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41. 发明授权

US10124742B2 Fastener apparatus, and methods of use and manufacture thereof 有权
公开(公告)号：US10124742B2
公开(公告)日：2018-11-13
申请号：US15457232
申请日：2017-03-13
申请人： Honda Patents & Technologies North America, LLC.
发明人： Edgar A. Martinez , Nicholas P. Ziraldo
IPC分类号： B60R13/01 , F16B21/07 , F16B5/06
摘要： Some embodiments are directed to a fastener assembly for attaching a cargo liner to a male fastener of a vehicle. The fastener assembly can include a cap defining a substantially cylindrical center portion configured to receive the male fastener therein, and a plurality of tabs each spaced from the cylindrical center portion. The fastener assembly can also include a ring-shaped retainer defining an opening with a plurality of protrusions that each define a ledge configured to receive a corresponding one of the tabs.

42. 发明申请

US20180272927A1 ILLUMINATED GRILLE 审中-公开
公开(公告)号：US20180272927A1
公开(公告)日：2018-09-27
申请号：US15469022
申请日：2017-03-24
申请人： Honda Patents & Technologies North America, LLC
发明人： Daniel Ian MOORE , Nicholas P. ZIRALDO
IPC分类号： B60Q1/26 , F21V5/04 , F21V8/00 , F21V11/00
CPC分类号： B60Q1/2661 , B60R19/52 , B60R2019/525 , G02B6/001
摘要： A grille for a motor vehicle includes a base extending around a perimeter of the grille, a light guide received in the base extending around the perimeter of the grille, a light source for illuminating the light guide when activated, and a lens covering the base and the light guide. A light blocker may mask an interior of the lens except at a portion where light from the light guide is to pass when the light guide is illuminated. A film covers an exterior of the lens and has a predetermined surface appearance when the light guide is not illuminated and allows light to pass through the film upon illumination of the light guide.

43. 发明授权

US10041544B2 Preloading axle clamp for a landing gear wheel bearing and a method of controlling a preloading force on a landing gear wheel bearing 有权
公开(公告)号：US10041544B2
公开(公告)日：2018-08-07
申请号：US14947087
申请日：2015-11-20
申请人： Honda Patents & Technologies North America, LLC
发明人： Charles T. O'Connell
IPC分类号： F16C35/00 , F16C35/063 , B60B27/02 , B60B35/02 , B64C25/36
摘要： A preloading axle clamp for a wheel bearing includes an axle adapted to receive a wheel bearing and a connecting fork. A bushing is positioned about a first end of the axle. A fastener having a first flange is coupled to the first end of the axle, wherein a portion of the fastener is inserted into the first end to retain the connecting fork on the axle. A nut is threadedly coupled to the bushing, wherein rotation of the nut on the bushing causes a preloading force on the wheel bearing.

44. 发明申请

US20140318266A1 FLIGHT CONTROL SYSTEM LOADING TEST APPARATUS AND METHOD 有权
标题翻译：飞行控制系统加载测试装置和方法
公开(公告)号：US20140318266A1
公开(公告)日：2014-10-30
申请号：US13871560
申请日：2013-04-26
申请人： Honda Patents & Technologies North America, LLC
发明人： Toshiaki Fujii , Pascal Brisson , Hiroshi Yamanouchi
IPC分类号： G01M99/00
CPC分类号： G01M5/005
摘要： A flight control system loading test apparatus includes a surface-mounted sector, a cam profile sector, a dummy weight, and a cable. The surface-mounted sector attaches to an aircraft flight control system body such that the surface-mounted sector pivots along with the body about a pivot axis. The cam profile sector is configured to rotate about a rotational axis among a plurality of loading positions. The cam profile sector includes a profile surface having a plurality of curves. Each curve follows a different radius emanating from a respective axis substantially parallel to the rotational axis of the cam profile sector. The cable contacts the cam profile sector along the profile surface. An applied hinge moment using the dummy weight varies as the cam profile sector rotates about the rotational axis.
摘要翻译：飞行控制系统装载测试装置包括表面安装的扇区，凸轮轮廓扇区，虚拟重物和电缆。表面安装的部分附接到飞行器飞行控制系统主体，使得表面安装的扇区与主体一起围绕枢转轴线枢转。凸轮轮廓扇区被配置为围绕多个加载位置之间的旋转轴线旋转。凸轮轮廓扇区包括具有多个曲线的轮廓表面。每个曲线跟随从基本上平行于凸轮轮廓扇区的旋转轴线的相应轴线发出的不同的半径。电缆沿轮廓表面接触凸轮轮廓部分。使用虚拟重物的施加的铰链力矩随着凸轮轮廓扇形围绕旋转轴线旋转而变化。

45. 发明授权

US10745141B2 Electronic rudder bias system 有权
公开(公告)号：US10745141B2
公开(公告)日：2020-08-18
申请号：US15780676
申请日：2016-12-01
申请人： Honda Patents & Technologies North America, LLC
发明人： Jukka Matti Hirvonen , Nilesh Arun Sahani , Jeremy Nathaniel Montgomery
IPC分类号： B64D31/00 , B64D31/10 , B64C13/00 , G05D1/00 , B64C13/16 , B64C13/50 , G05D1/08
摘要： A rudder bias system for an aircraft with a right engine and a left engine includes a component determining a left and right primary and secondary thrust estimates. The system includes a left engine thrust estimate selector determining a left selected estimate based on the left thrust estimates and a right engine thrust estimate selector determining a right selected estimate based on the right thrust estimates. The system includes an enable and mode component determining one or more corresponding validities for the thrust estimates. The system includes a control component generating an engage command based on a thrust differential between the right engine and the left engine, calculated from the left selected estimate and the right selected estimate and a torque command based on an equivalent pedal force assistance calculated as a difference between the thrust differential and an activation threshold.

