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

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

机译:一种混合ECS架构,以减少发动机流动依赖性的飞机舱压力和温度控制

摘要

An environmental control system includes an ambient air conduit (104) and a bleed air conduit (102), an electric compressor (110) connected to the ambient air conduit and a mechanical compressor (130) 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导管(104)和排出的空气管道(102),电动压缩机(110),其连接到环境空气管道和连接到电动压缩机的机械压缩机(130)。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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