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1. 发明申请

US20170137131A1 Furnishing Item for a Vehicle as well as a Vehicle with such a Furnishing Item 审中-公开
公开(公告)号：US20170137131A1
公开(公告)日：2017-05-18
申请号：US15418900
申请日：2017-01-30
申请人： Airbus Operations GmbH
发明人： Christian Seibt
IPC分类号： B64D11/02 , B64C1/14 , B64D11/06
CPC分类号： B64D11/02 , B60Y2200/50 , B64C1/1407 , B64D11/00 , B64D11/06
摘要： A furnishing item for a vehicle includes a first wall with an access opening situated therein, a door and an oblong flap. The door is arranged on the first wall so that it is swivable relative to the access opening around a first rotational axis. The oblong flap is arranged on the access opening in a vertical direction parallel to the door, and swivelably arranged on a second rotational axis, which is situated on a side of the access opening lying opposite the first rotational axis, and arranged parallel to the first rotational axis. The door and oblong flap extend from the first rotational axis or second rotational axis to the second rotational axis or first rotational axis and together completely close the access opening in a closed state.

2. 发明申请

US20150159968A1 HEAT DISSIPATION SYSTEM FOR AIRCRAFT DRIVE WHEEL DRIVE ASSEMBLY 有权
标题翻译：用于飞机驱动轮驱动装置的散热系统
公开(公告)号：US20150159968A1
公开(公告)日：2015-06-11
申请号：US13615930
申请日：2012-09-14
申请人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
发明人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
IPC分类号： F28F13/00 , B64C25/40
CPC分类号： B64C25/405 , B60K7/0007 , B60K11/02 , B60K2001/006 , B60K2007/0038 , B60K2007/0092 , B60Y2200/50 , B60Y2200/51 , B60Y2306/03 , H02K7/14 , H02K9/19 , Y02T50/823
摘要： A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.
摘要翻译：提供了一种用于在车内非发动机动力的飞机车轮驱动组件上散热的系统，其具有驱动装置，所述驱动装置为一个或多个飞行器轮提供动力，以在地面上自主地驱动飞行器而不直接使用飞机发动机。散热系统与基本上完全安装在鼻子或主起落架轮内的轮驱动组件是一体的。安装在车轮驱动组件的外侧或内侧的储存器增加了热分配质量并且与车轮驱动组件部件流体连通，以便在飞行器地面行驶期间工作温度超过预定最大温度时，在轮驱动组件和储存器之间自动循环传热流体。散热系统可以在现有的飞机上进行改装，以改善热分配，延长轮驱装配和驱动装置的使用寿命。

3. 发明申请

US20180304710A1 DUAL ENGINE AIR AND LAND MULTIMODAL VEHICLE 审中-公开
公开(公告)号：US20180304710A1
公开(公告)日：2018-10-25
申请号：US15889056
申请日：2018-02-05
申请人： SkyRunner, LLC
发明人： Stewart HAMEL
IPC分类号： B60F5/02 , B60K17/22 , B60K17/16 , B64C31/036 , B64C37/00 , B60K5/02
CPC分类号： B60F5/02 , B60K5/02 , B60K17/16 , B60K17/22 , B60Y2200/24 , B60Y2200/50 , B60Y2200/52 , B64C31/036 , B64C37/00
摘要： An air and land multimodal vehicle comprises a frame, a propeller engine attached to a first location of the frame supplying power and torque to a propeller, a ground engine attached to a second location of the frame supplying power and torque to one or more ground traction elements, and a flexible wing releasably connectable to the frame, wherein the propeller engine is vertically and horizontally spaced from the ground engine.

4. 发明申请

US20180278694A1 SYSTEM AND METHOD FOR SERVER BASED CONTROL 审中-公开
公开(公告)号：US20180278694A1
公开(公告)日：2018-09-27
申请号：US15992221
申请日：2018-05-30
申请人： May Patents Ltd.
发明人： Yehuda BINDER , Benjamin MAYTAL
IPC分类号： H04L29/08
CPC分类号： H04L67/12 , B60K31/00 , B60K31/18 , B60Y2200/11 , B60Y2200/12 , B60Y2200/126 , B60Y2200/13 , B60Y2200/30 , B60Y2200/40 , B60Y2200/50 , B60Y2200/90 , G01C21/00 , G06Q2240/00 , G07C5/008 , G08G1/00 , Y04S40/18
摘要： A system and method in a building or vehicle for an actuator operation in response to a sensor according to a control logic, the system comprising a router or a gateway communicating with a device associated with the sensor and a device associated with the actuator over in-building or in-vehicle networks, and an external Internet-connected control server associated with the control logic implementing a PID closed linear control loop and communicating with the router over external network for controlling the in-building or in-vehicle phenomenon. The sensor may be a microphone or a camera, and the system may include voice or image processing as part of the control logic. A redundancy is used by using multiple sensors or actuators, or by using multiple data paths over the building or vehicle internal or external communication. The networks may be wired or wireless, and may be BAN, PAN, LAN, WAN, or home networks.

