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公开(公告)号：US09840333B2
公开(公告)日：2017-12-12
申请号：US14695543
申请日：2015-04-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Paul M. D'Orlando , Donald E. Army, Jr. , Thomas M. Zywiak , Harold W. Hipsky , Erin G. Kline , Richard Rusich , John M. Maljanian, Jr. , Eric Surawski
IPC: B64D13/06
CPC classification number: B64D13/06 , B64D2013/0618 , B64D2013/0648 , B64D2013/0688 , Y02T50/56
Abstract: A system and method that comprises an air cycle machine, a flow of bleed air, at least one heat exchanger, and an inlet configured to supply the flow of the bleed air is provided. The bleed air directly flows from a source to mix with recirculated air downstream of a compressor of the air cycle machine in accordance with a high pressure mode or a recirculation chilling mode. The system and method can also utilize the recirculated air flowing from the chamber to drive or maintain the air cycle machine in accordance with the above modes.
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公开(公告)号：US20170342899A1
公开(公告)日：2017-11-30
申请号：US15604397
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 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：US20170341764A1
公开(公告)日：2017-11-30
申请号：US15604481
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky
Abstract: An air cycle machine is provided. The air cycle machine can be included an environmental control system of an aircraft. The air cycle machine can include a turbine comprising a plurality of inlet gas flow paths, a compressor driven by the turbine from a shaft, and a fan driven by the turbine from the shaft.
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公开(公告)号：US20170341761A1
公开(公告)日：2017-11-30
申请号：US15604455
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky
CPC classification number: B64D13/04 , B64D13/06 , B64D13/08 , B64D2013/0618 , B64D2013/0648 , B64D2013/0688 , Y02T50/56
Abstract: 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：US09783307B2
公开(公告)日：2017-10-10
申请号：US14695537
申请日：2015-04-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Eric Surawski , Donald E. Army, Jr. , Thomas M. Zywiak , Harold W. Hipsky , Erin G. Kline , Richard Rusich , John M. Maljanian, Jr. , Paul M. D'Orlando
IPC: B64D13/06
CPC classification number: B64D13/06 , B64D2013/0618 , B64D2013/0648 , B64D2013/0688 , Y02T50/56
Abstract: A system and method that comprises an air cycle machine, a flow of bleed air, at least one heat exchanger, and an inlet configured to supply the flow of the bleed air is provided. The bleed air directly flows from a source to either a compressor of the air cycle machine or the at least one heat exchanger in accordance with a high pressure, low pressure, or pressure boost operation mode. The system and method also can also utilize recirculated air flowing from the chamber to drive or maintain the air cycle machine in accordance with the above modes.
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Patent Agency Ranking
76.发明申请公开(公告)号：US20160355270A1
公开(公告)日：2016-12-08
申请号：US15176601
申请日：2016-06-08
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Donald E. Army , Thomas M. Zywiak , Harold W. Hipsky , Erin G. Kline
CPC classification number: B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , B64D2013/0662 , Y02T50/56
Abstract: An airplane is provided. The airplane includes a pressurized compartment and an environmental control system. The environmental control system includes a compressing device. The compressing device includes a compressor and a turbine. The airplane also includes a first flow of first medium configured to enter the pressurized compartment and a second flow of the first medium configured to enter the turbine.
Abstract translation: 提供飞机。 飞机包括加压隔间和环境控制系统。 环境控制系统包括压缩装置。 压缩装置包括压缩机和涡轮机。 该飞机还包括构造成进入加压隔间的第一介质的第一流和构造成进入涡轮的第一介质的第二流。
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公开(公告)号：US20160347456A1
公开(公告)日：2016-12-01
申请号：US14721603
申请日：2015-05-26
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Harold W. Hipsky , Donald E. Army, JR. , Erin G. Kline , Christina W. Millot , Paul M. D'Orlando
CPC classification number: B64D13/06 , B64D2013/0648 , F02C6/08
Abstract: An environmental control system (ECS) pack is provided including a primary heat exchanger and a secondary heat exchanger. An air cycle machine is arranged in fluid communication with at least one of the primary and second heat exchanger. The air cycle machine includes a compressor and a plurality of turbines. Discharged cabin air is supplied to at least one of the plurality of turbines to operate the compressor.
