-
Patent Agency Ranking
公开(公告)号：US10294957B2
公开(公告)日：2019-05-21
申请号：US14885614
申请日：2015-10-16
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Seth E. Rosen , Eric Chrabascz , Mark Vignali , Harold W. Hipsky
Abstract: 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.
-
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。
-
公开(公告)号：US09278759B2
公开(公告)日：2016-03-08
申请号：US13901831
申请日：2013-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Mark Vignali , Luke J. Mayo
CPC classification number: B64D13/02 , B64D13/00 , Y02T50/44 , Y10T29/49826
Abstract: A cross-support bracket for a cabin air compressor assembly includes a mating portion having a first group of apertures at a first end and a second group of apertures at a second end. A reference line is defined between a lowermost primary aperture of the first group of apertures and a lowermost primary aperture of the second group of apertures. A stiffener portion is formed along a lower edge of the mating portion. A curved region is formed in the mating portion between a first and second upper edge of the mating portion. The curved region includes a first curved portion, a substantially straight portion, and a second curved portion. A ratio of a radius of the first and second curved portions of the curved region to a length from the substantially straight portion to the reference line is between 9.06 and 10.19.
Abstract translation: 用于机舱空气压缩机组件的交叉支撑支架包括配合部分，该配合部分在第一端具有第一组孔，在第二端具有第二组孔。 参考线被限定在第一组孔径的最下面的主孔和第二组孔的最下面的一次孔之间。 加强部分沿着配合部分的下边缘形成。 在配合部分的第一和第二上边缘之间的配合部分中形成弯曲区域。 弯曲区域包括第一弯曲部分，大致直线部分和第二弯曲部分。 弯曲区域的第一和第二弯曲部分的半径与从基本上直的部分到参考线的长度的比率在9.06和10.19之间。
-
公开(公告)号：US08955809B2
公开(公告)日：2015-02-17
申请号：US13705490
申请日：2012-12-05
Applicant: Hamilton Sundstrand Corporation
Inventor： Mark Vignali , Brent J. Merritt
Abstract: A mount bracket for use in a cabin air supply system for an aircraft has three legs extending from a cylindrical central bore and at a first axial end of the bracket. There are two legs at an opposed second axial end. A central leg is on the first axial end, and two of the legs are positioned at each of two lateral sides at first and second ends. The legs extend to feet. Strengthening legs connect feet at each of the lateral sides, and to the central leg foot. A thickness of the strengthening legs connected to the central leg is defined as a first dimension. A distance along the first axial end between a laterally outermost portion of the feet at each of the lateral sides is defined as a second dimension. A ratio of the first dimension to the second dimension is between 0.032 and 0.037.
Abstract translation: 用于飞行器的客舱空气供应系统的安装支架具有从圆柱形中心孔和支架的第一轴向端部延伸的三条腿。 在相对的第二轴向端有两个腿。 中心腿在第一轴向端部上，并且两个腿部位于第一和第二端部的两个横向侧面中的每一个处。 腿延伸到脚。 加强腿在每个侧面和中央腿脚连接脚。 连接到中心腿的加强腿的厚度被定义为第一尺寸。 在每个侧面的脚的横向最外部分之间沿着第一轴向端的距离被定义为第二尺寸。 第一尺寸与第二尺寸之比在0.032和0.037之间。
-
公开(公告)号：US20140346302A1
公开(公告)日：2014-11-27
申请号：US13901831
申请日：2013-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： Mark Vignali , Luke J. Mayo
CPC classification number: B64D13/02 , B64D13/00 , Y02T50/44 , Y10T29/49826
Abstract: A cross-support bracket for a cabin air compressor assembly includes a mating portion having a first group of apertures at a first end and a second group of apertures at a second end. A reference line is defined between a lowermost primary aperture of the first group of apertures and a lowermost primary aperture of the second group of apertures. A stiffener portion is formed along a lower edge of the mating portion. A curved region is formed in the mating portion between a first and second upper edge of the mating portion. The curved region includes a first curved portion, a substantially straight portion, and a second curved portion. A ratio of a radius of the first and second curved portions of the curved region to a length from the substantially straight portion to the reference line is between 9.06 and 10.19.
Abstract translation: 用于机舱空气压缩机组件的交叉支撑支架包括配合部分，该配合部分在第一端具有第一组孔，在第二端具有第二组孔。 参考线被限定在第一组孔径的最下面的主孔和第二组孔的最下面的一次孔之间。 加强部分沿着配合部分的下边缘形成。 在配合部分的第一和第二上边缘之间的配合部分中形成弯曲区域。 弯曲区域包括第一弯曲部分，大致直线部分和第二弯曲部分。 弯曲区域的第一和第二弯曲部分的半径与从基本上直的部分到参考线的长度的比率在9.06和10.19之间。
-
-
-
-
Search Results
25
records
(took 0.022 seconds)