5. 发明授权

US09956817B2 Wheel assembly tie bolt retention system 有权
公开(公告)号：US09956817B2
公开(公告)日：2018-05-01
申请号：US14615000
申请日：2015-02-05
申请人： GOODRICH CORPORATION
发明人： Jerry Miller
IPC分类号： B60B3/08 , F16B39/04 , B64C25/36 , F16B39/28 , B60B3/00
CPC分类号： B60B3/087 , B60B3/008 , B60B3/08 , B60B2310/305 , B60B2310/306 , B60B2900/325 , B60Y2200/50 , B60Y2200/51 , B64C25/36 , F16B39/04 , F16B39/28
摘要： The present disclosure includes a wheel assembly having a tie bolt retention system. Tie bolt retention systems of the present disclosure include retention holes and retention elements. Retention elements may engage retention holes to prevent loosening or disengagement of a tie nut from the tie bolt.

6. 发明授权

US09597859B2 Self-sealing bladders and related methods 有权
公开(公告)号：US09597859B2
公开(公告)日：2017-03-21
申请号：US14722460
申请日：2015-05-27
申请人： The Boeing Company
发明人： James J. Childress , Mark Stewart Wilenski , Michael Patrick Kozar
IPC分类号： B64D37/06 , B32B25/04 , B64D37/32
CPC分类号： B32B25/042 , B32B3/263 , B32B3/266 , B32B5/06 , B32B7/12 , B32B25/10 , B32B27/12 , B32B27/306 , B32B2260/021 , B32B2262/0269 , B32B2262/0276 , B32B2262/101 , B32B2262/106 , B32B2274/00 , B32B2307/7265 , B32B2307/762 , B32B2439/00 , B32B2581/00 , B32B2605/00 , B32B2605/18 , B60K15/00 , B60K15/03 , B60K2015/03085 , B60K2015/03407 , B60Y2200/50 , B60Y2200/51 , B64D37/06 , B64D37/32
摘要： A self-sealing bladder may automatically seal a puncture wound formed in a bladder wall thereof, such as due to being perforated by a projectile. Self-sealing bladders may be used in containers, such as fuel tanks, in order to prevent loss of fuel or other fluid from the container. Self-sealing bladders may contain a sealant material contained within one or more localized reservoirs formed within the bladder wall, the sealant material being pressurized within the bladder wall such that a localized reduction in pressure due to a perforation in the bladder wall causes the sealant material to migrate to the perforated site, whereupon the sealant material hardens, thereby sealing the wound. The localized reservoirs may include one or more channels and/or connecting layers extending therefrom and in fluid communication therewith, to facilitate migration of the sealant material away from the localized reservoirs and towards the perforated portion of the bladder wall.

7. 发明申请

US20170078400A1 SYSTEM AND METHOD FOR SERVER BASED CONTROL 审中-公开
标题翻译：基于服务器的控制系统与方法
公开(公告)号：US20170078400A1
公开(公告)日：2017-03-16
申请号：US15361434
申请日：2016-11-27
申请人： May Patents Ltd.
发明人： Yehuda BINDER , Benjamin MAYTAL
IPC分类号： H04L29/08
CPC分类号： H04L67/12 , B60K31/00 , B60K31/18 , B60Y2200/11 , B60Y2200/12 , B60Y2200/126 , B60Y2200/13 , B60Y2200/30 , B60Y2200/40 , B60Y2200/50 , B60Y2200/90 , G01C21/00 , G06Q2240/00 , G07C5/008 , G08G1/00 , Y04S40/18
摘要： A system and method in a building or vehicle for an actuator operation in response to a sensor according to a control logic, the system comprising a router or a gateway communicating with a device associated with the sensor and a device associated with the actuator over in-building or in-vehicle networks, and an external Internet-connected control server associated with the control logic implementing a PID closed linear control loop and communicating with the router over external network for controlling the in-building or in-vehicle phenomenon. The sensor may be a microphone or a camera, and the system may include voice or image processing as part of the control logic. A redundancy is used by using multiple sensors or actuators, or by using multiple data paths over the building or vehicle internal or external communication. The networks may be wired or wireless, and may be BAN, PAN, LAN, WAN, or home networks.
摘要翻译：响应于根据控制逻辑的传感器的用于致动器操作的建筑物或车辆中的系统和方法，所述系统包括与与所述传感器相关联的设备通信的路由器或网关以及与所述致动器相关联的设备，建筑物或车载网络，以及与控制逻辑相关联的外部因特网连接的控制服务器，其实现PID闭合线性控制回路并且通过外部网络与路由器通信以控制建筑物内部或车内现象。传感器可以是麦克风或摄像机，并且系统可以包括作为控制逻辑的一部分的语音或图像处理。通过使用多个传感器或执行器或通过在建筑物或车辆内部或外部通信上使用多个数据路径来使用冗余。网络可以是有线或无线的，并且可以是BAN，PAN，LAN，WAN或家庭网络。