Abstract translation: 提供了包括主热交换器和二次热交换器的环境控制系统（ECS）包装。 空气循环机布置成与主和第二热交换器中的至少一个流体连通。 空气循环机包括压缩机和多个涡轮机。 向多个涡轮机中的至少一个提供排出的客舱空气以操作压缩机。
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78.发明申请公开(公告)号：US20160304208A1
公开(公告)日：2016-10-20
申请号：US14688272
申请日：2015-04-16
Applicant: Hamilton Sundstrand Corporation
Inventor： Harold W. Hipsky , Donald E. Army, JR. , Erin G. Kline , Louis J. Bruno , Christina W. Millot
CPC classification number: B64D13/06 , B64D2013/0648 , F01D25/24 , F02C6/08 , Y02T50/56
Abstract: A system that comprises a nozzle arrangement is provided. The nozzle arrangement includes at least one nozzle configured to supply a medium at a nozzle flow rate to a fan of an air cycle machine. The nozzle flow rate provides a pneumatic power assist or a power augmentation to a fan of an air cycle machine. The power augmentation, in accordance with the nozzle flow rate, reduces a need for a flow across a turbine of the air cycle machine.
Abstract translation: 提供了一种包括喷嘴装置的系统。 喷嘴装置包括至少一个喷嘴，其构造成以喷嘴流量向空气循环机的风扇供应介质。 喷嘴流量为空气循环机的风扇提供气动动力辅助或功率增加。 根据喷嘴流量的功率增加减少了对穿过空气循环机的涡轮机的流量的需要。
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公开(公告)号：US20160208823A1
公开(公告)日：2016-07-21
申请号：US14599829
申请日：2015-01-19
Applicant: Hamilton Sundstrand Corporation
Inventor： Eric Chrabascz , Dilip Prasad , Murtuza Lokhandwalla , Harold W. Hipsky
CPC classification number: F04D29/668 , B64D13/00 , B64D41/007 , F04D19/00 , F04D19/002 , F04D25/08 , F04D29/321 , F04D29/326 , F04D29/666 , F05D2230/10 , F05D2230/53
Abstract: A fan rotor for an aircraft environmental control system ram fan is provided. The fan rotor includes central body defining a central axis and a radius having a first radial distance that is defined as a distance from the central axis to an edge of the central body. A plurality of fan blades extend radially from the edge of the central body to a second radial distance, the second radial distance defined as a distance from the central axis to a tip of the fan blades. A shroud extends circumferentially between and connecting each of the plurality of fan blades. The shroud is located at a radial distance from the central axis that is greater than the first radial distance and includes one or more tuning features configured to mistune a vibration of the fan rotor during operation.
Abstract translation: 提供了一种用于飞机环境控制系统压头风扇的风扇转子。 风扇转子包括限定中心轴线的中心体和具有被定义为从中心轴线到中心体边缘的距离的第一径向距离的半径。 多个风扇叶片从中心体的边缘径向延伸到第二径向距离，第二径向距离被定义为从中心轴线到风扇叶片尖端的距离。 护罩在周边之间延伸并连接多个风扇叶片中的每一个。 护罩位于距离中心轴线的径向距离大于第一径向距离处，并且包括被配置为在操作期间消除风扇转子的振动的一个或多个调谐特征。
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公开(公告)号：US20160146511A1
公开(公告)日：2016-05-26
申请号：US14552121
申请日：2014-11-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Harold W. Hipsky , Thomas M. Zywiak
CPC classification number: F25B13/00 , B64D13/06 , F25B43/003
Abstract: An aircraft environmental conditioning system is disclosed that includes an air cycle system for conditioning a flow of hot compressed air by reducing its temperature and pressure. The air cycle system includes a heat exchanger having a heat rejection side in fluid communication with the airflow and a heat absorption side in fluid communication with external unconditioned air. The system also includes an airflow path from an external air inlet to the heat absorption side of the heat exchanger. A centrifugal separator is disposed in the airflow path, and includes a tubular body portion having an inlet that receives airflow, a deflector in the tubular body portion that imparts a vortex motion to airflow in the tubular body portion, and an outlet portion that includes a clean air outlet in fluid communication with the heat absorption side of the heat exchanger and a scavenge air outlet for removing particulate matter.
Abstract translation: 公开了一种飞行器环境调节系统，其包括用于通过降低其温度和压力来调节热压缩空气流的空气循环系统。 空气循环系统包括具有与气流流体连通的排热侧的热交换器和与外部未调节空气流体连通的吸热侧。 该系统还包括从外部空气入口到热交换器的吸热侧的气流路径。 离心分离器设置在气流路径中，并且包括具有容纳气流的入口的管状主体部分，管状主体部分中的偏转器，其对管状主体部分中的气流施加涡流运动，以及出口部分，其包括 与热交换器的吸热侧流体连通的清洁空气出口和用于除去颗粒物质的清除空气出口。
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