Gas Turbine Engine Flashcards

History of Jet Propulsion, Jet Engines Basic Operation, Types of Jet Propulsion, Types of Gas Turbine Engine (58 cards)

1
Q

a writer and mathematician named
___________ devised a toy that used the
______________. The toy, called
the ____________, consisted of a
covered kettle of water that was
heated to produce steam.

WHAT YEAR?

A

Hero, reaction principle , aeolipile, 250 BC

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2
Q

The first patent covering a gas
turbine was granted to ____________
of England. It included all the
essential elements of the modern
gas turbine except that it had a
reciprocating-type compressor.

WHAT YEAR?

A

John Barber. 1791

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3
Q

______________ applied some of
his concepts in the development of
the ________________. This unique
supercharger consisted of a small
turbine wheel that was driven by
exhaust gases. The turbine was then
used to drive a supercharger

WHAT YEAR?

A

Dr. Sanford Moss, turbo-supercharger, 1900

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4
Q

________________ of England
developed what became the
first successful turbojet
engine and was granted his
______________-

WHAT YEAR?

A

Frank Whittle, first patent for the jet engine, 1930

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5
Q

_______________, a German
engineer, designed and built a
jet engine that produced ____________ of thrust.

WHAT YEAR?

A

Hans Von Ohain, 1,100
pounds, 1936

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6
Q

Hans’ engine was installed in the _______________ aircraft in ____________. it became recognized as the _______________ by a jet propelled aircraft.

WHAT YEAR?

A

Heinkel He-178, first practical flight, 1939

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7
Q

Frank Whittle’s engine
completed its first flight in a
_______________ aircraft.
The engine produced about _____________ of thrust and propelled the aircraft at speeds over _________________.

WHAT YEAR?

A

Gloster model E28/39, one thousand lb, 400 miles per hour, 1941

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8
Q

Another step in the progression of
commercial and military aviation was
the ability to produce an engine that
would propel an aircraft faster than
the speed of sound. Such aircraft are
the _____________ which flies in
excess of _________ and the
____________ capable of flying ____________
the speed of sound.

A

SR-71 Blackbird, Mach five, Concorde, 2.2 times

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9
Q

Newton’s First Law

A

A body in motion remains in motion, a body at rest remains at rest, unless acted upon by a force.

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10
Q

Newton’s 2nd Law

A

F=m*a

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11
Q

Newton’s Third Lan

A

For every action, there is an equal and opposite reaction

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12
Q

The main function of any airplane propulsion system is to provide a force to
overcome the aircraft drag,this force is called ____________-

A

thrust

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13
Q

When a jet engine accelerates air (mass), it makes _____________.

A

thrust (force)

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14
Q

Jet engine thrust can be increased in two ways:

A

Increase the speed of exhaust gases.

Increase the quantity of exhaust gases.

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15
Q

Basic Operation of a Jet Engine

A

AIR ENTERS THROUGH THE INLET DUCT (COWL).

AIR COMPRESSED BY PASSAGE THROUGH THE COMPRESSOR.

MIXED WITH FUEL IN THE COMBUSTION
CHAMBER.

FUEL IS IGNITED, PRESSURE AND TEMPERATURE RAISED

SOME OF THE PRESSURE USED TO TURN A TURBINE;

TURBINE SHAFT DRIVES THE COMPRESSOR.

HOT, HIGH PRESSURE AIR FORCED THROUGH A NOZZLE.

THE REACTION FORCE IS THE ENGINE THRUST.

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16
Q

Propulsion Devices

A

Air-Breathing

Non Air-Breathing

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17
Q

Air-Breathing :

A

Reciprocating Engines

GasTurbine Engine

Ramjet Engine

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18
Q

Non Air-Breathing:

A

Rockets

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19
Q

Types of Jet Engines

A

ramjet

pulse jet

scram jet

rocket

gas turbine engine

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20
Q

athodyd(or aero-thermodynamicduct), an air-breathing engine with no moving parts

A

Ramjet

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21
Q

Ramjet

With no rotating compressor to draw air into the engine, a ramjet must be
_____________- before it can produce thrust.

A

moving forward at high velocity

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22
Q

similar to ramjets except that the air intake duct is equipped with a series of
shutter valves that are spring-loaded to the open position.

A

Pulse Jet

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23
Q

A pulsejet is typically considered more useful than a ramjet because pulse jets can ________________.

A

produce thrust prior to achieving a high forward speed.

