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公开(公告)号：US10017275B2
公开(公告)日：2018-07-10
申请号：US14705262
申请日：2015-05-06
Applicant: Hamilton Sundstrand Corporation
Inventor： Brent J. Merritt , Calvin R. Parent , Alpesh Patel
CPC classification number: B64F5/40 , B64D13/00 , B64D2013/0644 , Y02T50/56
Abstract: A compressor cross bracket for use in an air supply system for an aircraft comprises a ledge extending away from a main body. The main body has ends at opposed sides and a ditch defined between the ends. Each of the ends have at least one bolt hole which has a diameter. A thickness of the ledge is defined in a direction from which the main body extends from the ledge, with a ratio of the thickness to the diameter being between 0.636 and 0.680. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.
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公开(公告)号：US09511869B2
公开(公告)日：2016-12-06
申请号：US13723398
申请日：2012-12-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Pieter Van Lieu , Mark Vignali , Calvin R. Parent , Brent J. Merritt , Gary T. Luedtke
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0688
Abstract: A mixer has an internal bore with an inlet to a chamber, and an outlet at an opposed end/A duct is connected to receive a recirculated air flow. The duct communicates air into the chamber through recirculating air ports such that the recirculating air can mix with the air from the inlet. The mixer housing has a cockpit outlet for delivering air to a second outlet, with the cockpit output being located axially upstream from the recirculating air ports. An isolator is mounted at an outer periphery of the mixer housing, and has flat sides on each of two circumferentially spaced sides. A belly band is bolted to an outer periphery of the mixer housing and to flat sides of the isolator.
Abstract translation: 混合器具有内孔，其具有到室的入口，并且在相对端/ A管道处的出口被连接以接收再循环的空气流。 管道通过再循环的空气端口将空气进入室，使得再循环空气可以与来自入口的空气混合。 混合器壳体具有用于将空气输送到第二出口的驾驶舱出口，驾驶舱输出位于循环空气端口的轴向上游。 隔离器安装在混合器壳体的外周，并且在两个周向间隔开的侧面中的每一个上具有平坦侧面。 腹部带被螺栓连接到混合器壳体的外周边和隔离器的平坦侧面。
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公开(公告)号：US20220196154A1
公开(公告)日：2022-06-23
申请号：US17689323
申请日：2022-03-08
Applicant: Hamilton Sundstrand Corporation
Inventor： Scott W. Simpson , Calvin R. Parent , David J. Zawilinski
Abstract: A valve member is mounted on a shaft to pivot within a fluid passage. A control selectively moves a piston in a linear direction to control a position of the valve member in the fluid passage. The piston causes a roller pin to move as the piston moves linearly. The roller pin is mounted in crank collars of a crank shaft such that movement of the roller pin causes the crank collars to rotate crank shaft rotating position, and the valve shaft. The roller pin is mounted within the crank collars by bearings. The bearings each have an outer race associated with a crank collar, an inner race associated with the roller pin, and bearing members separate the inner and outer race. There is a spring bias resisting movement of the inner races relative to said roller pin. An anti-ice system is also disclosed.
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公开(公告)号：US11313473B2
公开(公告)日：2022-04-26
申请号：US17012666
申请日：2020-09-04
Applicant: Hamilton Sundstrand Corporation
Inventor： Scott W. Simpson , Calvin R. Parent , David J. Zawilinski
Abstract: A valve member is mounted on a shaft to pivot within a fluid passage. A control selectively moves a piston in a linear direction to control a position of the valve member in the fluid passage. The piston causes a roller pin to move as the piston moves linearly. The roller pin is mounted in crank collars of a crank shaft such that movement of the roller pin causes the crank collars to rotate crank shaft rotating position, and the valve shaft. The roller pin is mounted within the crank collars by bearings. The bearings each have an outer race associated with a crank collar, an inner race associated with the roller pin, and bearing members separate the inner and outer race. There is a spring bias resisting movement of the inner races relative to said roller pin. An anti-ice system is also disclosed.
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Patent Agency Ranking
公开(公告)号：US20220074500A1
公开(公告)日：2022-03-10
申请号：US17012666
申请日：2020-09-04
Applicant: Hamilton Sundstrand Corporation
Inventor： Scott W. Simpson , Calvin R. Parent , David J. Zawilinski
Abstract: A valve member is mounted on a shaft to pivot within a fluid passage. A control selectively moves a piston in a linear direction to control a position of the valve member in the fluid passage. The piston causes a roller pin to move as the piston moves linearly. The roller pin is mounted in crank collars of a crank shaft such that movement of the roller pin causes the crank collars to rotate crank shaft rotating position, and the valve shaft. The roller pin is mounted within the crank collars by bearings. The bearings each have an outer race associated with a crank collar, an inner race associated with the roller pin, and bearing members separate the inner and outer race. There is a spring bias resisting movement of the inner races relative to said roller pin. An anti-ice system is also disclosed.
