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Bombardier Challenger 605 - Air Conditioning & Pressurization
GENERAL
The air conditioning system provides temperature-regulated, conditioned air to the cockpit and passenger cabin using two air conditioning units (ACU’s), commonly referred to as “packs”.
An electric cockpit heating system and an avionics cooling system are also provided.
Aircraft pressurization is accomplished by regulating the overboard discharge of the conditioned air through two outflow valves. The automatic pressurization system maintains cabin pressure to provide passenger comfort throughout all phases of flight within the limitations of the aircraft structure.
During unpressurized flight, ram air may be used to ventilate the cockpit and cabin.
AIR CONDITIONING SYSTEM
Description
The air conditioning system converts 10th-stage bleed air from the engines, APU, or an external source into temperature-regulated pressurized air for distribution to the cockpit and cabin.
The air conditioning system consists of two packs, a temperature control system, distribution ducting, and a ram air system for pack cooling and supplementary ventilation.
A single pack can provide sufficient air to cool and pressurize the aircraft.
Components and Operation
Packs
The packs are located in the aft equipment bay, and are referred to as the left pack and right pack. The L (R) PACK switch/lights on the AIR CONDITIONING panel are used to operate the respective air conditioning pack.
The packs are monitored for overtemperature and overpressure conditions and have automatic protection for both cases.
The left pack is powered by the DC essential bus, and the right pack is powered by DC bus 2. In the event of a double-generator failure when airborne, leading to deployment of the air-driven generator, the left pack remains operational, enabling continued flight at high altitude.
In the event of a single-pack failure, the remaining pack can supply sufficient conditioned air to both compartments.
Pack Pressure Regulation
When the L (R) PACK switch/light is pressed in, the corresponding pressure-regulating shutoff valve (ACU valve) allows bleed air from the 10th-stage manifold to enter the pack. The ACU valves operate in two different modes, low mode or high mode, according to the following conditions:
• Low Mode: Airborne during dual-pack operation, or on the ground with the engines supplying the bleed air, output pressure 24 psig;
庞巴迪挑战者605公务机 培训资料
压缩包里面包括的文件:
7,778,559 CL605-AIRPLANE_GENERAL.pdf
3,362,510 CL605-AIR_CONDITIONING_and_PRESS.pdf
3,607,777 CL605-AURAL_and_VISUAL_WARNING_SYSTEM.pdf
6,119,393 CL605-AUTOMATIC_FLIGHT_CONTROL_SYSTEM.pdf
5,601,155 CL605-AUXILIARY_POWER_UNIT.pdf
2,342,420 CL605-COMMUNICATIONS.pdf
6,116,199 CL605-ELECTRICAL.pdf
2,098,712 CL605-FIRE_PROTECTION.pdf
3,924,271 CL605-FLIGHT_CONTROLS.pdf
5,291,121 CL605-FLIGHT_INSTRUMENTS.pdf
3,400,074 CL605-FUEL_SYSTEM.pdf
2,185,962 CL605-HYDRAULIC_SYSTEM.pdf
1,592,810 CL605-ICE_and_RAIN_PROTECTION.pdf
2,633,855 CL605-LANDING_GEAR.pdf
1,787,840 CL605-LIGHTING.pdf
7,698,337 CL605-NAVIGATION_SYSTEMS.pdf
2,053,024 CL605-PNEUMATIC.pdf
4,224,701 CL605-POWER_PLANT.pdf
18 个文件 71,818,720 字节 |
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