Cabin Atmospheric Control Systems

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    Cabin Atmospheric ControlSystems

    By: Eric Spoor

    Information in this section was taken from:Transport Category Aircraft Systemsp.2-1through 2-25Aircraft Maintenance and Repairp.506-548

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    Cabin Atmospheric

    Control Systems Heating Systems Cooling Systems Pressurization Systems Oxygen Systems

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    Heating Systems

    Exhaust Heating Systems Combustion Heater Systems Electric Heating Systems Bleed Air Heating Systems

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    Exhaust Heating Systems

    Exhaust heating systems are thesimplest of aircraft heating systems andare used on most light aircraft

    The systems components includeo A heater muff around the exhaust stackso An air scoop to direst ram air into the heater

    muffo Ducting to carry the heated air into the cabin

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    Combustion Heater Systems

    Combustion heaters or surfacecombustion heaters are often used toheat the cabin of larger, more expensiveaircraft

    This type of heater burns the aircrafts

    fuel in a combustion chamber or tube todevelop required heat

    Air flowing around the tube is heated

    and ducted to the cabin

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    Electric Heating Systems

    These systems provide cabin heat whenthe aircraft is on the ground and enginesare not running

    Electric heaters are often used on smallturbo-prop aircraft

    Air is taken from the cabin, passed overelectric heater coils, and returned to thecabin

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    Bleed Air Heating Systems

    Bleed air heating systems are used onunpressurized turbine-engine aircraft

    Extremely hot compressor bleed air isducted into a chamber where it is mixedwith ambient or recirculated air to cool

    the air to a useable temperature This air mixture is then ducted into the

    cabin

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    Bleed Air Heating Systems

    (cont.)

    This system contains several safetyfeatureso Temperature sensors prevent excessive heat

    from entering the cabino Check valves to prevent a loss of

    compressor bleed air when starting theengine and when full power is required

    o Engine sensors eliminate the bleed system ifthe engine becomes inoperative

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    Cabin Cooling Systems

    Aircraft-cooling systems are used to coolair inside the aircraft for passenger andcrew comfort

    There are two basic methods of coolingcabin air, they are:o Freon Vapor-Cycle Cooling Systemso Air-Cycle Cooling Systems

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    Vapor-Cycle Cooling

    Systems Vapor-cycle cooling systems are used

    on reciprocating-engine aircraft and insome small turboprop aircraft

    This is a closed system that uses theevaporation and condensation of freon

    to remove heat from the cabin

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    Air-Cycle Cooling Systems

    Air-cycle cooling systems are used onmodern large turbine-powered aircraft

    These systems use the compressionand expansion of air to adjust thetemperature in passenger and crew

    compartments

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    Cabin Pressurization

    Systems Cabin pressurization provides a

    comfortable environment for passengersand crew while allowing the aircraft to flyat higher altitudes

    Flying at high altitudes is more fuel

    efficient and it allows the aircraft to flyabove most undesirable weatherconditions

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    Aircraft Structures

    If an aircraft is to be pressurized, thepressurized section (pressure vessel) must be

    strong enough to withstand operationalstresses

    In general, the maximum altitude at which anaircraft can fly is limited by the maximum

    allowable cabin differential pressureo Cabin differential pressure is the pressure

    difference between ambient air and the air insidethe pressure vessel

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    Aircraft Structures (cont.)

    The stronger the aircraft structure, the higherthe allowed differential pressure will be

    General cabin pressure differentials allowed bydifferent aircraft types:o Light aircraft approx. 3-5 psio Large reciprocating-engine aircraft approx. 5.5 psio

    Turbine-powered transport aircraft approx. 9psi

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    Sources of Pressurization

    The source of aircraft pressure variesdepending on the type of engineinstalled on the aircraft and aircraftdesign

    Although the specific method of

    pressurizing cabin air varies betweendifferent aircraft, pressurization is alwaysdone, in some form, by the aircraft

    engines

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    Reciprocating Engines

    Reciprocating engines can pressurize cabin airthrough the use of:o Superchargerso Turbochargerso Engine-driven air pumps

    The use on superchargers and turbochargers

    for pressurized air:

    o May introduce fumes and oil into the cabin airo Greatly reduces engine power output

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    Turbine-engines

    Turbine-engine aircraft usually utilizeengine bleed air for pressurization

    In these systems, high pressure air isbled from the turbine-enginescompressor

    This also causes a reduction in enginepower but it is not as significant of a loss

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    Independent Cabin

    Compressors Some aircraft use independent cabin

    compressors for pressurization which are used

    to eliminate the problem of air contamination Independent cabin compressors are driven byeither:o The engine accessory sectiono Turbine-engine bleed air These compressors may use one of two types

    of pumps:o Roots-type positive displacement pumpso

    Centrifugal cabin compressors

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    Pressurization System

    Components Heat exchanger

    o used to cool the hot pressurized air to a usable

    temperature Outflow valveo primary cabin pressure control, regulates the

    amount of pressurized air that is allowed to exit thecabin

    Safety valve (positive pressure relief valve)o prevents cabin over-pressurization by opening

    automatically at a predetermined pressure

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    Pressurization System

    Components (cont.) Negative pressure-relief valve

    o Prevents cabin pressure from going below

    that of the ambient air Dump valve

    o Releases all cabin pressure when aircraftlands

    o Often controlled by landing gear squat switch

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    Oxygen Systems

    Oxygen systems are required on aircraftthat operate for extended periods above10,000 ft

    The two types of oxygen systems areused on private and commercial aircraft

    are:o Stored-gas Oxygen Systemso Chemical or Solid State Oxygen Systems

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    Stored-Gas Oxygen Systems

    Stored-gas oxygen systems use oxygencylinders (bottles) to hold the aircrafts

    oxygen supply Oxygen bottles may be:

    o high-pressureo

    low-pressure

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    Stored-Gas Oxygen Systems

    High-pressure bottleso Contain oxygen at 1800psio Green in color

    o Labeled Aviators Breathing Oxygen

    Low-pressureo Contain oxygen at 450psio Yellow in coloro Labeled Aviators Breathing Oxygen

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    Chemical or Solid State

    Oxygen Systems There are many advantages of using

    solid-state oxygen systemso Safeo Lower in cost than stored-gas systemso Comparatively maintenance free