Power Distribution and External and Auxiliary Power Supplies Flashcards

1
Q

In most types of aircraft, the output from the generating sources is coupled to one or more low impedance conductors, what are these called?

A

busbars

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2
Q

perform a “carry-all” function

A

busbar systems

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3
Q

usually situated in junction boxes or distribution panels located at central points within the aircraft

A

busbars

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4
Q

provide a convenient means for connecting positive supplies to various consumer circuits

A

busbar

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5
Q

Categories of consumer services

A

vital services, essential services, non-essential services

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6
Q

those which would be required after an emergency wheels-up landing

A

vital services

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7
Q

these services are connected directly to the battery

A

vital services

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8
Q

required to ensure safe flight in an in-flight emergency situation

A

essential services

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9
Q

connected to dc and ac busbars and in such a way that they can always be supplied from a generator or from batteries

A

essential services

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10
Q

those which can be isolated in an in-flight emergency for load shedding purposes, and are connected to dc and ac busbars supplied from a generator

A

non-essential services

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11
Q

is required for the starting of engines, operation of certain services during “turnaround” servicing periods at airports

A

electrical power

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12
Q

is required for the testing of electrical systems during routine maintenance checks

A

electrical power

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13
Q

are restricted to the supply of power under emergency conditions

A

batteries of an aircraft

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14
Q

provides power for engine starting, ground air conditioning, and other electrical services

A

Auxiliary Power Unit (APU)

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15
Q

used for supplying power in flight in the event of an engine-driven generator failure and for supplementing the delivery of air to the cabin during take-off and climb

A

Auxiliary Power Unit (APU)

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16
Q

consists of a small gas turbine engine, a bleed air control and supply system, and an accessory gearbox

A

Auxiliary Power Unit (APU)

17
Q

comprises a two-stage centrifugal compressor connected to a single-stage turbine

A

gas turbine

18
Q

automatically regulates the amount of air bleed from the compressor for delivery to the cabin air conditioning system

A

bleed air control and supply system

19
Q

drives a generator which is of the same type as those driven by the main engines and having the same type of control and protection unit

A

accessory gearbox