Are you familiar with the phrase, aircraft bleed systems? The uncontrolled loss of blood air from the pneumatic system or any of the pneumatically powered services have the potential to inflict damage to aircraft structures. Bleed air is comprised of air taken from the compressor stage of a gas turbine upstream of its fuel-burning sections. Try this quiz and test your knowledge about aircraft bleed air systems.
14.69 psi
12.32 psi
13.45 psi
17.36 psi
To operate or control hydraulic systems or components.
To operate or control pneumatic systems or components.
To operate or control electrical systems or components.
To operate or control engine systems or components.
150 psi and 300-600 degrees Fahrenheit.
150 psi and 600-900 degrees Fahrenheit.
200 psi and 300-600 degrees Fahrenheit.
200 psi and 600-900 degrees Fahrenheit.
To protect upstream components from excessive pressure.
To protect downstream components from excessive pressure.
To protect upstream components from inadequate pressure.
To protect downstream components from inadequate pressure.
Inlet pressure and and temperature regulation.
Air temperature regulation and sensing.
Flow control and pressure limiting.
Pressure sensing and flow limiting.
Titanium.
Plastic.
Aluminum.
Stainless steel.
Oil.
Water.
Grease.
None.
Left and right secondary bleed air check valves.
Forward and aft secondary bleed air check valves.
Left and right primary bleed air check valves.
Forward and aft primary bleed air check valves.
0-150 psi
0-275 psi
0-350 psi
0-550 psi
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