Aircraft Electrical Power Systems Quiz
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Questions and Answers

What is the primary frequency of the AC electrical system?

  • 50 Hz
  • 400 Hz (correct)
  • 1000 Hz
  • 60 Hz
  • What is the voltage of the DC electrical system?

  • 28 V (correct)
  • 12 V
  • 200 V
  • 115 V
  • How many engine-driven generators are part of the electrical power system?

  • 1
  • 3
  • 2 (correct)
  • 4
  • What is the maximum power output of each engine-driven generator?

    <p>90 kVA</p> Signup and view all the answers

    What is the main purpose of the Generator Control Unit (GCU)?

    <p>To control the frequency and voltage of the generator output</p> Signup and view all the answers

    What is the purpose of the emergency generator?

    <p>To supply backup AC power if all main generators fail.</p> Signup and view all the answers

    What type of power does the static inverter transform?

    <p>Direct current to alternating current</p> Signup and view all the answers

    What is the output frequency of the AC power produced by the static inverter?

    <p>400 Hz</p> Signup and view all the answers

    When will the static inverter automatically activate if only the batteries are supplying electrical power and the aircraft speed is above 50 knots?

    <p>Regardless of BAT 1 and BAT 2 pushbutton positions</p> Signup and view all the answers

    When will the static inverter activate if only the batteries are supplying electrical power and the aircraft speed is below 50 knots?

    <p>If both BAT 1 and BAT 2 pushbuttons are on.</p> Signup and view all the answers

    What is the power output of the static inverter?

    <p>1 kVA</p> Signup and view all the answers

    What is the maximum DC current each main transformer rectifier (TR 1 or TR 2) can provide?

    <p>200 A</p> Signup and view all the answers

    What is the primary function of the Battery Charge Limiter (BCL)?

    <p>To monitor and control battery charging</p> Signup and view all the answers

    Under what circumstance would the ESS TR be used?

    <p>When either TR1 or TR2 fails, or the engine and APU generators fail</p> Signup and view all the answers

    What components are directly connected to the hot buses?

    <p>The main batteries</p> Signup and view all the answers

    Study Notes

    Aircraft Electrical Power System

    • The system has a three-phase 115/200 V 400 Hz AC and a 28 V DC system.
    • Electrical transients are acceptable for equipment.
    • Commercial supply is secondary.
    • Normal operation uses AC power.
    • The system has 2 engine generators and 1 APU generator.
    • Each generator can provide AC power to all bus bars.
    • Some AC power is converted to DC for specific uses.
    • Transformer rectifiers (TRs) supply DC power.
    • Two main TRs (TR 1 and TR 2) supply up to 200 A of DC current.
    • A third TR (ESS TR) powers the essential DC circuit from the emergency generator if main generators fail or if TR 1 or TR 2 fails.
    • A fourth TR (TR Entertainment) powers the DC Entertainment bus for In-Flight Entertainment (IFE).
    • If normal AC power fails, an emergency generator provides AC power.
    • If all AC power sources fail, the system can invert DC power from batteries to AC.
    • A static inverter transforms DC power from Battery 1 to 1 KVA of single-phase 115 V 400 Hz AC power. This power is then provided to part of the essential AC bus.
    • The inverter automatically activates when the aircraft speed is above 50 kt, if only batteries supply power.
    • The inverter activates at aircraft speeds below 50 kt if only batteries power the aircraft and both battery pushbuttons (BAT 1 and BAT 2) are on.

    Engine-Driven Generators

    • Two AC generators (GEN 1, GEN 2) provide power, one per engine.
    • Each generator supplies up to 90 KVA of 115/200 V 400 Hz three-phase power.
    • Generator Control Units (GCUs) control each generator's output.
    • GCU functions include: frequency and voltage control, and protecting the network through associated generator line contactor control.

    APU Generator and External Power

    • A third generator (APU GEN) can replace either or both main engine generators.
    • APU GEN supplies the same output as main engine generators.
    • Ground power is available through a nosewheel connector to all busbars.
    • A Ground Power Control Unit (GPCU) controls the external power contactor.
    • A Ground and Auxiliary Power Control Unit (GAPCU) regulates and protects the network via the APU Electronic Control Box, controlling external power and APU line contactors.

    Emergency Generator

    • A hydraulic circuit drives an emergency generator.
    • This generator supplies emergency AC power if all main generators fail.
    • The emergency generator delivers 5 KVA of 115/200 V 400 Hz three-phase power.
    • Its Generator Control Unit (GCU) maintains constant speed, controls output voltage, protects the network (with line contactor control), and controls start-up.

    Batteries

    • Two main batteries (each 23 Ah capacity) are connected to two hot buses.
    • Each battery has a Battery Charge Limiter (BCL) to monitor and control charging and its contactor.

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    Description

    Test your knowledge on aircraft electrical power systems, focusing on three-phase AC and DC systems, engine-driven generators, and APU generators. This quiz covers operational procedures, power generation, and emergency power scenarios critical for aircraft functionality.

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