Lecture 24 Flashcards

1
Q

What fuel was used in turbine engines in early days?

Why was it an issue?

A

Kerosene

Difficult cold-weather starting (primary issue with straight kerosene)

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2
Q

What fuel is used in turbine engines today?

A

Kerosene Type Fuel (additives blended into kerosene)
Blended Type Fuel (gas and kerosene)

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3
Q

What is the freeze point of Jet A fuel? How about Jet A-1?

Is Jet A fuel interchangeable with Jet A-1 fuel?

A

Jet A starts to freeze at -40°F
Jet A-1 starts to freeze at -58°F (same freeze point as avgas)

In a Jet A engine, you can use Jet A-1
In a Jet A-1 engine, you cannot use Jet A

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4
Q

What is the freeze point of Jet B fuel?

What is it a combination of?

A

Jet B starts to freeze at -60°F

Combo of Jet A and AVGAS

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5
Q

How much does kerosene weigh per gallon?

How much does avgas weigh per gallon?

A

6.7 pounds per gallon (required weight)

Aviation gasoline weighs 6 pounds per gallon (average, there is no required weight)

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6
Q

Can you use avgas when turbine fuel is not available?*

Should you use avgas all the time?*

A

Yes

No
Tetraethyl Lead (TEL) in AVGAS causes deposits to form on the turbine blades
Avgas does not lubricate as well as kerosene and causes excessive wear

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7
Q

Why does jet fuel viscosity cause issues?*

A

Jet fuel is more viscous than gasoline causing contaminants and water to take a long time to settle

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8
Q

What is scum?*

How can you prevent it?

A

Microscopic organisms living and multiplying at the interface between water and fuel

Additives such as Prist or other biocides to help prevent scum NOT remedy it

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9
Q

What additional precautions are taken with jet fuel to avoid microbial growth?

A

Protection against water contamination
-Fuel storage facilities
-Fuel delivery trucks
-Underground fuel hydrants
Fire Hazard
-Static Electricity produced as fuel flows at a high rate
-Fuel truck and delivery hose must be grounded
-Aircraft structure must be connected to the fuel hose with a low-resistance ground wire

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10
Q

What is the function of turbine engine fuel systems?

A

Under all operating conditions, provide the fuel control with the correct amount of clean fuel, free from vapor and at the correct pressure

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11
Q

What are the components of the fuel system?

A

Fuel Pumps
Fuel Strainers
Fuel Controls: Hydro-mechanical (older) and FADEC (newer)
Fuel Flowmeter
Fuel-Oil Heat Exchanger
Fuel Nozzles
Pressurizing and Dump Valve

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12
Q

What do fuel nozzles do?*

What are the two types?

What type of nozzles is more commonly used?

A

Atomize the fuel at the end of the fuel system to mix with air and form a combustible mixture

Simplex
Duplex

Atomizing nozzles

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13
Q

What is the equivalent of a throttle in a turbine engine?

A

Thrust lever

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14
Q

Why is it bad to be a “throttle jockey” in a turbine engine?

A

In a piston engine, throttle is instantaneous
In a turbine engine, you have to wait for thrust lever input to take effect

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15
Q

What are the two types of fuel control?

Which are you more likely to encounter?

A

Hydro-mechanical type (old)
Electronic type

Electronic

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16
Q

What is FADEC?

How does it control engine power?

A

Full-Authority Digital Electronic Control (FADEC)
Controls all engine functions and eliminates the need for a backup hydro-mechanical control

Controls engine power through direct control of the EPR (Engine Pressure Ratio)

17
Q

What are the advantages of FADEC?

A

No manual engine adjustments or tuning required
Improved engine starts
Constant idle speed
Saves fuel
Automatically limits critical engine pressures and speeds, reducing wear and possible damage

18
Q

What happens if both channels of FADEC fail?

A

All actuator motors are spring loaded to fail-safe positions
Fuel flow goes to minimum flow
Stator vanes will fully open
Air-oil cooler will fully open
ACC will shut off

19
Q

What is BITE?

How can an issue be identified by utilizing BITE?

A

Built-in test equipment (BITE)
FADEC uses it to perform self-test routines
Detects and isolates faults

Use a maintenance monitor to turn fault codes into English messages and identify the faulty line-replaceable unit (LRU)