8. 发明授权

US09475574B2 Heat dissipation system for aircraft drive wheel drive assembly 有权
标题翻译：飞机驱动轮驱动总成散热系统
公开(公告)号：US09475574B2
公开(公告)日：2016-10-25
申请号：US13615930
申请日：2012-09-14
申请人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
发明人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
IPC分类号： B64C25/40 , H02K9/19 , H02K7/14 , B60K7/00 , B60K1/00 , B60K11/02
CPC分类号： B64C25/405 , B60K7/0007 , B60K11/02 , B60K2001/006 , B60K2007/0038 , B60K2007/0092 , B60Y2200/50 , B60Y2200/51 , B60Y2306/03 , H02K7/14 , H02K9/19 , Y02T50/823
摘要： A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.
摘要翻译：提供了一种用于在车内非发动机动力的飞机车轮驱动组件上散热的系统，其具有驱动装置，所述驱动装置为一个或多个飞行器轮提供动力，以在地面上自主地驱动飞行器而不直接使用飞机发动机。散热系统与基本上完全安装在鼻子或主起落架轮内的轮驱动组件是一体的。安装在车轮驱动组件的外侧或内侧的储存器增加了热分配质量并且与车轮驱动组件部件流体连通，以便在飞行器地面行驶期间工作温度超过预定最大温度时，在轮驱动组件和储存器之间自动循环传热流体。散热系统可以在现有的飞机上进行改装，以改善热分配，延长轮驱装配和驱动装置的使用寿命。

9. 发明申请

US20180266541A1 PLANET-CARRIER FOR AN EPICYCLIC GEARING AND EPICYCLIC GEARING PROVIDED WITH SUCH A PLANET CARRIER 审中-公开
公开(公告)号：US20180266541A1
公开(公告)日：2018-09-20
申请号：US15921490
申请日：2018-03-14
申请人： GE Avio S.r.l.
发明人： Michele GRAVINA , Giuseppe CASAMIRRA
IPC分类号： F16H57/08 , F16H1/28
CPC分类号： F16H57/082 , B60Y2200/50 , B60Y2400/73 , F02C3/107 , F05D2250/73 , F05D2260/40311 , F16H1/28 , F16H1/2809 , F16H2001/289 , F16H2057/085
摘要： A planet-carrier for an epicyclic gearing is provided with a ring having a plurality of plate sectors and a plurality of connection sectors, alternating with one another about a first axis; a connection structure connects in an angularly fixed manner the connection sectors to a rotating member or to a static member; the planet-carrier is also provided with a plurality of pins, which are fixed with respect to the plate sectors and protrude in opposite directions from the plate sectors along respective second axes, parallel and eccentric with respect to the first axis; each pin has two coaxial outer surfaces, adapted to support respective planet gears of the gearing and symmetrical to each other with respect to a symmetry plane orthogonal to the first axis; the plate sectors are asymmetrical with respect to this symmetry plane.

10. 发明申请

US20180115265A1 HYBRID POWER SYSTEM CHARACTERIZATION 审中-公开
公开(公告)号：US20180115265A1
公开(公告)日：2018-04-26
申请号：US15787911
申请日：2017-10-19
申请人： Top Flight Technologies, Inc.
发明人： Samir Nayfeh , Julian Lemus , Soojae Jung , Matthew Sweetland , Long N. Phan
IPC分类号： H02P6/34 , H02P9/04 , H02K11/24 , B64C39/02 , B64D27/24 , B64F5/60 , B60K6/26 , B60K6/24 , B60K6/40 , B60W20/10
CPC分类号： H02P6/34 , B60K6/24 , B60K6/26 , B60K6/40 , B60W20/10 , B60W2050/0026 , B60Y2200/50 , B60Y2200/92 , B60Y2300/60 , B60Y2400/604 , B60Y2400/61 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/108 , B64D27/24 , B64D2027/026 , B64F5/60 , F16C1/02 , G01L5/13 , G01M15/04 , G01M15/05 , H02K11/24 , H02P9/04 , Y02T50/44 , Y02T50/64 , Y10S903/905 , Y10S903/906 , Y10S903/951
摘要： A system includes a torque sensor; and a hybrid power system. The hybrid power sensor includes a frame; an engine mounted on the frame; and a generator, the generator including: a generator rotor mechanically coupled to a shaft of the engine; and a generator stator coupled to the frame by the torque sensor. The torque sensor is configured to measure a torque on the generator stator.

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