PRESSURIZED CLOSED COOLING SYSTEM
    1.
    发明申请
    PRESSURIZED CLOSED COOLING SYSTEM 审中-公开
    压缩冷却系统

    公开(公告)号:US20080264084A1

    公开(公告)日:2008-10-30

    申请号:US11740089

    申请日:2007-04-25

    IPC分类号: F28B9/00 F25D9/00

    摘要: An aircraft air conditioning system includes an air supply system (engine bleed or cabin air compressor taking ambient air and pressurizing it at or above cabin pressure) and a cooling system (air cycle or vapor cycle cooling packs to reject heat outside the vessel). These systems can exist as independent systems or combined into a single unit. Air supply and cooling are powered from either engine bleed air or electric power. In order to increase the airflow through the cabin, some cabin air is re-circulated and mixed with fresh air from the air supply system.

    摘要翻译: 飞机空调系统包括空气供应系统(发动机排气或机舱空气压缩机,其承受环境空气并在舱室压力或以上加压)和冷却系统(空气循环或蒸汽循环冷却组件以排除容器外部的热量)。 这些系统可以作为独立系统存在或组合成单个单元。 空气供应和冷却由发动机排气或电力供电。 为了增加通过机舱的气流,一些客舱空气被再循环并与来自供气系统的新鲜空气混合。

    ENVIRONMENTAL CONTROL SYSTEM WITH ADSORPTION BASED WATER REMOVAL
    2.
    发明申请
    ENVIRONMENTAL CONTROL SYSTEM WITH ADSORPTION BASED WATER REMOVAL 审中-公开
    基于吸附水去除的环境控制系统

    公开(公告)号:US20080110193A1

    公开(公告)日:2008-05-15

    申请号:US11751480

    申请日:2007-05-21

    IPC分类号: F25B11/00

    摘要: The present invention includes an adsorbent sub-system to concentrate water vapor from an incoming pressurized air stream to a level that allows efficient water condensation with ambient air as the single cooling source. The heat released when condensing the water is transferred to the ambient air, without affecting the cooling capacity of the system.

    摘要翻译: 本发明包括将来自加压空气流的水蒸汽浓缩到允许与环境空气作为单个冷却源的高效水冷凝的水平的吸附剂子系统。 冷凝水时释放的热量被转移到环境空气中,而不影响系统的冷却能力。

    ECS with 2-stage water separation
    3.
    发明授权
    ECS with 2-stage water separation 失效
    ECS与2级水分离

    公开(公告)号:US06381969B1

    公开(公告)日:2002-05-07

    申请号:US09466329

    申请日:1999-12-17

    IPC分类号: F25B900

    摘要: A two spool environmental control system includes a low pressure spool subsystem comprising a low pressure turbine and a condenser downstream of the low pressure turbine. A high pressure spool subsystem is in air flow communication with the low pressure spool subsystem and includes the condenser, a first water extractor in air communication with the condenser, a high pressure turbine downstream of the condenser, a second water extractor in air flow communication with the condenser, and a reheater downstream of the high pressure turbine.

    摘要翻译: 两个卷轴环境控制系统包括低压卷轴子系统,其包括低压涡轮机和低压涡轮机下游的冷凝器。 高压阀芯子系统与低压阀芯子系统进行空气流动连通,并且包括冷凝器,与冷凝器空气连通的第一抽水机,冷凝器下游的高压涡轮机,第二抽水机与空气流连通 冷凝器和高压涡轮机下游的再热器。

    Air cycle environmental control systems with two stage compression and
expansion and separate ambient air fan
    4.
    发明授权
    Air cycle environmental control systems with two stage compression and expansion and separate ambient air fan 失效
    空气循环环境控制系统具有两级压缩和扩展和独立的环境空气风扇

    公开(公告)号:US6128909A

    公开(公告)日:2000-10-10

    申请号:US324306

    申请日:1999-06-02

    IPC分类号: B64D13/06 F25B9/00

    摘要: An environmental control system provides for two stage compression and expansion of a bleed air within a cooling cycle, while allowing for a separately driven fan to handle ambient air as a heat sink. The system comprises a plurality of compressors capable of compressing a water vapor bearing air to produce a compressed air. A reheater is capable of cooling the compressed air. A condenser is in flow communication with the reheater, with the condenser being capable of condensing the water vapor. A water extractor is in flow communication with and intermediate of the condenser and the reheater. A plurality of turbines are in flow communication with and downstream of the reheater.