46. 发明授权

US10723473B2 Method for dynamic command limiting in a distributed control system 有权
公开(公告)号：US10723473B2
公开(公告)日：2020-07-28
申请号：US15780665
申请日：2016-12-01
申请人： Honda Patents & Technologies North America, LLC
发明人： Jukka Matti Hirvonen
IPC分类号： B64D31/08 , B64D31/12 , B64C13/00
摘要： According to one or more aspects, a control system for managing operational limits associated with two or more actuators includes a controller. The controller may continually monitor a first operational limit associated with a first actuator and a first operational limit associated with a second actuator. The controller may determine a first overall distributed control system operating limit based on the first operational limit associated with the first actuator, the first operational limit associated with the second actuator, and a type of operational limit associated with both operational limits.

47. 发明授权

US10023288B2 Aircraft door mechanism with handle actuated descender 有权
公开(公告)号：US10023288B2
公开(公告)日：2018-07-17
申请号：US13664215
申请日：2012-10-30
申请人： Honda Patents & Technologies North America, LLC
发明人： Eugene Petit Harter , Michael T. Hamilton
IPC分类号： B64C1/14 , B64D11/00
摘要： A door assembly for an aircraft includes a partition panel disposed laterally within a fuselage of the aircraft and a descender panel moveably secured to a lower end of the partition panel for selectively closing an aisle opening defined below the partition panel. The door assembly further includes a handle disposed on the partition panel that is operatively connected to the descender panel through a link mechanism such that rotation of the handle is translated into movement of the descender panel to move the descender panel between a retracted position and a deployed position.

48. 发明授权

US09919789B2 Window of an aircraft 有权
公开(公告)号：US09919789B2
公开(公告)日：2018-03-20
申请号：US15401689
申请日：2017-01-09
申请人： Honda Patents & Technologies North America, LLC
发明人： Michimasa Fujino , Yasuhiro Homma
IPC分类号： B64C1/14 , B64D11/02
CPC分类号： B64C1/1484 , B64C1/1492 , B64D11/02
摘要： An aircraft includes a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction. The fuselage defines an aircraft interior. A compartment is located in the interior of the fuselage. The compartment defines an interior area. A first window assembly is mounted to an upper portion of the fuselage for introducing daylight into the interior area. The first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers. The first window assembly includes a window pane, an inner cover and a retainer. The inner cover introduces daylight from the window pane into the interior area. The retainer secures the window pane and the inner cover to the fuselage.

49. 发明申请

US20170146068A1 PRELOADING AXLE CLAMP FOR A LANDING GEAR WHEEL BEARING AND A METHOD OF CONTROLLING A PRELOADING FORCE ON A LANDING GEAR WHEEL BEARING 审中-公开
公开(公告)号：US20170146068A1
公开(公告)日：2017-05-25
申请号：US14947087
申请日：2015-11-20
申请人： Honda Patents & Technologies North America, LLC
发明人： Charles T. O'Connell
IPC分类号： F16C35/063 , B60B35/02 , B64C25/36 , B60B27/02
CPC分类号： F16C35/063 , B60B27/02 , B60B35/02 , B60B2900/131 , B60B2900/133 , B64C25/36 , B64F5/60 , F16C2229/00 , F16C2326/43
摘要： A preloading axle clamp for a wheel bearing includes an axle adapted to receive a wheel bearing and a connecting fork. A bushing is positioned about a first end of the axle. A fastener having a first flange is coupled to the first end of the axle, wherein a portion of the fastener is inserted into the first end to retain the connecting fork on the axle. A nut is threadedly coupled to the bushing, wherein rotation of the nut on the bushing causes a preloading force on the wheel bearing.

50. 发明授权

US09073620B2 Fastening device for window 有权
标题翻译：窗户紧固装置
公开(公告)号：US09073620B2
公开(公告)日：2015-07-07
申请号：US13912579
申请日：2013-06-07
申请人： Honda Patents & Technologies North America, LLC
发明人： Junichi Kondo
IPC分类号： B64C1/06 , B64C1/14 , B63B19/02 , B64G1/22
CPC分类号： B64C1/1492 , B63B19/02 , B63B2019/0038 , B64C1/1484 , B64G1/22 , B64G1/60 , F16B5/02 , F16B19/02
摘要： A fastening assembly for a window of a pressurized fuselage of an aircraft includes a fastener received through a mounting hole defined in the window, an edge attachment member fixing the window to the fuselage, and a bushing assembly embedded in the mounting hole. The bushing assembly includes an inner sleeve bushing radially interposed between the fastener and the window and an outer sleeve bushing radially interposed between the inner sleeve bushing and the window. The inner sleeve bushing is formed from relatively less rigid metal compared with metal of the fastener and the outer sleeve bushing is formed from relatively rigid metal compared with material of the window and the metal of the inner sleeve bushing.
摘要翻译：用于飞行器加压机身的窗户的紧固组件包括通过限定在窗口中的安装孔接收的紧固件，将窗口固定到机身的边缘附接构件以及嵌入安装孔中的衬套组件。衬套组件包括径向介于紧固件和窗口之间的径向插入的内部套筒衬套和径向插入在内部套筒套管和窗户之间的外部套筒衬套。与套筒的金属相比，内衬套由较硬的金属形成，并且外套筒衬套由相对刚性的金属形成，与窗口的材料和内套筒衬套的金属相比。

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