Supercharging and Turbocharging Flashcards

1
Q

Supercharger

A

A piston engine with an engine driven compressor
May be used to :
1. Boost the manifold pressure at sea level
2. Compensate for reduced density at altitude by maintaining the power available at sea level

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2
Q

Measuring Power Output

A

In an engine with a CSU the pressure of the mixture in the manifold is a measure of the power output
Power can be monitored on the RPM and manifold pressure gauge

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3
Q

Maintaining Power at Altitude

A

Pumps high pressure air into the inlet manifold using a compressor, allowing the engine to burn extra fuel and produce extra power
Allows engine to maintain power in the climb

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4
Q

Rated Boost

A

The highest manifold pressure the engine can tolerate without the danger of detonation

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5
Q

Ground Boosting

A

When manifold pressure can exceed 30 inches
Can tolerate a manifold pressure greater than normal sea level pressure without the risk of detonation and can boost the inlet manifold pressure above the normal sea level pressure
Engine develops more power at sea level and maintain better power output at altitude
MAP will progressively reduce in a climb, however it will reduce from a higher manifold pressure

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6
Q

Altitude Boosting

A

To allow the engine to develop the power required at altitude the compressor is able to overboost the engine at sea level and damage it at sea level if full throttle is used
Open the throttle partially at sea level and continue to open it as you climb
At a point in the climb, the throttle will be fully open and max MAP will still be maintained, as you climb higher the MAP will then start to reduce

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7
Q

Detonation Risks

A

As the supercharger compresses the mixture, the MAP increases and the temperature rises
If the manifold air pressure is too high (overboosted) the temperature limits may be exceeded and there is a risk of detonation
High manifold pressure and low RPM

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8
Q

To Avoid Detonation

A

Use only approved power settings

Use correct leaning procedures

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9
Q

The Compressor

A

Air enters at the centre of a rapidly rotating impeller
Inertia causes the air to be thrown outwards, accelerating in the process
It is slowed by passing through diffuser vanes and the kinetic energy is converted to pressure energy
The compressed air then enters the manifold

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10
Q

PLANE = BHP

A
P = Power
L = Length of the stroke
A = Area of the piston
N = RPM
E = Number of cylinders
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11
Q

Increasing the Power

A

Mixture
RPM
Manifold pressure

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12
Q

Decreasing the Power

A

Manifold Pressure
RPM
Mixture

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13
Q

Normally Aspirated Engines

A

Best manifold pressure = 29.92 inches of mercury (1013.25hpa) at sea level
As the aircraft climbs this will gradually decrease at approx 1hpa per 30ft

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14
Q

Power Augmentation Process

A

Pushing more air into the engine

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15
Q

Impellor

A

Works 6-12 times faster than the engine

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16
Q

Rated Altitude

A

The maximum height at which manifold pressure can maintain 30 inches
Manifold pressure increases to rated altitude as the exhaust gases exit more easily as the density of the air decreases and can be higher than 30 inches

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17
Q

Automatic Boost Controller

A

Controls the amount of air going into the cylinder
Ensures you don’t exceed 30 inches otherwise the cylinder may pop
Boost gauge = tells an increase in PSI according to 30 inches

18
Q

Types of Superchargers

A

Geared (internally driven)

Turbochargers (driven externally by exhaust gases)

19
Q

Geared Superchargers

A

The impeller is driven from the crankshaft via gears

A clutch arrangement enables them to operate at different speeds

20
Q

Speeds of Geared Superchargers

A

Single-speed
Two-speed
Variable speed

21
Q

Gear Ratios

A

Usually between 6:1 and 12:1 to give the required boost

It is important to make smooth RPM changes at avoid dramatic acceleration or deceleration of the impeller

22
Q

Single-Speed Superchargers

A

Have a high gear ratio (high impeller RPM) which provides optimum performance at high altitude but lower performance near sea level

23
Q

Two-Speed Superchargers

A

Have two optimum altitude ranges

Means you can change gears to gain a greater manifold pressure at higher altitude (a greater BHP for longer)

24
Q

Variable Speed Superchargers

A

Maintain an impeller speed close to optimum throughout the altitude range of the aircraft
Are more complex in design

25
Q

Turbocharger

A

Driven by the exhaust gases by placing a turbine in the exhaust system, which creates a better way to control the speed of the impeller
Exhaust gases drive the turbine and then exit to the exhaust pipe, the turbine controls how fast the compressor turns

26
Q

Waste Gate

A

Varies the amount of exhaust gas that drives the turbine

Either fixed or variable

27
Q

Open Waste Gate

A

All the exhaust gas goes overboard and the turbine ‘free-wheels’ with the engine working as if normally aspirated

28
Q

Closed Waste Gate

A

As the gate is closed, more exhaust gas is directed over the turbine, increasing the compressor speed and boosting the manifold pressure

29
Q

Advantage of Turbochargers

A

The compressor does nothing until the throttle butterfly is open
As the throttle is opened further, the waste gate closes and the turbine delivers power to the compressor

30
Q

Fixed Waste Gate

A

A fixed proportion of the exhaust gas goes to the turbine all the time
Overboosting is possible at low altitude
At no stage is all the gas available to drive the turbine so the boost is limited

31
Q

Variable Waste Gate

A

Movement is controlled by:

  1. A pilot operated lever
  2. Throttle operated
  3. Automatic operation
32
Q

A Pilot Operated Lever Waste Gate

A

Allows you to adjust the wast gate manually

During the climb the pilot can gradually close the waste gate and maintain MAP

33
Q

Throttle Operated Waste Gate

A

The first portion of throttle movement opens the throttle butterfly
Once the throttle is fully open, any further movement of the throttle closes the waste gate and powers the turbine

34
Q

Automatic Operation Waste Gate

A

Controlled automatically to maintain MAP

35
Q

Waste Gate Control

A

Fully closed at critical height
Spring opens the waste gate
Oil pressure closes the waste gate
At higher altitude settings, the oil pressure increases, which closes the gate, as the oil aneroid capsule increases pushing the needle down stopping oil flow and creating a build up

36
Q

Density Controller

A

Takes into account pressure and temperature

37
Q

Advantages of Increased Manifold Pressure

A

Can carry more weight

Require less runway

38
Q

Full Throttle Height

A

The height at which a certain power is available with only full throttle

39
Q

Full Throttle Height In a Supercharged Engine

A

The altitude at which the rated boost is available at a certain RPM (any lower MAP setting will also have a higher full throttle height)

40
Q

Handling Techniques

A

Do not exceed rated boost - only use recommended MAP/RPM settings
Avoid sudden throttle movements
Avoid sudden shutdowns