Cabin Atmospheric Control Systems
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Transcript of 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