RECIRCULATION SYSTEM FOR PARALLEL RAM HEAT EXCHANGERS
    131.
    发明申请
    RECIRCULATION SYSTEM FOR PARALLEL RAM HEAT EXCHANGERS 有权
    并行RAM热交换器的再循环系统

    公开(公告)号:US20160355267A1

    公开(公告)日:2016-12-08

    申请号:US14732157

    申请日:2015-06-05

    Abstract: A system includes an inlet line configured to receive a medium flowing from a low-pressure location of an engine to a chamber, a plurality of heat exchangers configured to receive the medium from the inlet line, and a valve located upstream from the plurality of heat exchangers. The valve is configured to divide in parallel the medium across at least a first heat exchanger and a second heat exchanger of the plurality of heat exchangers. A recirculation air system is configured to supply a recirculation

    Abstract translation: 一种系统包括入口管线,其构造成接收从发动机的低压位置流向腔室的介质;多个热交换器,被配置为从入口管线接收介质;以及阀,其位于多个热量的上游 交换器。 阀构造成在多个热交换器中的至少第一热交换器和第二热交换器之间并联分配介质。 再循环空气系统被配置为提供再循环

    ENVIRONMENTAL CONTROL SYSTEM UTILIZING CABIN AIR TO DRIVE A POWER TURBINE OF AN AIR CYCLE MACHINE
    134.
    发明申请
    ENVIRONMENTAL CONTROL SYSTEM UTILIZING CABIN AIR TO DRIVE A POWER TURBINE OF AN AIR CYCLE MACHINE 审中-公开
    环境控制系统利用空气空气驱动空气循环机的动力涡轮机

    公开(公告)号:US20160144965A1

    公开(公告)日:2016-05-26

    申请号:US14553012

    申请日:2014-11-25

    Abstract: A system, which includes a plurality of heat exchangers and a compressing device, prepares a medium bled from a low-pressure location of an engine and flowing through a plurality of heat exchangers into a chamber. The compressing device is in communication with the plurality of heat exchangers and regulates a pressure of the medium flowing through the plurality of heat exchangers. The compressing device includes a turbine that provides supplemental power to the compressing device based on a pressure of the medium in the chamber.

    Abstract translation: 包括多个热交换器和压缩装置的系统从发动机的低压位置准备介质,并且流过多个热交换器进入腔室。 压缩装置与多个热交换器连通,并且调节流过多个热交换器的介质的压力。 压缩装置包括涡轮机,其基于腔室中的介质的压力向压缩装置提供补充功率。

    COLD CORNER FLOW BAFFLE
    135.
    发明申请
    COLD CORNER FLOW BAFFLE 审中-公开
    冷拐角流

    公开(公告)号:US20160131431A1

    公开(公告)日:2016-05-12

    申请号:US14996459

    申请日:2016-01-15

    Abstract: A heat exchanger for an aircraft includes a hot fluid inlet, a hot fluid outlet, a cold fluid inlet, a cold fluid outlet, and a header connected to the hot fluid outlet. The header includes a housing defining a header volume and a baffle separating the header volume into a first volume and a second volume, wherein the first volume and the second volume are in fluid communication with each other.

    Abstract translation: 用于飞机的热交换器包括热流体入口,热流体出口,冷流体入口,冷流体出口和连接到热流体出口的集管。 集管包括限定集管容积的壳体和将集管体积分成第一体积和第二体积的挡板,其中第一体积和第二体积彼此流体连通。

    ENVIRONMENTAL CONTROL SYSTEM UTILIZING SHOESTRING CYCLE TO MAXIMIZE EFFICIENCY
    136.
    发明申请
    ENVIRONMENTAL CONTROL SYSTEM UTILIZING SHOESTRING CYCLE TO MAXIMIZE EFFICIENCY 有权
    环境控制系统利用鞋袜周期实现最大化效率

    公开(公告)号:US20150307196A1

    公开(公告)日:2015-10-29

    申请号:US14695611

    申请日:2015-04-24

    Inventor: Louis J. Bruno

    Abstract: A method for providing recirculation air to an environmental control system is provided. The method includes supplying via an inlet a flow of bleed air to the environmental control system at a first energy, providing the bleed air from the environmental control system at a second energy into a chamber, and providing the recirculation air to the environmental control system by recirculating the bleed air at a third energy from the chamber to an air cycle machine.

    Abstract translation: 提供了一种向环境控制系统提供再循环空气的方法。 该方法包括以一种第一能量经由入口将排放空气流供给环境控制系统,将来自环境控制系统的排出空气以第二能量提供到室中,并且通过以下方式将再循环空气提供给环境控制系统: 将来自腔室的第三能量的排出空气循环到空气循环机器。

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM SELECTIVELY POWERED BY THREE BLEED REPORTS
    137.
    发明申请
    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM SELECTIVELY POWERED BY THREE BLEED REPORTS 审中-公开
    飞机环保控制系统由三份报告提供

    公开(公告)号:US20150307183A1

    公开(公告)日:2015-10-29

    申请号:US14755929

    申请日:2015-06-30

    Abstract: An engine compressor bleed system of an engine for an aircraft is provided including a plurality of compressor pressure ports configured to supply bleed air to satisfy a cooling load for at least a first stage of a flight profile of an aircraft. A first pressure port of the plurality of compressor pressure ports is configured to provide bleed air having a pressure at least equal to a cabin pressure of an aircraft and a temperature that does not exceed a predetermined threshold.

