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ARP292C
Environmental Control Systems for Helicopters
Environmental Control Systems for Helicopters
2008-11-01
有效
【范围】 This ARP discusses design philosophy, system and equipment requirements, environmental conditions, and design considerations for helicopter environmental control systems (ECS). The helicopter ECS comprises that arrangement of equipment, controls, and indicators which supply and distribute dehumidified conditioned air for ventilation, cooling and heating of the occupied compartments, and cooling of the avionics. The principal features of the system are: a. A controlled fresh air supply b. A means for cooling (air or vapor cycle units and heat exchangers) c. A means for removing excess moisture from the air supply d. A means for heating e. A temperature control system f. A conditioned air distribution system The ARP is applicable to both civil and military helicopters where an ECS is specified; however, certain requirements peculiar to military applications, such as nuclear, biological and chemical (NBC) protection, are not covered. The integration of NBC protection into aircraft ECS is discussed in AIR4362. 1.1 Purpose: The purpose of this ARP is to provide the guidelines and requirements for analysis, design, and installation of helicopter ECS.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

Air Conditioning Systems for Subsonic Airplanes
Heater
Aircraft Compartment Automatic Temperature Control Equipment
High Temperature Pneumatic Duct Systems for Aircraft
General Requirements for Application of Vapor Cycle Refrigeration Systems for Aircraft
Aircraft Electrical Heating Systems
Guide for Qualification of Aircraft Air Valves
Environmental Control System Contamination
Engine Bleed Air Systems for Aircraft
Environmental Control Systems Life Cycle Cost
Acoustic Environment
Air Cycle Air Conditioning Systems for Military Air Vehicles
NBC Consideration for ECS Design
Procedure for Sampling and Measurement of Engine Generated Contaminants in Bleed Air Supplies From Aircraft Engines Under Normal Operating Conditions
Heater
Environmental Control
Environmental Control Systems
Bleed Air Systems
Climatic Extremes for Military Equipment
Environmental Test Methods for Aerospace and Ground Equipment
Human Engineering Design Criteria for Military Systems
Connection
Extreme Climatic Conditions and Derived Conditions for Use in Defining Design/ Test Criteria for NATO Forces Material
Air Conditioning Connections
Air Cabin Pressurizing Test Connections
Pneumatic Starting Nipple
Characteristics of Conditioned Breathable Air Supplied to Aircraft on the Ground
Environmental Conditions and Test Procedures for Airborne Equipment

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(R) Control of Water Carryover from the Environmental Control System and Condensation on the Structure
Construction and Calibration of Parallel Plate Transmission Line for Electromagnetic Interference Susceptibility Testing
Installation of Liquid Oxygen Systems in Civil Aircraft
Anti Blow-By Design Practice for Cap Seals
Fault Isolation in Environmental Control Systems of Commercial Transports
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包含图表

Part 27 and Part 29
Vapor Cycle System C
Air Cycle System ACM
Air Cycle System Wat
Air Cycle Integral R
NATO Standardization
Design Temperatures
Design Humidity for
Joint Values of High

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