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1.发明申请公开(公告)号：US20140216088A1
公开(公告)日：2014-08-07
申请号：US13761081
申请日：2013-02-06
Applicant: RAYTHEON COMPANY
Inventor： Richard M. Weber
Abstract: A system for cooling an aircraft includes a fuel tank, a fuel delivery system, a cooling system, and a heat exchanger. The fuel tank is configured to hold cooled fuel for the aircraft. The fuel delivery system is configured to provide at least a portion of the fuel from the fuel tank to an engine of the aircraft. The cooling system is configured to absorb heat generated by components on the aircraft. The heat exchanger is thermally connected to the fuel delivery system and the cooling system. The heat exchanger is configured to transfer at least a portion of the heat from the components on the aircraft to the cooled fuel. The system may further include a two or three phase expendable liquid system. The expendable liquid system is configured to transfer heat to a frozen or liquid coolant to vaporize and expend the coolant from the aircraft.
Abstract translation: 用于冷却飞行器的系统包括燃料箱，燃料输送系统，冷却系统和热交换器。 燃料箱配置为保持飞机的冷却燃料。 燃料输送系统构造成将来自燃料箱的燃料的至少一部分提供给飞行器的发动机。 冷却系统被配置为吸收飞机上的部件产生的热量。 热交换器热连接到燃料输送系统和冷却系统。 热交换器被配置成将至少一部分热量从飞机上的部件转移到冷却的燃料。 该系统还可以包括两相或三相消耗液体系统。 消耗性液体系统被配置为将热量传递到冷冻或液体冷却剂以蒸发和消耗来自飞行器的冷却剂。
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公开(公告)号：US09725185B2
公开(公告)日：2017-08-08
申请号：US13951515
申请日：2013-07-26
Applicant: Raytheon Company
Inventor： Richard M. Weber , Scott E. Johnson
CPC classification number: B64D41/007 , F01D21/02 , F02C7/32 , F03D1/04 , F03D9/00 , F03D9/25 , F03D9/32 , F05D2220/34 , Y02E10/72
Abstract: A power generation system includes a ram air turbine that is connected to a generator. The power generation system may be located in a pod, for example a pod for mounting on an aircraft. The ram air turbine receives air that passes through an air path through the pod, going in through an air inlet, through the turbine to turn the turbine, and out through an air outlet. The system includes a deployable flow obstruction, such as one or more airbags, that are deployable to suddenly obstruct the flow through the air path. The obstruction may be used to cut off flow (or greatly reduce flow), when overspeed of the ram air turbine is detected. The obstruction deploys (for example, airbags deploy in an air inlet of the system) to prevent continuation of the overspeed operation of the turbine, which may damage parts of the system.
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3.发明授权公开(公告)号：US09561857B2
公开(公告)日：2017-02-07
申请号：US13761081
申请日：2013-02-06
Applicant: Raytheon Company
Inventor： Richard M. Weber
Abstract: A system for cooling an aircraft includes a fuel tank, a fuel delivery system, a cooling system, and a heat exchanger. The fuel tank is configured to hold cooled fuel for the aircraft. The fuel delivery system is configured to provide at least a portion of the fuel from the fuel tank to an engine of the aircraft. The cooling system is configured to absorb heat generated by components on the aircraft. The heat exchanger is thermally connected to the fuel delivery system and the cooling system. The heat exchanger is configured to transfer at least a portion of the heat from the components on the aircraft to the cooled fuel. The system may further include a two or three phase expendable liquid system. The expendable liquid system is configured to transfer heat to a frozen or liquid coolant to vaporize and expend the coolant from the aircraft.
Abstract translation: 用于冷却飞行器的系统包括燃料箱，燃料输送系统，冷却系统和热交换器。 燃料箱配置为保持飞机的冷却燃料。 燃料输送系统构造成将来自燃料箱的燃料的至少一部分提供给飞行器的发动机。 冷却系统被配置为吸收飞机上的部件产生的热量。 热交换器热连接到燃料输送系统和冷却系统。 热交换器被配置成将至少一部分热量从飞机上的部件转移到冷却的燃料。 该系统还可以包括两相或三相消耗液体系统。 消耗性液体系统被配置为将热量传递到冷冻或液体冷却剂以蒸发和消耗来自飞行器的冷却剂。
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公开(公告)号：US20140037423A1
公开(公告)日：2014-02-06
申请号：US13951515
申请日：2013-07-26
Applicant: Raytheon Company
Inventor： Richard M. Weber , Scott E. Johnson
CPC classification number: B64D41/007 , F01D21/02 , F02C7/32 , F03D1/04 , F03D9/00 , F03D9/25 , F03D9/32 , F05D2220/34 , Y02E10/72
Abstract: A power generation system includes a ram air turbine that is connected to a generator. The power generation system may be located in a pod, for example a pod for mounting on an aircraft. The ram air turbine receives air that passes through an air path through the pod, going in through an air inlet, through the turbine to turn the turbine, and out through an air outlet. The system includes a deployable flow obstruction, such as one or more airbags, that are deployable to suddenly obstruct the flow through the air path. The obstruction may be used to cut off flow (or greatly reduce flow), when overspeed of the ram air turbine is detected. The obstruction deploys (for example, airbags deploy in an air inlet of the system) to prevent continuation of the overspeed operation of the turbine, which may damage parts of the system.
Abstract translation: 发电系统包括连接到发电机的冲压空气涡轮机。 发电系统可以位于荚中，例如用于安装在飞行器上的荚。 压头空气涡轮机接收穿过空气通道的空气，通过空气入口通过涡轮进入涡轮以转动涡轮机，并通过出气口排出。 该系统包括可部署的流动障碍物，例如一个或多个安全气囊，其可展开以突然阻塞通过空气路径的流动。 当检测到冲压空气涡轮的超速时，障碍物可用于切断流动（或大大减少流量）。 阻塞部署（例如，安全气囊部署在系统的空气入口中）以防止涡轮机的超速运行的继续，这可能损坏系统的部分。
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