Chapter 7 - Engine Fuel Systems section A Flashcards

1
Q

What are the two types of fuel systems?

A

Gravity-feed

Pressure-feed

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2
Q

What are the typical components of a gravity-feed fuel system?

A

Two fuel tanks

fuel selector valve

strainer

primer

carburetor

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3
Q

What item is required for pressure-feed fuel system?

A

Auxiliary Pump

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4
Q

Where can the engine fuel shutoff vlave be NOT located at?

A

On the engine side of any firewall

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5
Q

The fuel flow rate of a pump-feed fuel system for each reciprocating engine must be at what percentage of the takeoff required fuel flow?

A

125%

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6
Q

What expansion space must each fuel tank have for unfilled fuel?

A

2%

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7
Q

The fuel filler opening of an reciprocating and turbine aircraft fuel tank must be mark as what?

A

Reciprocating aircraft -

  • “AVGAS”
  • minimum grade of fuel

Turbine aircraft -

  • “Jet Fuel”,
  • the permissible fuel designation
  • maximum permissible fueling and defueling pressures
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8
Q

What is the purpose of an auxiliary fuel pump?

A

To maintain positve fuel pressure on the inlet side of the engine-driven fuel pump. It is also used to transfer fuel between tanks to redistribute fuel weight and maintain stability.

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9
Q

Define Volatility.

A

The measure of Avgas’ ability to change from a liquid into a vapor.

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10
Q

Define Reid Vapor Pressure.

A

The amount of pressure needed to prevent Avgas from changing from a liquid to a vapor.

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11
Q

What is the vapor pressure of 100LL fuel?

A

7 psi

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12
Q

What is the ideal ratio for the fuel/air mixture?

A

12(air):1(fuel)

Anything more than 12, mixture becomes lean, anything less mixture becomes rich

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13
Q

What is the proper way to adjust for mixture?

A

Monitor the RPM guage then idle cut off the mixture. The should be a rise of 10-25 RPM before engine dies. If there was anything more, the mixture was too rich. If there was anything less, the mixture was too lean.

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14
Q

What is Fractional Distillation?

A

A seperation of mixture into it’s component parts by heating or boiling them to their boiling points at which one or more compound or fraction will vaporize, then cooling the rest to retrieve a different chemical.

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15
Q

What is added to AVGAS to eliminate or reduce detonation? What does this substance do?

A

Tetraethyl Lead

It is able to retain heat energy for long periods of time without knocking

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16
Q

If fuel changes it state prior to reaching the fuel control unit, what is it called?

A

Vapor lock

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17
Q

Give three reasons why vapor lock might occur?

A

routing the fuel line too close to a heat source

Excessive fuel spirals

no fuel

Low fuel pressure

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18
Q

What is unusable fuel?

A

fuel trapped in the system that can never be used by the f.c.u

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19
Q

Define Viscosity.

A

A substance internal resistance to flow. (It’s thickness)

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20
Q

Name the different ratings of fuel.

A

80/87 - Red

90/93 - Clear

100LL - Blue

100/130 - Green

115/130 - Purple

The meaning: Hectane (lean)/Iso Octane (rich)

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21
Q

What formula is used to calculate horsepower?

A

PLANK

P = Internal Pressure

L = Length of stroke

A = Area of cylinders

N = number of power strokes

K = number of cylinders

ANY CHANGES affects H.P

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22
Q

Avgas ratings higher than 100 is it’s what?

A

Performance

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23
Q

The heat value of fuel is measured in what?

A

British Thermal Unit

(BTU)

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24
Q

How much does water weigh?

A

8 pounds per gallon

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25
Q

What is edge sealer used for?

A

Sealing the edges of placards

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26
Q

What fuel flow rate is required for gravity feed systems?

A

150%

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27
Q

What is a micron rated fuel filter?

A

A filter that only allows particles the size of a micron to filter through.

28
Q

What does it mean when a Delta-P indicator is protruding?

A

The filter is blocked

29
Q

What is the size of a micron?

A

One millionth of a meter

.000039

30
Q

Name the three parts of a filter

A

Housing

Element

Head

31
Q

What type of valve can be found in the head of a filter?

A

Relief Valve

32
Q

Define Vapor Lock.

