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21.发明授权公开(公告)号：US10144517B2
公开(公告)日：2018-12-04
申请号：US15604517
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky
Abstract: An airplane is provided. The airplane includes a first medium at a first pressure, a second medium at a second pressure, a third medium at a third pressure; and an air conditioning system. The air conditioning system includes a compressor, a first heat exchanger configured to transfer heat from the first medium to the third medium, a second heat exchanger configured to reject heat from the first medium, a third heat exchanger configured to reject heat from the second medium, a first turbine configured to receive the first medium, and a second turbine configured to receive the second medium.
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公开(公告)号：US09976568B2
公开(公告)日：2018-05-22
申请号：US14507021
申请日：2014-10-06
Applicant: Hamilton Sundstrand Corporation
Inventor： Brent J. Merritt , Harold W. Hipsky
CPC classification number: F04D29/441 , F04D29/4213 , F04D29/444 , F05D2230/60 , F05D2250/51 , F05D2250/52 , Y10T29/49245 , Y10T29/53
Abstract: A diffuser for an air cycle machine defines airflow both to a compressor rotor from the inlet and from the compressor rotor through a plurality of vanes that define radially extending airflow passages. The size and shape of both the inlet and the vanes of the diffuser define and tailor the character of airflow presented to and leaving the compressor rotor to provide a desired change in air flow.
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公开(公告)号：US20170354908A1
公开(公告)日：2017-12-14
申请号：US15176970
申请日：2016-06-08
Applicant: Hamilton Sundstrand Corporation
Inventor： Dilip Prasad , Harold W. Hipsky , Thomas M. Zywiak
IPC: B01D45/06
CPC classification number: B01D45/06 , B01D45/02 , B01D45/04 , B01D45/12 , B01D45/16 , B01D53/26 , B64D13/00 , B64D2013/0603 , B64D2013/0651
Abstract: A particle separation device to remove particulate matter from an exterior air flow for use with an environmental control system includes a curved airflow path with an inner radius and an outer radius, the curved air flow path to receive the exterior air flow, a particle passage disposed along at least one of the inner radius and the outer radius to receive the particulate matter from the exterior air flow, a circumferential volute to receive the particulate matter from the particle passage, and a duct to transport the particulate matter from the circumferential volute to a downstream region.
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公开(公告)号：US20170341760A1
公开(公告)日：2017-11-30
申请号：US15604534
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： David E. Hall , Louis J. Bruno , Harold W. Hipsky
CPC classification number: B64D13/02 , B64D13/06 , B64D13/08 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , F01D1/023 , F01D5/06 , F02C1/02 , F02C6/08 , F04D25/045 , F04D25/06 , F04D29/053 , F05D2220/323 , F05D2220/62 , F05D2260/606 , Y02T50/56
Abstract: An airplane is provided. The airplane includes a compressing device. The compressing device includes a turbine with a first inlet and a second inlet. The turbine provides energy by expanding mediums. The first inlet is configured to receive a first medium of the mediums. The second inlet is configured to receive a second medium of the mediums. The compressing device includes a compressor and a motor. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode. The motor provides a supplementary energy to the compressor
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公开(公告)号：US20170341759A1
公开(公告)日：2017-11-30
申请号：US15604526
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky
CPC classification number: B64D13/02 , B64D13/08 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , F02C1/02 , F02C6/08 , F05D2220/323 , F05D2220/62
Abstract: An airplane is provided. The airplane includes a compressing device including a turbine and a compressor. The turbine includes first and second inlets and provides energy by expanding one or more mediums. The first inlet is receives a first medium of the one or more mediums. The second inlet receives a second medium of the one or more mediums. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode.
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Patent Agency Ranking
公开(公告)号：US20170306786A1
公开(公告)日：2017-10-26
申请号：US15136210
申请日：2016-04-22
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky
Abstract: A system is provided. The system includes a first inlet providing a medium from a source; a compressing device in communication with the first inlet; and at least one heat exchanger. The compressing device includes a compressor that receives the medium and a turbine downstream of the compressor. The system is powered by mechanical power from the medium and by electrical power through a motor. The motor input power is less than or equal to 0.5 kilowatt per pounds per minute of the medium compressed.
