Module 1 Flashcards

HISTORY OFGAS TURBINE ENGINES AND INTRODUCTION TO JET PROPULSION (54 cards)

1
Q

it states that for every force acting on a body, there is an opposite and equal reaction.

A

Isaac Newton’s Third Law of Motion

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2
Q

It is the force which is generated in the
opposite direction to that of a discharge of fluid under
pressure, escaping through an opening.

A

Jet propulsion

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3
Q

Whatever the form that device utilizing the jet propulsion, it is essentially a __________________ in which it operates on _____________________.

A

reaction engine
Sir Isaac Newton’s Third Law of Motion

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4
Q

It consisted of a sphere into which steam was introduced
under pressure.

A

HERO’S ENGINE

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5
Q

What is the shape of a Hero’s engine?

A

Sphere

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6
Q

What is introduced into the sphere of Hero’s Engine to create motion?

A

Pressure

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7
Q

In hero’s engine, the ___________ escaping through nozzle mounted opposite one another on the surface of the sphere, created ____________,
which caused the sphere to rotate around its axis.

A

steam
thrust

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8
Q

In hero’s engine, where do steam passes through?

A

nozzle

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9
Q

It is one of the first attempts in developing jet powered
aircraft.

A

CAMPINI CAMPRONI CC-2

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10
Q

CAMPINI CAMPRONI CC-2 is one of the first attempts in developing jet powered aircraft resulted in the development of a ___________.

A

hybrid design

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11
Q

It is the force that pushes you deep into your seat as you speed down the runway for take-off. It is the force that propels an airplane forward through the air.

A

Thrust

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12
Q

What law is applied in jet propulsion by taking in a quantity of air and accelerating it through an orifice or nozzle.

A

Newton’s Third Law of Motion

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13
Q

In a applying Law of action and reaction in jet propulsion, The______________ is the action and _______________ is the reaction.

A

Acceleration of the air
Forward movement

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14
Q

During operation, a jet engine pushes gases out of the ___________________. This makes an unbalanced force towards the front of the engine.

A

exhaust nozzle

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15
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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16
Q

_____________will make an aircraft fly faster or with more weight.

A

Increased engine thrust

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17
Q

In hero’s engine, the sphere object is called _______

A

aeolipile

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18
Q

In CAMPINI CAMPRONI CC-2, Compressor output was mixed with ______, the combination was burnt and jet thrust resulted.

A

fuel

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19
Q

Year earlier than CC-2, the Germans had flown their
version of a jet powered aircraft namely________

A

HEINKEL 178

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20
Q

The HEINKEL 178 was powered by an engine designed by
young German scientist ________________.

A

Hans von Ohain

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21
Q

____________________ submitted patents for his jet engine in1930 but it was not until 1939 that sufficient financial
and technical backing was found to enable him to
manufacture a flyable version of his engine.

A

Sir Frank Whittle

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22
Q

The firm of _______- had initially been contracted to
produce the Whittle engine, but ____________ eventually
took over the development of the engine.

A

Rover
Rolls Royce

23
Q

Rolls Royce reworked the ____________ to produce the
_____________. Later versions of the engine, capable
of ____________ of thrust, were used to power the ______________

A

Whittle engine
‘Derwent’ engine
3,600 lb
Gloster Meteor F8.

24
Q

During a visit to the United States, the leader of the Rolls
Royce design team found that the Americans were
developing engines capable of producing up to__________lb of thrust. On his return to Britain, he initiated a project
which culminated in the ___________, which at the time
was the most powerful engine in the world, with _______
of thrust.

A

4000
Nene Engine
5,000 lb

25
What are two propulsion devices?
1. Air Breathing 2. Rockets
26
It Carries the entire propellant composed of liquid or solid fuel and the oxygen.
rockets
27
this propulsion device Uses atmospheric air and some fuel as main propellant.
air breathing
28
The examples of this propulsion device are piston engines, ramjet, scramjet, pulsejet, and gas turbine engines.
air breathing
29
What are the 8 basic steps of operation of jet propulsion engines?
1.Air enters through the air intake. 2.Air is compressed by passage through the compressor. 3.Air is mixed with fuel in the combustion chamber. 4. Fuel is ignited; Pressure and Temperature raised. 5. Some of the pressure is used to turn the turbine. 6. Turbine shaft drives the compressor. 7. Hot and high-pressure air is forced through the nozzle. 8. The reaction force is the engine thrust.
30
1. The main function of this system in any airplane is to provide a force to overcome the aircraft drag. 2. This force is called _________-.
1. Propulsion system 2. Thrust
31
The _____________ is by far the most practical form of jet engine in use today. In fact, It has become the standard on nearly all transport category, business, and military aircraft.
gas turbine engine
32
Types of Jet Engines
1. Ramjet 2. Pulse Jet 3. Scram Jet 4. Rocket Engine
33
what is the meaning of the acronym athodyd
aero-thermodynamic-duct
34
An athodyd (aero-thermodynamic-duct) which has no rotating parts and consists of a duct with a divergent entry and a convergent or convergent-divergent exit.
Ramjet
35
the concept of this jet engine is: With a forward motion imparted by an external source, air is forced in the divergent inlet (increasing its pressure) the total energy of air is further increased by combustion of fuel and the rapid expanding gases accelerate to the atmosphere through the outlet duct.
Ramjet
36
It can be run at static conditions unlike the ram jet and is constructed with a robust construction.
Pulse Jet
37
In pulse engine, its inlet duct has ______________ to the open position
spring loaded inlet valves
38
the operation of this engine is : as air passes to the combustion chamber, it produces high pressures as to force the valves close. As the exhaust gases exits, this creates a low pressure allows the valves to open and repeat the cycle.
Pulse Jet
39
Unstable as a powerplant due to high fuel consumption and cannot match performance of modern gas turbine engines.
pulse jet
40
It is a variant of a ramjet air breathing jet engine in which combustion takes place in supersonic airflow.
Scram Jet
41
Another name of scram jet
Supersonic combustion ramjet
42
What's the difference of scramjet and ram jet
Ramjet: It decelerates the air to subsonic velocities before combustion. Scramjet: It is supersonic throughout the entire engine.
43
This engine operate efficiently at high speeds
scramjet
44
A jet engine that does not use atmospheric air as a propulsive fluid stream (non-air breathing).
rocket engine
45
Rocket engines uses _________ thus enabling outside atmosphere operations
propellants.
46
The _____________ is the air delivered by the compressor.
mass
47
What delivers air as mass?
compressor
48
____________ is the difference between the outlet velocity of the air to that of its inlet velocity due to the addition of the heat energy.
acceleration
49
In gas turbine engines, combustion occurs at constant ____________.
pressure
50
Power is developed in the _________________.
turbine of the engine
51
The processes occur in a ____________manner in a gas turbine engine.
continuous
52
In a four-stroke piston engine,____________ stroke is utilized in producing power, the other __________are effectively absorbing power.
one three
53
In relation to a four-stroke piston engine, the gas turbine engine eliminates the _______________strokes, allowing more time for fuel combustion.
three idle
54
Theoretically, combustion in the gas turbine occurs at a constant _____________. This is achieved partly because of the continuous process of the __________ cycle, and also the fact that the combustion chamber is not an enclosed space.
Pressure Brayton