    Abstract translation: 提供了一种用于飞行器的发动机的发动机压缩机排放系统,其包括多个压缩机压力端口,所述多个压缩压力端口被配置为提供放气以满足飞行器的飞行剖面的至少第一级的冷却负载。 多个压缩机压力端口的第一压力端口被配置为提供具有至少等于飞行器的舱室压力的压力和不超过预定阈值的温度的排气。

    INTERCOMPRESSOR BLEED TURBO COMPRESSOR
    138.
    发明申请
    INTERCOMPRESSOR BLEED TURBO COMPRESSOR 审中-公开
    INTERCOMPRESSOR BLEED涡轮压缩机

    公开(公告)号:US20150065023A1

    公开(公告)日:2015-03-05

    申请号:US14472686

    申请日:2014-08-29

    Inventor: Louis J. Bruno

    Abstract: A bleed system that comprises a bleed inter-compressor fluidly coupled to a low pressure port of the bleed system and configured to utilize a portion of a medium received from the low pressure port to increase the pressure of another portion of that medium. A turbine of the bleed inter-compressor is coupled to a compressor of the bleed inter-compressor and drives the compressor via a shaft, so as to regulate the pressure of the medium.

    Abstract translation: 一种排放系统,其包括流体耦合到所述排放系统的低压端口并且被配置为利用从所述低压端口接收的介质的一部分来增加所述介质的另一部分的压力。 排放压缩机的涡轮机联接到排放压缩机的压缩机,并通过轴驱动压缩机,以便调节介质的压力。

    METHOD OF OPERATING A MULTI-PACK ENVIROMENTAL CONTROL SYSTEM
    139.
    发明申请
    METHOD OF OPERATING A MULTI-PACK ENVIROMENTAL CONTROL SYSTEM 有权
    多重环境控制系统的运行方法

    公开(公告)号:US20150059397A1

    公开(公告)日:2015-03-05

    申请号:US14088549

    申请日:2013-11-25

    CPC classification number: B64D13/06 B64D2013/0603 B64D2013/0614 Y02T50/56

    Abstract: An environmental control system (ECS) pack is provided including a primary heat exchanger, a secondary heat exchanger, and an air cycle machine. The air cycle machine includes a compressor and a turbine. The compressor is fluidly coupled to an outlet of the primary heat exchanger and to an inlet of the secondary heat exchanger. The outlet of the secondary heat exchanger is fluidly coupled to the turbine. A first conduit connects the outlet of the primary heat exchanger and the inlet of the secondary heat exchanger. The first conduit includes a first valve. A second conduit connects the outlet of the secondary heat exchanger to an air load. The second conduit includes a second valve.

    Abstract translation: 提供了包括主热交换器,二次热交换器和空气循环机的环境控制系统(ECS)包装。 空气循环机包括压缩机和涡轮机。 压缩机流体耦合到主热交换器的出口和二次热交换器的入口。 二次热交换器的出口流体地联接到涡轮机。 第一导管连接主热交换器的出口和二次热交换器的入口。 第一导管包括第一阀。 第二导管将二次热交换器的出口连接到空气负载。 第二导管包括第二阀。

    LOW PRESSURE COMPRESSOR BLEED EXIT FOR AN AIRCRAFT PRESSURIZATION SYSTEM
    140.
    发明申请
    LOW PRESSURE COMPRESSOR BLEED EXIT FOR AN AIRCRAFT PRESSURIZATION SYSTEM 审中-公开
    低压压缩机出口飞机升压系统

    公开(公告)号:US20140196469A1

    公开(公告)日:2014-07-17

    申请号:US14212136

    申请日:2014-03-14

    CPC classification number: B64D13/02 B64D13/06 B64D2013/0618 Y02T50/56

    Abstract: An aircraft pressurization system, includes an auxiliary compressor for further compressing compressed air received from a low pressure compressor section of a gas turbine engine while the compressed air is below a predetermined pressure level; a bleed passage for fluidically connecting the auxiliary compressor to the low pressure compressor section; and an environmental control system coupled to an output of the auxiliary compressor for conditioning the compressed air to a predetermined level.

    Abstract translation: 一种飞机加压系统,包括辅助压缩机,用于在压缩空气低于预定压力水平时进一步压缩从燃气涡轮发动机的低压压缩机部分接收的压缩空气; 用于将辅助压缩机流体连接到低压压缩机部分的排放通道; 以及耦合到辅助压缩机的输出的环境控制系统,用于将压缩空气调节到预定水平。

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