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公开(公告)号：US10525485B2
公开(公告)日：2020-01-07
申请号：US15679772
申请日：2017-08-17
Applicant: Hamilton Sundstrand Corporation
Inventor： John D. Monacchio , Murtuza Lokhandwalla , Brian R. Shea , Lance R. Bartosz
Abstract: A water extractor includes an outer duct with an inlet and an outlet, and an inner duct with an inlet and an outlet. The inner duct is positioned in the outer duct. The water extractor further includes a gap between the inner duct and the outer duct. The gap is tapered between a first position and a second position.
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公开(公告)号：US20190015844A1
公开(公告)日：2019-01-17
申请号：US15679772
申请日：2017-08-17
Applicant: Hamilton Sundstrand Corporation
Inventor： John D. Monacchio , Murtuza Lokhandwalla , Brian R. Shea , Lance R. Bartosz
CPC classification number: B04C3/06 , A47L7/00 , A47L7/0009 , A47L9/0411 , B01D45/12 , B01D45/16 , B04C3/00 , B64D13/06 , B64D2013/0662
Abstract: A water extractor includes an outer duct with an inlet and an outlet, and an inner duct with an inlet and an outlet. The inner duct is positioned in the outer duct. The water extractor further includes a gap between the inner duct and the outer duct. The gap is tapered between a first position and a second position.
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公开(公告)号：US20180118352A1
公开(公告)日：2018-05-03
申请号：US15340662
申请日：2016-11-01
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Brian R. Shea
Abstract: An ozone converter includes an outer housing having an inlet and an outlet and a core disposed within the outer housing, the core including a central passageway formed therein and passing thorough the core. The converter also includes an ozone control assembly that allows air to pass through the central passageway in an closed mode and prevents flow thorough the central passageway in an open mode, the assembly including cover flaps that cover a portion of the core in the closed mode and that do not cover the core in the open mode.
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公开(公告)号：US20170144767A1
公开(公告)日：2017-05-25
申请号：US14947328
申请日：2015-11-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Luke J. Mayo , Brian R. Shea
CPC classification number: F28F3/025 , B64D13/06 , B64D2013/0688 , F28D9/0037 , F28D9/0062 , F28D9/0068 , F28D2021/0021 , F28F2215/04 , F28F2250/106
Abstract: A recirculation heat exchanger for use in an environmental control system of an aircraft is provided including a rectangular core having a plurality of alternately stacked first fluid layers and second fluid layers. The rectangular core has a width of about 4.750 inches (12.065 cm), and a length of about 10.6 inches (26.924 cm). A first air header is arranged adjacent a first surface of the core and a second air header is arranged adjacent a second, opposite surface of the core. The first and second air header form a portion of a flow path for a first fluid. A first fluid header is arranged adjacent a third surface and a second fluid header is arranged adjacent a fourth surface of the core. The first and second fluid header form a flow path for the second fluid having a multi-pass configuration.
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公开(公告)号：US20240367801A1
公开(公告)日：2024-11-07
申请号：US18775044
申请日：2024-07-17
Applicant: Hamilton Sundstrand Corporation
Inventor： Brian R. Shea , Peter Zywiak , Luke Martin
Abstract: A method of operating an aircraft air conditioning system is includes delivering cabin air to a lower recirculation heat exchanger included in a lower cooling zone to generate lower cooled recirculated cabin air and delivering the cabin air to an upper recirculation heat exchanger included in an upper cooling zone to generate upper cooled recirculation air. The method further comprising generating power via a power system, and invoking, via the controller, a recirculation ground maintenance mode to command the power system to deliver power to one or both of the lower cooling zone and the upper cooling zone so as to output one or both of the lower cooled recirculated cabin air and the upper cooled recirculated cabin to an aircraft cabin.
