Pressurization Flashcards
Pressure
Pressure decreases as Altitude increases
Temperature decreases as Altitude increases
●-2 degrees Celsius per 1000’ gained
Sealed cabin
High altitude/space flight
Oxygen is circulated and filtered
Pressurized cabin
Forces ambient air into the cabin
Pressurization terms
Cabin Altitude – air pressure inside the cabin
●Ex: Cabin Altitude is 8000ft (MSL)
Cabin Differential Pressure – the difference between the air pressure inside the cabin and the air pressure outside the cabin.
●Cabin Pressure – Ambient Pressure = CDP
Cabin Rate of Climb – the rate of change of air pressure inside the cabin (fpm).
Pressurization requirements
Be able to maintain a cabin pressure of 8000’ or lower, regardless of cruising altitude
Be able to prevent rapid changes of cabin pressure
Circulate air from inside to outside to eliminate odors and remove stale air
Be able to produce comfortable temps inside the cabin
A pressurized cabin must have
●Air tight Seal
●Cabin structure
●Source of compressed air
●Temperature regulation
●Pressure regulation
Cabin structure
A structure strong enough to withstand forces in flight plus act as a pressure chamber.
●Doors
●Windows
●Control cables
●Electrical wires
•Must also be light weight
Source of air pressure
Reciprocating Engines
●Turbocharger
●Supercharger
●Engine Driven Compressor
Independent compressor for pressurization
Less air available for engine when used for cabin pressure
Turbine engine
Turbine’s purpose is to compress large amounts of air to be mixed with fuel and burned
Provides a great source for uncontaminated air
Types:
●Jet Pump
●Turbo Compressor
●Air Cycle Machine
Jet pump
Bleed air goes into a Venturi Pump
Low pressure from venturi also brings in outside air
Air is mixed and used to pressurize
Turbo compressor
Bleed air drives a separate compressor
Outside air is drawn in and compressed
Air is mixed and used to pressurize aircraft
●Usually found on turboprop aircraft
Air cycle machine
Bleed air turns turbine
Air is compressed and then allowed to expand and cool
Bypass air is mixed back in to control temperature
Isobaric pressure control
Maintains the set Cabin Altitude at a single pressure as the aircraft changes altitude
●Ex: Flight crew will set cabin altitude at 8000’ (10.92 psi)
●Pressure is established at 8000’ and remains constant as aircraft altitude fluctuates
Differential pressure control
Constant differential pressure is kept by controlling cabin pressure to maintain a pressure difference between the air inside the cabin and ambient air outside the cabin
●Pressure remains lower than max differential pressure which would cause airframe damage
Automatic mode
●Cabin pressure is maintained automatically via the outflow valve which is modulated to maintain pre-programmed cabin altitudes.
●Specific aircraft configuration will cause the outflow valve to open. (Weight on Wheels switch)
●Takeoff abort mode allows the cabin pressure controller to remember the takeoff altitude in case a RTF is required.