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公开(公告)号：US20170144769A1
公开(公告)日：2017-05-25
申请号：US14951818
申请日：2015-11-25
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Craig M. Beers , Christopher McAuliffe , Harold W. Hipsky
CPC classification number: B64D13/08 , B64D13/02 , B64D2013/0651 , F01N13/008 , F01N2560/08 , F04D25/0666 , F16L41/004 , F16L41/008 , F16L41/08 , F25B31/00 , F25B49/022 , F25B2700/193 , G01F1/46 , G01P5/16 , G01P5/165
Abstract: A sensor supply tube assembly is provided for disposition within a compressor outlet through which a main flowpath is defined and a sensor port transversely coupled to the compressor outlet. The sensor supply tube assembly includes first and second tubes. The first tube is formed to direct main flowpath fluid from the compressor outlet and through a portion of the sensor port and includes first and second ends disposed within the sensor port and the compressor outlet, respectively, and a curved section interposed between the first and second ends. The second tube includes a sleeve tightly fittable between the first end and the sensor port and a base. The base has an exterior surface from which the sleeve extends and which is disposed and configured to non-rotatably abut with an interior surface of the compressor outlet.
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公开(公告)号：US20160281721A1
公开(公告)日：2016-09-29
申请号：US14668016
申请日：2015-03-25
Applicant: Hamilton Sundstrand Corporation
Inventor： Donald E. Army, JR. , Harold W. Hipsky , Christopher McAuliffe
IPC: F04D17/16
CPC classification number: F04D17/16 , F04D25/024 , F04D29/5806 , F16C37/00 , F24F5/0085
Abstract: An air cycle machine is provided. The machine includes a housing configured to enable airflow therethrough, a fan disposed within the housing and configured to rotate within the housing, and at least one aperture formed in the housing and configured to allow airflow through the at least one aperture from a cooling airflow path of an air cycle machine and into the housing. The at least one aperture is configured to optimally direct airflow passing therethrough toward the fan.
Abstract translation: 提供一台空气循环机。 机器包括构造成能够使气流通过的壳体，设置在壳体内并被配置为在壳体内旋转的风扇，以及形成在壳体中的至少一个孔，并且构造成允许气流从冷却气流路径通过至少一个孔 的空气循环机并进入壳体。 所述至少一个孔被配置成最佳地将通过其的气流引向风扇。
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公开(公告)号：US20160221122A1
公开(公告)日：2016-08-04
申请号：US14612923
申请日：2015-02-03
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Paul M. D'Orlando , Kiley James Versluys , Colette O. Fennessy , Sergey Mironets , Harold W. Hipsky , Timothy D. DeValve
CPC classification number: F01D9/02 , B22F3/1055 , B22F5/04 , B22F2003/1056 , B23K26/342 , B23K2101/001 , B23P15/006 , B23P15/02 , B23P2700/01 , B33Y10/00 , B33Y30/00 , B33Y80/00 , C23C24/103 , F05D2230/31 , Y02P10/295
Abstract: A method of manufacturing a rotor having a hub and a plurality of vanes extending therefrom includes providing the hub, the hub having an outer surface, and depositing a laser cladding on the hub outer surface to form the plurality of vanes.
Abstract translation: 制造具有轮毂和从其延伸的多个叶片的转子的方法包括提供轮毂，轮毂具有外表面，并且在轮毂外表面上沉积激光包层以形成多个叶片。
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公开(公告)号：US20140357176A1
公开(公告)日：2014-12-04
申请号：US13903460
申请日：2013-05-28
Applicant: Hamilton Sundstrand Corporation
Inventor： Craig M. Beers , Harold W. Hipsky
IPC: B64D13/08
CPC classification number: B64D13/00 , B64D13/06 , B64D2013/0644 , F25B9/004 , Y02T50/56
Abstract: A cabin air compressor assembly that include a cabin air compressor disposed at a compressor inlet and a cabin air compressor motor operably connected to the cabin air compressor. At least one cooling flow inlet is configured to direct a cooling flow through various pathways in the cabin air compressor assembly, including across the cabin air compressor motor. A blower is configured to boost the cooling flow across the cabin air compressor motor, thereby increasing cooling flow provided to the air compressor motor. A static seal plate is downstream of the blower and guides the boosted cooling flow toward a cooling flow exit. In addition, the static seal plate isolates boosted cooling flow from a moving rotor of the cabin air compressor, and also forms part of a containment structure that contains fragments and breakage that may come from the cabin air compressor rotor.
Abstract translation: 一种机舱空气压缩机组件，其包括设置在压缩机入口处的机舱空气压缩机和可操作地连接到机舱空气压缩机的机舱空气压缩机马达。 至少一个冷却流入口构造成引导冷却流通过机舱空气压缩机组件中的各种通路，包括在机舱空气压缩机马达上。 鼓风机被配置为增加机舱空气压缩机马达的冷却流量，从而增加提供给空气压缩机马达的冷却流。 静密封板在鼓风机的下游，并将升压的冷却流向导向冷却流出口。 此外，静密封板隔离来自机舱空气压缩机的移动转子的增强的冷却流，并且还形成包含可能来自机舱空气压缩机转子的碎片和断裂的容纳结构的一部分。
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