A

When fuel changes its state from liquid to gas prior to reaching the fuel control unit and blocks the fuel lines.

33
Q

What are the advantages of Kerosene

A

Its has a high heat content and provides lubrication

34
Q

What is the foundation of all these different types of fuels?

A

They are all hydrocarbon based.

35
Q

What system is required for an aircraft that has a designated landing weight?

A

Jettison

36
Q

Name a characteristic of a constant displacemnt pump?

A

It is able to move the same volume of fuel regardless of speed.

Supplies more fluid than the system requires

37
Q

What is the weight of AVGAS vs Kerosene?

A

AVGAS = 6 pounds per gallon

Kerosene = 6.5 pounds per gallon

38
Q

An altitude compensating pump relief valve is vented to the _____ to maintain sea level pressure.

A

Upper deck pressure

39
Q

How to you lower pressure if the fuel pressure is too high?

A

Relief valve

40
Q

What can be used to prevent vapor lock?

A

Putting a fire sleeve over the fuel lines

41
Q

What is the purpose of a lay line?

A

It provides a visual reference to identify whether a hose is twisted.

42
Q

Name three requirements for the Jettison System?

A

It must be free from fire hazards.

It must not alter or effect the flight.

It must be able to dumb fuel and save enough for the aircraft to climb from sea level to 10,000 ft at full power.

43
Q

What is stoichiometric?

A

A air/fuel ratio of 15:1

With a stoiciometric mixture, all available fuel and oxygen are used in combustion, releasing the maximum amount of heat from the fuel.

44
Q

What antimicrobial agent is used to kill microbes, fungi, and bacteria?

What are two benifits of PRIST?

A

Biobore

PRIST

Two benifits of PRIST: Used for Anti-icing and its a antimicrobial agent.

45
Q

Define backfiring and afterfiring.

A

Backfiring - describes the fuel/air mixture burning in the induction system with a lean fuel/air mixture

Afterfiring - is the burning of fuel in the exhaust system because of a rich fuel/air mixture.

46
Q

What is the process of fuel’s energy transformation?

A

Chemical -> Heat -> Mechanical

47
Q

What fuel nozzle is required for turbine engines?

A

Duplex

48
Q

What would happen if Kerosene was added to a recipricating engine?

A

Nothing because the compression ratio of a normal recipricatng engine is not enough to compress the fuel.

49
Q

What is the purpose of a primer and what are the two types?

A

Primer - ejects raw fuel into the manifold upstream of the intake valve. It is normally used for cold weather of the first flight of the day.

Two Types:

  • Plunger - This is a manual type and brings fuel into the cabin
  • Electrical - This is remotely located and draws fuel from the main fuel manifold.
50
Q

What are the two classifications of heat exchangers?

A

Liquid to Liquid

Liquid to Air

51
Q

What are two functions of a P&D Valve?

A

Pressurizes the fuel manifold

Delivers fuel to the nozzle

52
Q

What is the final component of the fuel system?

A

The nozzle

53
Q

List two functions of a restrictor.

A

If the diaphram becomes broken, it will limit the fuel sucked out.

If the diaphram becomes broken, it will limit the air sucked in causing pump cavitation

54
Q

What are the two classifications of pumps

A

Constant

Variable

55
Q

What does “Delta P” mean on a filter?

A

It indicates if there is a change in pressure

56
Q

Why would some filters be ‘pleated’?

A

To get more surface area for cleaning

57
Q

What two places does the relief valve return fuel?

A

Back to fuel reservior

Inlet side of the pump

58
Q

Which jet fuel is most common?

What is it’s blend?

A

Jet B (JP-4) “Raw Cut”

30% Kerosene

70% Gasoline

59
Q

What is FADEC

A

Full Authority Digital Engine Control

60
Q

Where is the fuel nozzle located at?

A

In the diffuser or inlet of combustion chamber

61
Q

2 Types of nozzles

A

Simplex

Duplex

62
Q

Name the parts of a constant displacement pump

A

Gears

Vanes

Geo Rotors

63
Q

Diaphram engine pump is driven by what?

A

Camshaft

64
Q

Fuel screens can be found where?

Name four places

A

Fuel tank outlet

Boot pump inlet

Inline

Inlet of F.C.U

65
Q
A