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公开(公告)号：US11506121B2
公开(公告)日：2022-11-22
申请号：US15604397
申请日：2017-05-24
发明人： Louis J. Bruno , Harold W. Hipsky
摘要： An airplane is provided. The airplane includes a pressurized medium, a turbine, and a valve. The turbine includes at least one nozzle. The valve is located upstream of the turbine. The valve provides the pressurized medium to the at least one nozzle of the turbine according to an operational mode.
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公开(公告)号：US11047237B2
公开(公告)日：2021-06-29
申请号：US15604440
申请日：2017-05-24
发明人： Louis J. Bruno , Harold W. Hipsky
IPC分类号： F01D1/02 , F01D5/02 , F04D17/02 , F04D27/00 , F04D29/58 , F04D29/44 , F04D29/54 , F02C6/08 , B64D13/06
摘要： A system is provided. The system includes a first medium at a first pressure, a second medium at a second pressure, and a medium conditioning sub-system. The medium conditioning sub-system includes a compressor, a first heat exchanger, a second heat exchanger, and a turbine. The turbine receives the first medium and the second medium.
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公开(公告)号：US10604263B2
公开(公告)日：2020-03-31
申请号：US15604455
申请日：2017-05-24
发明人： Louis J. Bruno , Harold W. Hipsky
摘要： An airplane is provided. The airplane includes a pressurized volume and an air conditioning system. The air conditioning system includes a compressor configured to receive a flow of a first medium, a turbine downstream of the compressor in a flow path of the first medium, a first valve that diverts the flow of the first medium around the turbine, a second valve that provides a second medium to the turbine, and a third valve downstream of the turbine that directs an outlet flow of the turbine towards the pressurized volume and that directs the outlet flow of the turbine away from the pressurized volume.
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公开(公告)号：US10294957B2
公开(公告)日：2019-05-21
申请号：US14885614
申请日：2015-10-16
发明人： Seth E. Rosen , Eric Chrabascz , Mark Vignali , Harold W. Hipsky
摘要： A fan rotor blade extending radially from a hub is described. The fan rotor blade may include first surface and a second surface, where the first surface and second surfaces are respectively defined by a set of X-coordinates, Y-coordinates and Z-coordinates. The X, Y and Z coordinates can be set out in any of Tables T-1, T-2, E-1, and E-2. The X, Y, and Z-coordinates can also be scaled by a predetermined factor, with the X-coordinates are oriented in a tangential direction, the Z-coordinates are oriented in an axial direction, and the Y-coordinates are oriented in a radial direction.
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公开(公告)号：US10232948B2
公开(公告)日：2019-03-19
申请号：US15604506
申请日：2017-05-24
发明人： Louis J. Bruno , Harold W. Hipsky
IPC分类号： F01D5/06 , B64D13/02 , B64D13/06 , B64D13/08 , F01D17/10 , F04D25/04 , F04D29/32 , F04D29/053
摘要： An air conditioning system for an aircraft is provided. The air conditioning system includes a first rotating component and a second rotating component. The first rotating component includes a compressor and a turbine. The compressor pressurizes a first medium. The first turbine receives a mixture of a second medium and a pressurized form of the first medium. The second rotating component includes a fan.
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公开(公告)号：US20190002110A1
公开(公告)日：2019-01-03
申请号：US16110163
申请日：2018-08-23
发明人： Louis J. Bruno , Harold W. Hipsky
IPC分类号： B64D13/08 , F01D5/06 , B64D13/06 , B64D13/02 , F01D17/10 , F04D25/04 , F04D29/053 , F04D29/32
摘要： An air cycle machine for an environmental control system for an aircraft is provided. The air cycle machine includes a compressor configured to compress a first medium, a turbine configured to receive second medium, a mixing point downstream of the compressor and downstream of the turbine; and a shaft mechanically coupling the compressor and the turbine.
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公开(公告)号：US09994322B2
公开(公告)日：2018-06-12
申请号：US14619632
申请日：2015-02-11
发明人： Louis J. Bruno , Donald E. Army, Jr. , Thomas M. Zywiak , Erin G. Kline , Christina W. Millot , Harold W. Hipsky , Paul M. D'Orlando
CPC分类号： B64D13/08 , B64D13/06 , B64D2013/0603 , B64D2013/0618 , Y02T50/56
摘要： A system, which includes a plurality of heat exchangers and a compressing device, is configured to prepare in parallel 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.
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公开(公告)号：US20180045114A1
公开(公告)日：2018-02-15
申请号：US15236085
申请日：2016-08-12
CPC分类号： F02C6/08 , F01D15/10 , F02C3/04 , F02C7/32 , F05D2220/50 , H02K7/1823
摘要： A generator arrangement includes a generator and a pneumatic turbine. The pneumatic turbine is operably connected to the generator. A gas turbine engine compressor section is in fluid communication with the pneumatic turbine through a bleed air conduit to provide pressurized air to the pneumatic turbine for applying mechanical rotation to the generator.
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公开(公告)号：US20170341768A1
公开(公告)日：2017-11-30
申请号：US15605697
申请日：2017-05-25
发明人： Louis J. Bruno , Harold W. Hipsky
CPC分类号： B64D13/08 , B64D13/02 , B64D13/06 , B64D2013/0618 , B64D2013/0648 , B64D2013/0688 , F25B9/004 , F25B9/10 , Y02T50/56
摘要： An airplane is provided. The airplane includes a pressurized volume and an air conditioning system. The pressurized volume provides a first medium. The air conditioning system includes a heat exchanger and a compressor. The heat exchanger transfers heat from a second medium to the first medium. The compressor receives the second medium. The compressor is upstream of the heat exchanger in a flow path of the second medium.
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公开(公告)号：US20170341767A1
公开(公告)日：2017-11-30
申请号：US15604510
申请日：2017-05-24
发明人： Louis J. Bruno , Harold W. Hipsky
CPC分类号： B64D13/08 , B64D13/02 , B64D13/06 , B64D2013/0618 , B64D2013/0648 , F01D5/06 , F01D17/105 , F04D25/045 , F04D29/5826 , F05D2260/213 , F05D2260/606 , Y02T50/56
摘要： An airplane is provided. The airplane includes a first medium, a second medium, and an air conditioning. The air conditioning system includes a first turbine, a compressor, and a mixing point. The compressor is located upstream of the turbine in a flow path of the first medium. The mixing point is a location at which the first medium mixes with the second medium. The mixing point is downstream of the compressor and upstream of the turbine.
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