首页> 外国专利> HYBRID ECS ARCHITECTURE TO REDUCE ENGINE BLEED DEPENDENCY FOR AIRCRAFT CABIN PRESSURE AND TEMPERATURE CONTROL

HYBRID ECS ARCHITECTURE TO REDUCE ENGINE BLEED DEPENDENCY FOR AIRCRAFT CABIN PRESSURE AND TEMPERATURE CONTROL

机译:混合ECS架构,以减少发动机流动依赖的飞机舱压力和温度控制

摘要

An environmental control system includes an ambient air conduit and a bleed air conduit, an electric compressor connected to the ambient air conduit and a mechanical compressor connected to the electric compressor. The electric compressor is supported for rotation independent of the mechanical compressor. A turbine is operatively connected to the mechanical compressor, the turbine connected to both the ambient air conduit and the bleed air conduit to provide conditioned air to a conditioned air conduit. Computer program products and methods of providing conditioned air to conditioned air loads are also described.
机译:环境控制系统包括环境空气管道和排出的空气管道,电动压缩机连接到环境空气管道和连接到电动压缩机的机械压缩机。电动压缩机被支撑用于独立于机械压缩机的旋转。涡轮机可操作地连接到机械压缩机,涡轮机连接到环境空气管道和排出的空气管道,以向调节空气管道提供调节空气。还描述了计算机程序产品和向调节空气提供调节空气的方法。

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