DC Power System Flashcards

1
Q

DC (Direct Current) system overview

TR (Tie Relay)

A
  • The 737 uses 3 transformer rectifiers to supply 28 volt DC power
  • The TRs transfer change 155 volts AC from the transfer busses into 28 volt DC for use by the DC busses
  • The TRs change 115 volt AC from the transfer busses into 28 volt DC for use by the DC busses
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2
Q

TR (Tie Relay)

A

-The TRs change 115 volt AC from the transfer busses into 28 volt DC for use by the DC busses

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3
Q

TR (Tie Relay) overview

A
  • TR 1 is supplied by transfer bus 1 and is the normal power source for DC bus 1
  • TR 2 is supplied by transfer bus 2 and is the normal source for DC bus 2
  • Transfer Bus 2 is the normal power source for TR 3 (Tie Relay) but transfer 1 can also be used
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4
Q

TR 3 (Tie relay)

A
  • TR 3 is an auxiliary sourced of DC power if TR 1 and 2 fails
  • TR 3 is also the normal source of power for the battery bus
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5
Q

TR failure (Tie relay)

A

-If a TR fails, the remaining TRs can supply power for the total DC load

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6
Q

DC busses distribution

A

-DC busses are connected by a cross bus tie relay

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7
Q

Relays on an ILS approach

A
  • The relay opens automatically when the glide-slope is captured during the ILS approach
  • The relay opens to isolate the navigation receivers and flight computers. This prevents the removal of all approach information because of only 1 electrical failure
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8
Q

Relays + bus transfer switches

A

-The relay also opens when the BUS TRANSFER switch is moved to off

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9
Q

Normal sources of power to the DC busses fail

A

-The emergency source of DC power is the batteries

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10
Q

Battery Power

A

-Battery power:

  • 2 standby busses
  • Battery Bus
  • Hot battery bus
  • Switched hit battery bus
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11
Q

The Hot Battery

A
  • Hot battery bus is always connected to battery power

- It’s components operate as long as battery voltage is above minimum value

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12
Q

Hot Battery Source

A
  • Power to the switched hot battery bus controlled by the battery switch
  • The battery switch and battery operations are discussed as part of the standby power system
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13
Q

Automatic battery

A

-The automatic battery charger retorted and maintains full battery voltage

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14
Q

Battery charger

A

-The battery charger is supplied power from AC ground service bus 2 when a source of AC power is available

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15
Q

Second battery charger (left side)

A

-A different battery charger for the auxiliary battery is supplied power AC ground service bus 1

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16
Q

AC and DC metering panel

A

Normal indications:
-Normal voltage 26 volts

  • Amps vary with elect
  • The maintenance switch is used by maintenance personnel to do electrical system tests