LESSON # 5 Flashcards

1
Q

Control of the fuel flow to the burners is by two main methods:

A

a. Manual control by the pilot.
b. Automatic adjustment of fuel flow to correct for basic engine requirements.

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2
Q

Automatic adjustment of fuel flow to correct for basic engine
requirements:

A

(i) Changes in intake pressure.
(ii) Excessive fuel to air ratio during engine acceleration.
(iii) Additional controlling devices as determined by specific engine requirements.

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3
Q

The flow of a fluid through an orifice (jet) depends on the area of the Orifice and the square root of the pressure drop across it.

A

Principle of Fuel Metering

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4
Q

= Orifice Area x √Pressure Drop

A

Fuel Flow

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5
Q

Fuel Flow =

A

Orifice Area x √Pressure Drop

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6
Q

it is possible to vary fuel flow by changing orifice area or the pressure drop across the orifice.

A

True

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7
Q

In a fuel system the (?) is variable and is in fact the throttle valve.

A

orifice

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8
Q

In the flow control system the fuel flow required to give a selected RPM is selected by throttle area under the control of the pilot (?).

A

manual control

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9
Q

Compensation for air density variation is superimposed on this selection
by the altitude sensing control unit (?) varying the pressure difference across the throttle valve.

A

pressure drop control unit

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10
Q

The controlling principle of a flow control system is that a constant throttle
pressure drop is [?] irrespective of throttle area (position) for a given
height and speed.

A

maintained

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11
Q

If however, height and speed change, then the [?] will
vary the pump output and fuel flow (thus throttle pressure drop)
by changing the pump output at constant throttle setting.

A

altitude sensing unit

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12
Q

two types of variable orifice

A
  1. Half-ball valve
  2. Kinetic valve
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13
Q

In [?], the method of control is to use servo fuel as a hydraulic fluid to vary fuel flow (eg. by varying pump swashplate angle).

A

hydro-mechanically operated flow control units (FCUs)

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14
Q

The (?) of the servo fuel is varied by controlling the rate of flow out of an orifice at the end of the servo line;

A

pressure

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15
Q

the (1) the outflow, the (?) will be servo pressure and vice versa.

A
  1. higher
  2. lower
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16
Q

The function of the (?) is to provide surge-free acceleration during rapid throttle openings.

A

Acceleration Control Unit (ACU)

17
Q

two main types of hydromechanical ACU in service

A
  1. FLOW TYPE ACU
  2. DASHPOT TYPE ACU
18
Q

All the fuel from the pump passes through the unit, which compares
fuel flow with compressor outletpressure (P3), which is proportional to [?].

A

engine speed

19
Q

The fuel from the pump passes through an orifice containing a contoured
plunger; the pressure drop across the orifice is also sensed across a diaphragm.

A

FLOW TYPE ACU

20
Q

When the throttle is opened, the pump moves towards maximum stroke and fuel flow increases. The increased flow through the ACU orifice increases the pressure drop across it and the diaphragm moves to the right, raising the half ball valve and restricting pump stroke.

A

FLOW TYPE ACU

21
Q

The engine now speeds up in response to the limited over fuelling and P3
rises, compressing the capsule. The plunger servo pressure drops and the
plunger falls until arrested by the increased spring force. The orifice size
increases, pressure drop reduces and the diaphragm moves to the left, closing the half-ball valve and increasing fuel flow. Fuel flow willincrease in direct proportion to the increase in P3.

A

FLOW TYPE ACU

22
Q

In order to keep the acceleration line close to the surge line, it is necessary to control on “Split P3 air” (a mix of P3/P1) initially and then on full P3 at higher engine speeds. This is achieved by the[?].

A

air switch
(or P1/P3 switch)

23
Q

P3

A

compressor outlet pressure

24
Q

At (?), P3 passes through a plate valve to P1 and the control capsule is operated by reduced, or split P3 until P3 becomes large enough to close the plate valve and control is then on full P3.

A

low speeds

25
Q

The (?) uses two co-axially mounted throttle valves.

A

DASHPOT TYPE ACU

26
Q

The inner one is moved by the pilot and the outer (main) throttle valve will move but is controlled by a [?] which slows the valve movement down to limit the acceleration fuel flow.

A

dashpot

27
Q

When closing the throttle the pilot pushes (?) sleeves in together.

A

both