Chap 1- Engine Principles Flashcards

1
Q

Newton’s third law

A

For every force acting on a body there is an equal and opposite reaction

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2
Q

What model was used in the history of jet propulsion

A

Aero themo dynamic duct

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3
Q

Modern day jet propulsion

A

Ram jet

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4
Q

How do Propel and jet produce thrust

A

Comes from thrusting backwards a large weight of air

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5
Q

What does a jet propulsion engine achieve

A

Accelerates a stream of air or gas and to expel at high velocity

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6
Q

What must the propeller engine be carefull off with regards to blade speed

A

It is kept below mach 1

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7
Q

What are the 5 types of jet engines

A

A. Rocket
B. Ram jet
C. Pulse jet
D. Tube jet/gas turbine engine
E. Turbo shaft

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8
Q

What jet engine is this :
Slef contained fuel/air mixture
When burnt exhaust is fed through an outlet nozzle no air needed

A

Rocket

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9
Q

What jet engine is this :
Consists of divergent entry or convergent
Or convergent/divergent exit
No rotating parts

A

Ram jet

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10
Q

What jet engine is this :
Similar to ATHODYD but with an added shutter system that help build pressure for combustion

A

Pulse jet

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11
Q

What jet engine is this :
Rotating components inside an ATHODYD that facilitates high pressure rise

A

Turbo jet/gas engine

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12
Q

What jet engine is this :
Gas turbine engine that is used to drive rotating component rather than being used for thrust

A

Turbo shaft

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13
Q

Look at the parts turbo jet engine

A
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14
Q

Basic layout photo of the gas turbine engine

A
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15
Q

What is a single spool and how does it work

A

Single shaft to the compressor
Number of turbine stages depends on power required to drive compressor

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16
Q

What is the highest amount of spool you can have

A

Triple spool

17
Q

Multi spool what is it how does it work

A

For engines with more than one compressor
Spool require a separate turbine for each of the spools
Each spool named after the lvl of pressure:
LP - low pressure
IP - intermediate pressure
HP - high pressure

18
Q

By pass what does it do

A

Allows a percentage of compressor air to flow around the outside the remainder of the engine
Designed to let over 50% = High by pass
Allow less than 50% = low by pass

19
Q

What can the by pass assist in

A

Noise reduction
Reduce fuel consumption

20
Q

What are the drive path configurations

A

Direct coupled turbo shaft
Free power turbine

21
Q

What type of path configuration is this :
Similar to single spool

A

Direct coupled turbo shaft

22
Q

What type of path configuration is this :
Engine compressor and turbines are separated from the turbine

A

Free power turbine

23
Q

What engine is most suitable for high forward speeds and high altitudes

24
Q

What engine is better at lower speed below 450 MPH

A

Propellor engine

25
What does the pure jet depend on largely
Forward speed
26
What is thermal efficency
The heat value or heat energy output of the engine, divided by the heat energy input ( fuel consumed )
27
When does thermal efficiency increase
As the turbine inlet temperature increases
28
When does combustion occur in gas turbine engine
Constant pressure
29
When does combustion occur in piston engines
Occurs at constant volume
30
What process is this : Pressure of the air does not rise during combustion, like that of a piston engines, but it's volume does increase
Heating at constant pressure
31
32
Brayton cycle
The working cycle
33
What is the relationships between pressure volume and temperature
The airflow or working fluid recieves and gives up heat changes P,V,T
34
Important understand photo
35
What are the advantages of a continuous working cycle
Smoother More power for a given engine size Use of lightweight combustion chambers and low octane fuels
36
What are the disadvantages of a continuous working cycle
High flame temperatures Critical component - THE TURBINE ( must not exceed turbine temperature otherwise turbine will just melt )
37
What is standard notation
Consists of pressure temperature or velocity and a number to represent a given position in an engine