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公开(公告)号：US20160325840A1
公开(公告)日：2016-11-10
申请号：US14705242
申请日：2015-05-06
Applicant: Hamilton Sundstrand Corporation
Inventor： Brent J. Merritt , Calvin R. Parent , Alpesh Patel
CPC classification number: B64D13/06 , B64D2013/0618 , B64D2013/0648 , Y02T50/56
Abstract: A compressor mount bracket has a mount floor extending to be perpendicular to a square side extending away from the mount floor in a first direction. A closure side extends from the mount floor in the first direction. An outer surface faces away from the square side. An angled side extends at a non-parallel angle from the square side and back over the mount floor. A mount location extends from the angled side, and further over the mount floor. The closure side extends along the angled side and the mount location. The mount location has a first thickness, and the angled side has a second thickness. A ratio of the first thickness to the second thickness is between 1.38 and 1.63. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.
Abstract translation: 压缩机安装支架具有安装底板，其垂直于在第一方向上远离安装地板延伸的方形侧面延伸。 封闭侧沿第一方向从安装地板延伸。 外表面远离方侧。 倾斜的一侧从正方形侧以非平行的角度延伸并且背靠着安装地板。 安装位置从成角度的一侧延伸，并进一步穿过安装地板。 封闭侧沿成角度的一侧和安装位置延伸。 安装位置具有第一厚度，并且倾斜侧具有第二厚度。 第一厚度与第二厚度的比值在1.38和1.63之间。 还公开了一种客舱供气系统和维修客舱空气供应系统的方法。
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公开(公告)号：US10017258B2
公开(公告)日：2018-07-10
申请号：US14705242
申请日：2015-05-06
Applicant: Hamilton Sundstrand Corporation
Inventor： Brent J. Merritt , Calvin R. Parent , Alpesh Patel
CPC classification number: B64D13/06 , B64D2013/0618 , B64D2013/0648 , Y02T50/56
Abstract: A compressor mount bracket has a mount floor extending to be perpendicular to a square side extending away from the mount floor in a first direction. A closure side extends from the mount floor in the first direction. An outer surface faces away from the square side. An angled side extends at a non-parallel angle from the square side and back over the mount floor. A mount location extends from the angled side, and further over the mount floor. The closure side extends along the angled side and the mount location. The mount location has a first thickness, and the angled side has a second thickness. A ratio of the first thickness to the second thickness is between 1.38 and 1.63. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.
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公开(公告)号：US20160327203A1
公开(公告)日：2016-11-10
申请号：US14705262
申请日：2015-05-06
Applicant: Hamilton Sundstrand Corporation
Inventor： Brent J. Merritt , Calvin R. Parent , Alpesh Patel
CPC classification number: B64F5/40 , B64D13/00 , B64D2013/0644 , Y02T50/56
Abstract: A compressor cross bracket for use in an air supply system for an aircraft comprises a ledge extending away from a main body. The main body has ends at opposed sides and a ditch defined between the ends. Each of the ends have at least one bolt hole which has a diameter. A thickness of the ledge is defined in a direction from which the main body extends from the ledge, with a ratio of the thickness to the diameter being between 0.636 and 0.680. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.
Abstract translation: 一种用于飞行器空气供应系统的压缩机十字支架，包括远离主体延伸的凸缘。 主体在相对侧具有端部，并且在端部之间限定沟槽。 每个端部具有至少一个具有直径的螺栓孔。 凸缘的厚度被限定在主体从凸缘延伸的方向上，厚度与直径的比率在0.636和0.680之间。 还公开了一种客舱供气系统和维修客舱空气供应系统的方法。
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公开(公告)号：US20140245775A1
公开(公告)日：2014-09-04
申请号：US13723398
申请日：2012-12-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Pieter Van Lieu , Mark Vignali , Calvin R. Parent , Brent J. Merritt , Gary T. Luedtke
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0688
Abstract: A mixer has an internal bore with an inlet to a chamber, and an outlet at an opposed end/A duct is connected to receive a recirculated air flow. The duct communicates air into the chamber through recirculating air ports such that the recirculating air can mix with the air from the inlet. The mixer housing has a cockpit outlet for delivering air to a second outlet, with the cockpit output being located axially upstream from the recirculating air ports. An isolator is mounted at an outer periphery of the mixer housing, and has flat sides on each of two circumferentially spaced sides. A belly band is bolted to an outer periphery of the mixer housing and to flat sides of the isolator.
Abstract translation: 混合器具有内孔，其具有到室的入口，并且在相对端/ A管道处的出口被连接以接收再循环的空气流。 管道通过再循环的空气端口将空气进入室，使得再循环空气可以与来自入口的空气混合。 混合器壳体具有用于将空气输送到第二出口的驾驶舱出口，驾驶舱输出位于循环空气端口的轴向上游。 隔离器安装在混合器壳体的外周，并且在两个周向间隔开的侧面中的每一个上具有平坦侧面。 腹部带被螺栓连接到混合器壳体的外周边和隔离器的平坦侧面。
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