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M15c13
27問 • 2ヶ月前
  • مقطع من الاغاني عراقيه قصيره
  • 通報

    問題一覧

  • 1

    When is the starter circuit terminated:

    when a self sustaining speed is reached

  • 2

    Selecting Start on the flight deck

    sets starter circuit and ignition circuit ON

  • 3

    In a low voltage starter system, how is the starter terminated in the event of self sustaining speed not being reached?

    By the cut- off time switch.

  • 4

    What is the main difference between the an AC and DC ignition circuit?

    the trembler switch or (chopper circuit) is not required in AC circuit

  • 5

    Why must the igniter plugs be depth checked before fitment?

    If too deep they will burn but if not deep enough they will not light the engine

  • 6

    If assistance from the starter were cut off below self accelerating speed the engine would

    fail to accelerate to idle speed. this is known as a hang start.

  • 7

    All air starter have a run time limitation to prevent

    overheating

  • 8

    Self starting speed is

    The RPM at which the engine continues without external assistance.

  • 9

    According to the large gas turbine engines the starter motor is mainly:

    air turbine

  • 10

    The start master switch on the cockpit

    switches the starting system ‘ON’. On some aircraft will prepare the aircraft electrical system for the start operation

  • 11

    An Igniter Plug for a large gas turbine takes the form of :

    surface discharge plug

  • 12

    An HEIU (high energy Ignition units )is rated in

    joules

  • 13

    Turbine engine igniter plug operates

    when starting or relighting the engine

  • 14

    Compared to an electrical starter, an air starter

    has a better power to weight ratio

  • 15

    The type and power source for the starter:

    varies in accordance with engine and aircraft Requirements

  • 16

    The electrical supply for starting system may be of

    low voltage or high voltage

  • 17

    As soon as the starter has accelerated the compressor sufficiently to establish an airflow through the engine

    the ignition is turned on, followed by the fuel.

  • 18

    Engagement and disengagement of Sprag Clutch in the starter is effected:

    centrifugally.

  • 19

    starter generator operates as a generator

    after the engine has reached a self-sustaining speed

  • 20

    The distribution of Air in the air Turbine Starter achieved by:

    electrically operated valves, switch controlled, from the flight deck.

  • 21

    Air for starting may be obtained from

    an auxiliary power unit

  • 22

    The Air supply to the starter control is regulated by

    the starting valve.

  • 23

    Hung Start means

    Engine lights up and reaches self-sustaining speed, but then the rpm is slow or fails to reach IDLE rpm

  • 24

    The discharge resistors are fitted to ensure that

    any stored energy in the capacitor is dissipated within one minute of the system being switched off.

  • 25

    The correct Starting Sequence for gas turbine engine

    starter, Ignition , fuel

  • 26

    On starting a jet engine, failure to light-up is indicated by

    low engine speed.

  • 27

    The glow plug operates

    by heat action

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    問題一覧

  • 1

    When is the starter circuit terminated:

    when a self sustaining speed is reached

  • 2

    Selecting Start on the flight deck

    sets starter circuit and ignition circuit ON

  • 3

    In a low voltage starter system, how is the starter terminated in the event of self sustaining speed not being reached?

    By the cut- off time switch.

  • 4

    What is the main difference between the an AC and DC ignition circuit?

    the trembler switch or (chopper circuit) is not required in AC circuit

  • 5

    Why must the igniter plugs be depth checked before fitment?

    If too deep they will burn but if not deep enough they will not light the engine

  • 6

    If assistance from the starter were cut off below self accelerating speed the engine would

    fail to accelerate to idle speed. this is known as a hang start.

  • 7

    All air starter have a run time limitation to prevent

    overheating

  • 8

    Self starting speed is

    The RPM at which the engine continues without external assistance.

  • 9

    According to the large gas turbine engines the starter motor is mainly:

    air turbine

  • 10

    The start master switch on the cockpit

    switches the starting system ‘ON’. On some aircraft will prepare the aircraft electrical system for the start operation

  • 11

    An Igniter Plug for a large gas turbine takes the form of :

    surface discharge plug

  • 12

    An HEIU (high energy Ignition units )is rated in

    joules

  • 13

    Turbine engine igniter plug operates

    when starting or relighting the engine

  • 14

    Compared to an electrical starter, an air starter

    has a better power to weight ratio

  • 15

    The type and power source for the starter:

    varies in accordance with engine and aircraft Requirements

  • 16

    The electrical supply for starting system may be of

    low voltage or high voltage

  • 17

    As soon as the starter has accelerated the compressor sufficiently to establish an airflow through the engine

    the ignition is turned on, followed by the fuel.

  • 18

    Engagement and disengagement of Sprag Clutch in the starter is effected:

    centrifugally.

  • 19

    starter generator operates as a generator

    after the engine has reached a self-sustaining speed

  • 20

    The distribution of Air in the air Turbine Starter achieved by:

    electrically operated valves, switch controlled, from the flight deck.

  • 21

    Air for starting may be obtained from

    an auxiliary power unit

  • 22

    The Air supply to the starter control is regulated by

    the starting valve.

  • 23

    Hung Start means

    Engine lights up and reaches self-sustaining speed, but then the rpm is slow or fails to reach IDLE rpm

  • 24

    The discharge resistors are fitted to ensure that

    any stored energy in the capacitor is dissipated within one minute of the system being switched off.

  • 25

    The correct Starting Sequence for gas turbine engine

    starter, Ignition , fuel

  • 26

    On starting a jet engine, failure to light-up is indicated by

    low engine speed.

  • 27

    The glow plug operates

    by heat action