It is an internal combustion engine that uses one or more reciprocating piston
Reciprocating engine
A rotary engine that extracts energy from a flow of combustion gases.
Turbine engine
Ambient air is drawn into the engine intake where an _ or a _ compressor (or both) increases both the pressure and temperature of the air before feeding it into the combustion chamber.
axial and centrifugal
2 means to keep pressurization air cool enough
Heat exchanger and full air cycle air conditioning system
The compression of air _ its temperature
raises
Turboprop aircraft often use this device
turbocompressor
Outside air is drawn in and compressed. It is mixed with the bleed air outflow from the turbine and is sent to the pressure vessel.
Turbine engine compressor
What is the advantage of the jet pump flow multiplier?
lack of moving parts
The disadvantage of the jet pump flow multiplier is only a _ can be pressurized in this manner.
relatively small volume of space
Mounted in air ducting that has one end open to the ambient air and the other end directed into the compartment to be pressurized.
venturi jet pump
Smaller turbine aircraft, or sections of a large aircraft, may make use of a
jet pump flow multiplier
With this device, bleed air is tapped off of the turbine engine's compressor section
jet pump flow multiplier
2 different ways hot, high pressure bleed air can be exploited are
Jet pump flow multiplier and turbine engine compressor
Modern large-cabin turbofan engine aircraft contain recirculation fans to reuse up to _ percent of the air in the cabin, maintaining high engine output
50
The main principle of operation of this engine involves the compression of large amounts of air to be mixed with fuel and burned.
Turbine engine
This engine is relatively free of contaminants. As such, it is a great source of air for cabin pressurization.
Bleed air
The limiting factors for determining the design ceiling of most reciprocating aircraft, which typically does not exceed _ feet.
25,000
Near _, the performance of any reciprocating engine and the pressurization compressor suffer.
maximum operating altitude
This engine aircraft overcome these shortcomings, permitting them to fly at much higher altitudes
turbine engine aircraft
Turbine engine aircraft overcome these shortcomings, permitting them to fly at much _ altitudes
higher
Both _ and _ are oil lubricated
superchargers and turbochargers
This is part of the fuel intake system
Supercharger
This is part of the exhaust system
Turbocharger
This component is driven by the exhaust
Turbine
This component pressurizes the incoming air
Compressor
Sometimes known as "turbosuperchargers"
Turbchargers
Is driven by engine exhaust gases
Turbochargers
Is the most common source of pressurization on modern reciprocating engine aircraft
Turbochargers
What are the 2 components of turbochargers?
Turbine and compressor
By using some of the turbocharger compressed air for cabin pressurization, less is available for the intake charge, resulting in _ overall engine performance
lower
What are the two types of engine driven compressor?
Belt driven and gear driven
An independent, dedicated compressor for pressurization
engine driven compressor
Engine driven compressor avoids some of the potential contamination issues of _ and _.
Superchargers and turbochargers
The _ does, however, add significant weight. It also consumes engine output since it is engine driven
compressor device
Is used to maintain a constant rate of airflow during changes of engine rpm
Ratio gear drive system
A type of engine driven compressor that is also found on reciprocating engine aircraft
Independent engine-driven centrifugal compressor
Found on older pressurized aircraft is gear driven by the engine. It pressurizes air as the rotors rotate very close to each other without touching.
Roots blower
Can be used as a source of pressurization if it is upstream of carburetion.
Supercharger
Mechanically driven by the engine
Supercharger
Have limited capability to increase engine performance.