JET PROPULSION Part 6 Thrust Augmentation and Reversers.
Click here to load reader
-
Upload
sabrina-kealey -
Category
Documents
-
view
272 -
download
3
Transcript of JET PROPULSION Part 6 Thrust Augmentation and Reversers.
JET PROPULSION
Part 6
Thrust Augmentationand Reversers
Thrust Augmentation
Is a method of extracting more power from Internal Combustion Engines.
It’s a form of ‘Power Boosting’
We shall examine two main typesof augmentation systems,
Water Injectionand
Reheat or Afterburning
Water Injection Systems
Operation of either Water or Water Methanol systems
cools the turbine, and allows water to be injected
into the fuel spray nozzleswhich cools the air flow in the combustor
allowing more fuel to be added.
Water Injection
Water InjectionRolls-Royce Spey Turbo Fan Series
Primary Fuel flow
Water flow
Water Injection allows water to be injectedvia additional nozzles built into the fuel spray nozzles.
Operation of the water injection systemautomatically resets the fuel control unit
to allow more fuel to flow.
IncreasedPrimary
Fuel flowCombustion Chamber
Water InjectionRolls-Royce Spey Turbo Fan Series
Primary Fuel flow
Water flow
Water Injection allows water to be injectedvia additional nozzles built into the fuel spray nozzles.
The water injection system automatically resets the fuel control unit to allow more fuel to flow.
Water cools the turbine, increases pressure and velocity.More Power.
Cooler turbine means more fuel can be added.More Power.
IncreasedPrimary
Fuel flowCombustion Chamber
Water InjectionRolls-Royce Spey Turbo Fan Series
Primary Fuel flow
Water flow
Combustion Chamber
IncreasedPrimary
Fuel flow
Water cools the turbine, increases pressure and velocity
More Power.
Cooler turbine means more fuel can be added More Power.
Water Methanol Control Unit
Water Methanol InjectionDart Engine Turbo Prop Series
Water Methanol Tank and Pump
The Control Unit has two functions:
1. Switching water-methanol flow through the unit when the throttle moves to the take-off position.
2. Regulating rate flow based upon engine power, and atmospheric pressure.
Water Methanol Control Unit
Water Methanol InjectionDart Engine Turbo Prop Series
Water Methanol Tank and Pump
Torque Pressure (ENGINE POWER)
More power means coarser propeller pitch More Thrust.
Cooler turbine means more methanol can be added Even More Power.
Water cools the turbine, increases pressure & velocityMore Power.
Questions ?
The Re-Heat/Afterburn System
Provides extra thrust
without increasing
the engine's frontal area
Engine Rear End Reheat System (Afterburner)
The Re-Heat/Afterburn System
The system consists of a larger diameter jet pipe, with internal heat shields.
Inside are vapour gutters and fuel spray tubes.
The variable nozzle is closed (reheat off) or opened (reheat on)
Reheat/Afterburn consists of burning additional fuelin the jet pipe.
Spray Tubes Vapour Gutters Heat Shields
Jet PipeVariable NozzleClosed
The Re-Heat/Afterburn System
Jet Pipe
The vapour gutters spray fuel into the gas stream.
The Spray Tubes add more fuel to the process, which is fired by catalytic igniters,
using oxygen from the combustion chambers.
The variable nozzles open to maintain pressureand to ensure reheat has no effect on the engine.
Gas stream without reheat
Variable NozzleOpens
Variable NozzleClosed
The Re-Heat/Afterburn System
Visible ‘shock waves’ appear in the exhaust plume
Concord was the only passenger aircraftto have Reheat/Afterburners.
In military aircraft afterburner use is used for Take-off,
In-flight accelerationand Combat only
due to the extremely high fuel consumption rate.
Questions ?
Thrust Reversal
Thrust Reversal is simply a method of altering Jet reaction
from a rearward direction (which provides normal forward thrust)
to a forward direction,
providing reverse thrust(using the power as a decelerating force)
and is operated by the pilot on landing.
Thrust reversersreduce the landing roll out.
In civilian aircraft this is primarily to save wear and tear on the brakes, to clear busy runways and to achieve quick turn-rounds, i.e. keeping passenger delays to a minimum.
In military aircraft the above can apply, and also to give shorter landings for tactical reasons,i.e. the aircraft can land and unload supplies quickly,thus minimizing any risk in hostile environments.
Reverser Effects
Shorter Landing Roll-out
Diverting some or all of a rearward directed jetin an almost forward direction,will provide a reverse thrust.
The gas stream should be directedin a completely forward direction; but this is not possible for aerodynamic reasons.
Yet an angle of 90o to 45o forward is common,giving reverse thrust up to 50% of forward thrust.
Reverser Effects
Questions ?
Thrust ReversersTranslating Cowl Type
BLOCKER DOORS
BLOCKER DOORS
TRANSLATING COWL
TRANSLATING COWL
Reverse Thrust
CASCADESUsed on –
The Tri-Star and C17 (illustrated)
The C17 deployment is extremely unusualin that it can deploy the thrust reversers in flight
for a tactical descent from high altitude,thereby minimising the threat of
anti-aircraft fire etc in a hostile area.
