

The radome is protected from lightning strike by

Diverter strips.

Ventilation to outside air is provided in a large transport aircraft fuselage structure in order to

relieve excess pressures and remove hazardous or foul smelling gases.

If an aircraft major structural element is replaced after a fixed number of flight cycles, this is known as

safe-life.

If an aircraft structure uses multiple load paths to ensure integrity, this design philosophy is known as

fail safe.

Damage tolerant structure is a structure where aeroplane damage is detected and repaired before

the strength is below a minimum level.

Exhaust gas deposits forming on areas of aircraft structure

can cause corrosion and must be removed with special solvents as recommended by the aircraft manufacturer.

The most common method of anodizing an aluminium alloy structural component is

sulphuric acid anodizing.

Fuselage formers are usually constructed of

pressed aluminium alloy sheet.

Stringers are usually constructed of

pressed aluminium alloy sheet.

Longerons are usually constructed of

pressed or rolled aluminium alloy.

The floor structure of a large transport aircraft passenger cabin is constructed of

beams, intercostals and composite/honeycomb sandwich panels.

A waffle doubler, bonded to the inside of a fuselage skin, performs the function of a

tear stopper.

An A symmetry check is carried out on aeroplane structure primarily

to check whether any distoration has taken place

The structure which carries flight, ground or pressure loads is called

primary structure

Damage to the nose cone of an aircraft is prevented during a lightning strike by

Bonding Strip

Composite materials are bonded by

special paint.

Most large transport aircraft skins are

2024.

oppose buckling in a semi-monocoque structure.

Stringers

The heat returned when the water vapour changes into a liquid is called

latent heat of condensation.

A method in which heat is transferred by vertical currents in a liquid or gas is

convection method.

The component that act as a reservoir for the refrigerant is

receiver/drier.

The actual height above sea level at which an aircraft is flying is called

aircraft altitude

The aircraft fuselage relies largely on the strength of the skin or covering to carry the primary stress is called

monocoque fuselage.

The colour used to identify the secondary structures is

Yellow or hatched.

The location identification system is used to pinpoint

the various locations in an aeroplane.

Pressurized aircraft cabin is affected by

Hoop stress.

The type of structure which carries only air or inertial loads is

tertiary

ATA zone 100 is

lower fuselage

The major zone number of landing gear is

700