CASA Part 66 - Turbine Aeroplane Systems Quiz
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Questions and Answers

What component in a turbine-powered aircraft converts the variable engine rpm to an alternator input speed of 12,000 rpm?

  • Hydraulic motor
  • CSD (correct)
  • Generator
  • IDG
  • How does the Quick Attach/Detach (QAD) adapter facilitate the maintenance of a turbine aircraft?

  • Converts engine power to electrical power
  • Is an integral part of the IDG system
  • Allows quick removal and replacement of the generator and CSD assembly (correct)
  • Regulates the AC frequency to 400 Hz
  • What is the purpose of the Integrated Drive Generator (IDG) in modern turbine-powered aircraft?

  • To operate at 9000 rpm
  • To drive the hydraulic motor
  • To convert AC to DC power
  • To reduce the weight and size of the traditional two-unit system (correct)
  • Which component cannot be replaced separately from the Integrated Drive Generator (IDG)?

    <p>Generator</p> Signup and view all the answers

    What is the typical rotation speed range of older alternators in turbine-powered aircraft?

    <p>$8000$ to $9000$ rpm</p> Signup and view all the answers

    What does the Constant Speed Drive (CSD) in a turbine aircraft contain that helps in RPM conversion?

    <p>Hydraulic trim units and a differential assembly</p> Signup and view all the answers

    What is the purpose of oil cooling in a generator section?

    <p>To increase the speed of the rotor</p> Signup and view all the answers

    In case of a complete failure of engine-driven generators, what powers emergency generators in aircraft?

    <p>Airstream-driven generator</p> Signup and view all the answers

    What type of alternators are emergency generators typically equipped with?

    <p>Permanent magnet alternators</p> Signup and view all the answers

    What is the function of the hydraulic motor-driven emergency generator system on larger transport aircraft like the Airbus A330?

    <p>To restore essential power during a loss of normal electrical power</p> Signup and view all the answers

    Why do emergency AC generation systems on aircraft typically use hydraulic motors?

    <p>To avoid battery usage</p> Signup and view all the answers

    What is the key advantage of emergency generators being constructed with permanent magnet rotors?

    <p>Elimination of battery dependency</p> Signup and view all the answers

    What causes the external power relay to open?

    <p>Tripping the operational generators</p> Signup and view all the answers

    What happens when the GCB of the second aircraft engine closes?

    <p>The BTB trips</p> Signup and view all the answers

    How are the essential AC loads supplied under normal operating conditions?

    <p>From the no. 1 generator bus</p> Signup and view all the answers

    What happens when one of the generators becomes inoperative?

    <p>The BTB closes to allow power distribution</p> Signup and view all the answers

    What is the purpose of connecting both generator buses together by closing the BTB?

    <p>To enable power supply from the serviceable generator to all system loads</p> Signup and view all the answers

    What does supplying power via auxiliary contacts of a tripped GCB to the BTB's close coil achieve?

    <p>Closes the BTB</p> Signup and view all the answers

    What is the purpose of the three-phase contactor in an aircraft AC external power system?

    <p>To monitor the input voltage and phase rotation of the external power source.</p> Signup and view all the answers

    Why is the external power contactor de-energized when an onboard generating source is brought online?

    <p>To prevent any conflicts between different sources of power.</p> Signup and view all the answers

    What happens when any inconsistency in the input external power is detected?

    <p>The three-phase contactor inhibits the application of power to aircraft systems.</p> Signup and view all the answers

    Why is it important to remove ground power when onboard generating sources are brought online?

    <p>To enable the aircraft to switch between different power sources seamlessly.</p> Signup and view all the answers

    What role does the external AC power schematic play in an aircraft's electrical system?

    <p>It ensures a continuous and stable supply of power to the aircraft systems.</p> Signup and view all the answers

    Why is the DC external power receptacle designed with two large pins and a smaller pin?

    <p>To enable interlock sensing and polarity check</p> Signup and view all the answers

    What purpose does the plug design with different-sized prongs serve?

    <p>To prevent incorrect insertion of the plug in the receptacle</p> Signup and view all the answers

    Why is the smaller pin in the DC external power receptacle shorter than the main pins?

    <p>To prevent arcing at the pins during plug withdrawal</p> Signup and view all the answers

    What safety feature is implemented by the DC external power receptacle design?

    <p>Preventing reverse polarity or reverse phase sequence issues</p> Signup and view all the answers

    Why is it important for the external power relay to de-energize before the main pins are disengaged during plug withdrawal?

    <p>To prevent damage to the aircraft's electrical components</p> Signup and view all the answers

    What event triggers the de-energization of the external power relay?

    <p>Removal of the plug from the receptacle while in use</p> Signup and view all the answers

    Study Notes

    Hydraulic Motor and Generator

    • The pump supplies hydraulic pressure to a hydraulic motor, which varies the ratio of input rpm to output rpm to maintain a constant output rpm to drive the generator and maintain an AC frequency of 400 Hz.
    • Quick Attach/Detach (QAD) adapter allows for quick removal and replacement of the generator and CSD assembly in a matter of minutes.

    Integrated Drive Generator (IDG)

    • The IDG contains both the generator and the CSD in one unit, reducing weight and size compared to traditional two-unit systems.
    • The generator is an integral part of the IDG and cannot be replaced separately.
    • The CSD converts variable engine rpm to an alternator input speed of 12,000 rpm.
    • Oil cooling allows for a higher-speed rotor within the generator section, resulting in a lighter, more compact generator.

    Emergency Power Generation

    • Emergency power generation is installed on many aircraft to supply essential power in the event of losing all normal power generation.
    • Emergency generators are typically permanent magnet alternators and do not require battery power to function.
    • Hydraulic electrical generating system (HEGS) uses a hydraulic motor-driven emergency generator system to provide emergency or standby electrical power.

    Hydraulic Electrical Generating System (HEGS)

    • The system consists of a hydraulic motor-driven generator designed to restore the essential power network in case of the loss of both normal main generator buses.
    • The generator is driven by a hydraulic motor supplied by an airstream-driven hydraulic pump.

    External and Ground Power

    • External AC power systems incorporate circuits that monitor input voltage and phase rotation.
    • If any inconsistency in input external power is sensed, the application of power to aircraft systems is inhibited by the three-phase contactor.
    • The DC external power receptacle has specific design features to prevent incorrect connection and ensure safe power supply.

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    Description

    Test your knowledge on hydraulic systems, generators, and CSD assemblies in the context of turbine aeroplane aerodynamics, structures, and systems as per CASA Part 66 training materials.

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