    摘要翻译: 环境控制系统在冷却循环中提供两级压缩和膨胀放气,同时允许单独驱动的风扇来处理环境空气作为散热器。 该系统包括能够压缩含水蒸气的空气以产生压缩空气的多个压缩机。 再热器能够冷却压缩空气。 冷凝器与再热器流动连通,冷凝器能够冷凝水蒸气。 抽水器与冷凝器和再热器流体连通并且与中间体连通。 多个涡轮机与再热器流体连通和下游。

    Augmented catalytic heat exchanger system
    5.
    发明授权
    Augmented catalytic heat exchanger system 失效
    增强催化热交换器系统

    公开(公告)号:US07250141B2

    公开(公告)日:2007-07-31

    申请号:US10789692

    申请日:2004-02-27

    IPC分类号: B01D50/00

    摘要: Systems, apparatus, and methods for the catalytic removal of at least one pollutant from an air stream via a catalytic precooler arranged in series with at least one augmentative catalytic device. The augmentative catalytic device may be located upstream or downstream from the catalytic precooler. The augmentative catalytic device may be integrated with the catalytic precooler, thereby eliminating the need for a separate housing and minimizing weight. Alternatively, the augmentative catalytic device may be disposed within a separate housing, thereby facilitating access for maintenance and decreasing direct maintenance costs.

    摘要翻译: 用于通过与至少一个增强催化装置串联布置的催化预冷器从气流中催化除去至少一种污染物的系统,装置和方法。 增量催化装置可以位于催化预冷器的上游或下游。 增强催化装置可以与催化预冷器一体化,从而不需要单独的壳体并使重量最小化。 或者,增强催化装置可以设置在单独的壳体内,从而便于进行维护并降低直接维护成本。

    Smart hybrid electric and bleed architecture
    8.
    发明授权
    Smart hybrid electric and bleed architecture 失效
    智能混合电力和流体结构

    公开(公告)号:US07970497B2

    公开(公告)日:2011-06-28

    申请号:US11681686

    申请日:2007-03-02

    IPC分类号: G01C23/00

    摘要: An aircraft architecture may be designed to create an optimal balance between electric power and bleed power in order to match or improve current more electric architecture (MEA) performance while simplifying power extraction from the engines as well as simplifying the electrical system. Conventional aircraft architectures may use electric only ECS and cabin pressurization systems (so-called “no bleed” systems). Alternatively, older conventional aircraft may use strictly engine bleed air to provide power for ECS and cabin pressurization systems. The present invention, on the other hand, provides an architecture which may optimize the use of both engine bleed air and MEA designs to provide a system that may be simpler and potentially more reliable and available as compared to conventional aircraft architectures.

    摘要翻译: 飞机架构可以设计成在电力和泄放功率之间创建最佳平衡,以便匹配或改善当前更多的电气结构(MEA)性能,同时简化从发动机的功率提取以及简化电气系统。 传统的飞行器架构可以仅使用电动ECS和客舱加压系统(所谓的“无出血”系统)。 或者,较旧的常规飞行器可以严格地使用发动机排气来为ECS和客舱加压系统提供动力。 另一方面,本发明提供了一种架构,其可以优化发动机放气和MEA设计的使用,以提供与常规飞行器架构相比可以更简单并且可能更可靠和可用的系统。

    SMART HYBRID ELECTRIC AND BLEED ARCHITECTURE
    9.
    发明申请
    SMART HYBRID ELECTRIC AND BLEED ARCHITECTURE 失效
    智能混合电动和结构建筑

    公开(公告)号:US20090326737A1

    公开(公告)日:2009-12-31

    申请号:US11681686

    申请日:2007-03-02

    IPC分类号: B64D13/04 G06F7/00

    摘要: An aircraft architecture may be designed to create an optimal balance between electric power and bleed power in order to match or improve current more electric architecture (MEA) performance while simplifying power extraction from the engines as well as simplifying the electrical system. Conventional aircraft architectures may use electric only ECS and cabin pressurization systems (so-called “no bleed” systems). Alternatively, older conventional aircraft may use strictly engine bleed air to provide power for ECS and cabin pressurization systems. The present invention, on the other hand, provides an architecture which may optimize the use of both engine bleed air and MEA designs to provide a system that may be simpler and potentially more reliable and available as compared to conventional aircraft architectures.

    摘要翻译: 飞机架构可以设计成在电力和泄放功率之间创建最佳平衡,以便匹配或改善当前更多的电气结构(MEA)性能,同时简化从发动机的功率提取以及简化电气系统。 传统的飞行器架构可以仅使用电动ECS和客舱加压系统(所谓的“无出血”系统)。 或者,较旧的常规飞行器可以严格地使用发动机排气来为ECS和客舱加压系统提供动力。 另一方面,本发明提供了一种架构,其可以优化发动机放气和MEA设计的使用,以提供与常规飞行器架构相比可以更简单并且可能更可靠和可用的系统。