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23
Q

SCRAM Jet vs. Ramjet

A

a ramjet decelerates the air to subsonic
velocities before combustion,the airflow in a scramjet is supersonic throughout
the entire engine.

24
A _______________ is a variant of a ramjet air breathing jet engine in which combustion takes place in supersonic airflow.
scramjet (supersonic combustion ramjet)
25
A ___________ is a non-air-breathing engine that carries its own fuel and the oxygen needed for the fuel to burn
rocket
26
The two types of rockets in use:
solid-propellant rockets liquid-propellant rockets
27
used primarily to propel some military weapons and occasionally to provide additional thrust fortakeoff of heavily loaded aircraft.
solid-propellant rockets
28
The _____________ and oxidizer are carried in tanks aboard the rocket.
liquid propellant rockets
29
The __________ is the most practical form of jet engine in use today.
gas turbine engine
30
gas turbine engine Use ___________ to power a propeller or produce direct thrust by ____________________
high-temperature gases expanding and accelerating the exhaust gases through a nozzle
31
Types of GTE
Turbojet Turboprop Turboshaft Turbofan
32
The difference in velocity in the inlet and exit produces thrust.
Turbojet
33
which is the ratio of turbine discharge pressure to the inlet air pressure
engine pressure ratio
34
____________ engines are similar in design to turbojet engines except that the power produced by a ____________ engine is delivered to a _____________ that spins a propeller.
Turboprop, reduction gear system
35
______________ is necessary in turboprop engines because optimum propeller performance is achieved at much slower speeds than the engine's operating rpm.
Reduction gearing
36
The output of a turboprop or turboshaft engine is measured by __________ rather than thrust.
shaft horsepower
37
Turboshaft vs Turboprop
The main difference between the two variants is that a TP engine might also produce a fraction of its overall thrust via a hot core exhaust jet, while a conventional TS engine will have a lower exhaust velocity but correspondingly somewhat higher shaft power as the tradeoff
38
___________ were developed to provide a compromise between the best features ofthe turbojet and the turboprop.
Turbofans
39
Turbofan Nearly all present day airliners are powered by turbofan engines forthese reasons as well as because turbofans are _____________________
relatively fuel-efficient
40
Turbofans are likeTurbojets but also have a large fan accelerating the air’s entry into the engine and adding to the thrust as an ________________.
internal propeller
41
Inlet air passing through a turbofan engine is usually divided into two separate streams of air
One stream passes through the engine core Second stream coaxially bypasses the engine core
42
One stream passes through the engine core, and.....
i. Fuel and air is burned in the combustion chamber, ii. Air expands and spins the turbine which in turn drives the compressor. (self-sustaining) iii. Air leaves the exhaust at high velocities which produces thrust.
43
Second stream coaxially bypasses the engine core. and....
i. Air is accelerated through the bypass engine which contributes a significant amount ofthrust. ii. Aside from thatit also helps cooling the engine.
44
45
From this bypass stream of air, this powerplant is referred to as a ____________
bypass engine
46
a comparison ofthe thrust produced by the fan to the thrust produced by the engine core exhaust
Thrust ratio
47
refers to the ratio ofincoming airthat bypasses the core to the amount of airthat passes through the engine core.
Bypass ratio
48
Bypass ratios
low bypass (1:1) medium bypass (2:1 or3:1) high bypass (4:1 or greater)
48
_____________ determines a fan 's bypass ratio and thrustratio.
Fan diameter
48
ratio of air pressure leaving the fan to the air pressure entering the fan
Fan pressure ratio
48
The fan pressure ratio on a typical low bypass fan is approximately __________, Whereas the fan pressure ratio for somehigh bypass fans can be as high as _____________
1.5:1 7:1
48
Types Of PropFan
Unducted FanEngines Ducted Ultra High Bypass Engines
48
New engine designs with higher efficiencies than most engines in use are designated as ___________ and ____________
ultra-high bypass (UHB) propfan and unducted fan (UDF) engines.
49
Prop Fan These new engines use ___________, __________, and _____________ to improve fuel economy over several high bypass turbofan engines by more than _______ percent.
titanium, lightweight stainless steel, composite materials 15 percent
50
PropFan By incorporating propellers with composite blades between 12and 15 feet in diameter, engine designers have achieved __________ bypass ratios.
30:1
51
Another design encases the propfan in a conventional cowl-type inlet which can achieve _________ .These engines are known as _______________.
Mach 0.9 ducted ultra high bypass engines
58
Disassembly of A Gas Turbine Engine
Disassembly Cleaning Inspection Repairs Balancing Assembling Testing