Normal Forward Thrust
Thrust ReversersPivoting Door Type
Normal Forward Thrust
Reverse Thrust
PIVOTING DOOR
PIVOTING DOOR
SENTINEL LANDING – THRUST REVERSERS DEPLOYED
Used on –
The RAF Sentinel R17 (illustrated)
It comprises of two doors on this system, but multi door systems are replacing
the translating cowl designs on high by-pass fan engines.
Thrust ReversersClam Shell Door Type
Normal Forward Thrust
CLAM SHELL DOOR
CLAM SHELLDOOR
Reverse Thrust
VC10 LANDING – THRUST REVERSERS DEPLOYED
Used on –
The VC 10 (illustrated)
All four engines have the reverser fitted,but on RAF aircraft, the two inboard
reversers have been inhibited because the jet blast from all four
created too much buffeting on the fin and elevator.
TARGET DOOR
TARGET DOOR
Thrust ReversersTarget Door Type
Normal Forward Thrust
Reverse Thrust
Used on –
The Tornado (illustrated)
This system does redirect the jet thrust slightly forward, witness the exhaust staining
on the aircraft fuselage and tail.
Thrust ReversersOther Methods
Reversing the pitch of the propeller blades, sends the thrust in a totally forward direction.
Used on Hercules
REVERSE PITCH PROPELLER
Parachutes can be deployed whichincrease the drag and increase thedeceleration of the aircraft.
Used on Vulcan
DROGUE PARACHUTE
Thrust Reversers
Translating Cowl TypeThe Tri-Star and C17
Pivoting Door TypeThe Sentinel R17
Clam Shell Door TypeThe VC 10
Target Door TypeThe Tornado
Questions ?
How does water injection increase power in a jet engine?
It cools the air flow in the combustorallowing more fuel to be added
It makes the combustion burn slower
It allows less fuel to be used
It heats the air flow into the engineallowing more fuel to be added
Check of Understanding
Check of Understanding
Which of the following is a type of jet engine augmentation system?
Turbocharging
Rocket Boosting
Supercharging
Water Injection
In a typical reheat system, oxygen is required in the jet pipe for combustion.
Where does the reheat oxygen come from?
From on board oxygen bottles
Oxygen is pumped in with the extra fuel
Unburnt oxygen from the combustion chambers
Slipstream air is scooped into the jet pipe
Check of Understanding
Which sentence is true? Afterburning….
a. is restricted for take-off and combat.
b. adds more fuel to the reheat section.
c. results in an extremely high fuel consumption.
d. produces visible shock waves in the exhaust.
A, B, C and D
A and C only
A, B and D only
A, C and D only
Check of Understanding
After-burning in a jet engine involves burning additional fuel in the:
Turbine
Combustion Chamber
Jet pipe
Compressor
Check of Understanding
What is the function of the Spray tubes in the afterburner?
To add more fuel to the combustion process
To inject water to control the temperature
To control the afterburner internal pressure
To add more air to the combustion process
Check of Understanding
When is reheat used in a combat aircraft?
All of the above
At take-off
During combat manoeuvrings
For in-flight acceleration
Check of Understanding
In a modern reheat system, how is the flame ignited?
By heat and compression
By the heat from the combustor
By igniter plugs in the jet pipe
By catalytic igniters
Check of Understanding
Thrust reversers generally fall into four types,what are these types?
Transmission cowl, pilot doors, clamshell doors and target doors
Transmission cowl, pilot doors, crab shell doors and bucket doors
Translating cowl, pivot doors, clamshell doors and target doors
Translating cowl, balanced doors, clamshell doors and target doors
Check of Understanding
Check of UnderstandingWhat is thrust reversing?
Driving the aircraft wheels backwards
Turning the engine to point in the opposite direction
Making the engine shaftrotate in the opposite direction
Redirecting the engine exhaust in a forward direction
Check of UnderstandingWhich type of thrust reverseris shown in the illustration?
Target door
Pivot door
Clamshell door
Translating cowl
Reverse thrust is simply a method of altering what?
The engine RPM
Primary air-flow
Jet reaction
The engine cooling
Check of Understanding
Check of UnderstandingWhich type of thrust reverseris shown in the illustration?
Target door
Translating cowl
Pivot door
Clamshell door
Which of the following aircraft use the clamshell door system?
Tristar
Tornado
VC 10
Sentinel R17
Check of Understanding
Check of UnderstandingWhich type of thrust reverseris shown in the illustration?
Target door
Translating cowl
Pivot door
Clamshell door
Which of the following aircraft use the target door system?
Tristar
Tornado
Hercules
Vulcan
Check of Understanding
Check of UnderstandingWhich type of thrust reverseris shown in the illustration?
Target door
Pivot door
Clamshell door
Translating cowl
Which of the following aircraft use the translating cowl system?
Hercules
C17 Globemaster
R17 Sentinel
Vulcan
Check of Understanding
Check of UnderstandingWhich type of thrust reverseris shown in the illustration?
Target door
Pivot door
Clamshell door
Translating cowl
Which of the following aircraft use the pivot door system?
Tristar
Tornado
VC 10
Sentinel R17
Check of Understanding
Which of the following statements applies to the process of afterburning,
as used in some jet engines? It provides extra thrust without:
The use of additional fuel
Increasing the exhaust velocity
Increasing the engine's frontal area
Removing any more oxygen from the exhaust gases
Check of Understanding
Questions ?
JET PROPULSION
End of Presentation