Supercharging and Turbocharging Flashcards
Supercharger
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
Measuring Power Output
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
Maintaining Power at Altitude
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
Rated Boost
The highest manifold pressure the engine can tolerate without the danger of detonation
Ground Boosting
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
Altitude Boosting
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
Detonation Risks
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
To Avoid Detonation
Use only approved power settings
Use correct leaning procedures
The Compressor
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
PLANE = BHP
P = Power L = Length of the stroke A = Area of the piston N = RPM E = Number of cylinders
Increasing the Power
Mixture
RPM
Manifold pressure
Decreasing the Power
Manifold Pressure
RPM
Mixture
Normally Aspirated Engines
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
Power Augmentation Process
Pushing more air into the engine
Impellor
Works 6-12 times faster than the engine
Rated Altitude
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