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Patent Agency Ranking
公开(公告)号：US12065250B2
公开(公告)日：2024-08-20
申请号：US17116224
申请日：2020-12-09
Applicant: Hamilton Sundstrand Corporation
Inventor： Brian R. Shea , Peter Zywiak , Luke Martin
CPC classification number: B64D13/06 , B64D13/02 , B64D13/08 , B64D41/00 , B64D2013/0611 , B64D2013/0618 , B64D2013/0688
Abstract: An aircraft air conditioning system includes a lower cooling zone and an upper cooling zone. The lower cooling zone includes a lower recirculation heat exchanger configured to receive cabin air from a cabin and convert the cabin air into lower cooled recirculated cabin air. The upper cooling zone includes an upper recirculation heat exchange configured to receive the cabin air from the cabin and convert the cabin air into upper cooled recirculated cabin air. A power system selectively delivers power to the lower cooling zone and the upper cooling zone. A controller is in signal communication with the power system. The controller determines a target temperature of the cabin and invokes a recirculation ground maintenance mode that commands the power system to deliver power to one or both of the lower cooling zone and the upper cooling zone so that a temperature of the cabin reaches the target temperature.
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公开(公告)号：US11529535B2
公开(公告)日：2022-12-20
申请号：US16821389
申请日：2020-03-17
Applicant: Hamilton Sundstrand Corporation
Inventor： Xiaohong Liao , Beakal T. Woldemariam , Brian R. Shea , Earl Jean LaVallee , Eric Surawski
Abstract: Fuel tank inerting systems are described. The systems include a fuel tank, a catalytic reactor arranged to receive a reactant mixture comprising a first reactant and a second reactant to generate an inert gas to be supplied to the fuel tank to fill an ullage space of the fuel tank, a condenser heat exchanger arranged between the catalytic reactor and the fuel tank and configured to cool an output from the catalytic reactor, and a fan assembly arranged within an inerting system flow path upstream of the catalytic reactor, wherein the fan assembly is arranged within a gas flow having a temperature of at least 185° C.
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公开(公告)号：US10766623B2
公开(公告)日：2020-09-08
申请号：US15340662
申请日：2016-11-01
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Brian R. Shea
Abstract: An ozone converter includes an outer housing having an inlet and an outlet and a core disposed within the outer housing, the core including a central passageway formed therein and passing thorough the core. The converter also includes an ozone control assembly that allows air to pass through the central passageway in an closed mode and prevents flow thorough the central passageway in an open mode, the assembly including cover flaps that cover a portion of the core in the closed mode and that do not cover the core in the open mode.
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公开(公告)号：US09745069B2
公开(公告)日：2017-08-29
申请号：US13746073
申请日：2013-01-21
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Brian R. Shea
CPC classification number: B64D15/06 , B64D2013/0666 , B64D2013/0674 , F28D2021/0021 , F28F27/02 , F28F2250/06
Abstract: An air-liquid heat exchanger assembly for an environmental control system of an aircraft includes a heat exchanger, a controller, and a bypass valve. The heat exchanger includes a first chamber and a second chamber. The first chamber has a first inlet that is provided a liquid and a first end that is provided air. The second chamber is arranged adjacent the first chamber. The bypass valve is operably coupled to the controller. The bypass valve having an inlet coupled to a first outlet of the first chamber, a first outlet coupled to a second inlet of the second chamber, and a second outlet coupled to a bypass conduit. The controller adjusts a position of the bypass valve to control the flow of liquid through the second chamber and the bypass conduit.
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公开(公告)号：US20140202663A1
公开(公告)日：2014-07-24
申请号：US13746073
申请日：2013-01-21
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Brian R. Shea
IPC: B64D15/06
CPC classification number: B64D15/06 , B64D2013/0666 , B64D2013/0674 , F28D2021/0021 , F28F27/02 , F28F2250/06
Abstract: An air-liquid heat exchanger assembly for an environmental control system of an aircraft is provided including a heat exchanger configured to transfer heat between air and a liquid. The heat exchanger includes a first chamber and a second chamber arranged generally in series relative to a flow of the liquid. A movable bypass valve is operably coupled to a controller. The bypass valve is positioned between and coupled to the first chamber and the second chamber. The bypass valve is configured to control the flow of the liquid through the second chamber and a bypass conduit in response to measured operating conditions of the assembly.
Abstract translation: 提供了一种用于飞行器的环境控制系统的空气 - 液体热交换器组件，其包括被配置为在空气和液体之间传递热量的热交换器。 热交换器包括第一腔室和第二腔室，第一腔室和第二腔室相对于液体的流动大致串联布置。 可移动旁通阀可操作地联接到控制器。 旁通阀位于第一腔室和第二腔室之间，并连接到第一腔室和第二腔室。 旁通阀配置成响应于测量的组件的操作条件来控制通过第二室的液体流和旁路管道。
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