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公开(公告)号：US11970022B2
公开(公告)日：2024-04-30
申请号：US16194804
申请日：2018-11-19
Applicant: SAFRAN LANDING SYSTEMS
Inventor： Pierrick Soubrant , Michaël Arnoux
CPC classification number: B60B21/02 , B60B21/026 , B60B25/002 , B64C25/36 , B60B21/023 , B60B21/04 , B60B21/08 , B60B2900/513 , B60Y2200/50 , B60Y2200/51
Abstract: A rim for a braked aircraft wheel includes an outer circular portion whose ends are terminated flanges for receiving a tire. The outer circular portion is connected by a wheel disk to a hub for fitting on an undercarriage axle in order to rotate about an axis of rotation coinciding with a central axis of the rim. The rim is designed to receive the tire on the outside of the outer circular portion and a brake on the inside of the outer circular portion, the outer circular portion presenting on one side of the wheel disk that is to receive the brake, in a plane containing the central axis of the wheel, a profile that has two slopes forming non-zero angles with the central axis, the two slopes extending in the continuation of one another from the wheel disk to the corresponding flange and flaring towards said corresponding flange.
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公开(公告)号：US20230322022A1
公开(公告)日：2023-10-12
申请号：US17717424
申请日：2022-04-11
Applicant: Jerry White, Jr.
Inventor： Jerry White, Jr.
CPC classification number: B60B31/04 , B60B25/002 , B60B2320/14 , B60B2310/305 , B60B2900/3314 , B60Y2200/50 , B60B2900/212
Abstract: A device and method for assisting a user in aircraft wheel assemblies is disclosed herein. The device enables a single user to readily connect two wheel sections in a split wheel assembly. The device is lightweight and reusable and preferably includes two bushings, two washers, a bolt, and a nut. After inserting the bolt through the wheel sections, a nut can be tightened, thereby creating a compressive force that compresses the bushings and the wheel sections together. While the wheel sections are compressed together, a plurality of tie bolts and tie nuts can be installed on the wheel sections to complete the wheel assembly.
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3.发明申请
公开(公告)号：US20180266541A1
公开(公告)日：2018-09-20
申请号：US15921490
申请日：2018-03-14
Applicant: GE Avio S.r.l.
Inventor： Michele GRAVINA , Giuseppe CASAMIRRA
CPC classification number: F16H57/082 , B60Y2200/50 , B60Y2400/73 , F02C3/107 , F05D2250/73 , F05D2260/40311 , F16H1/28 , F16H1/2809 , F16H2001/289 , F16H2057/085
Abstract: 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.
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公开(公告)号：US20180115265A1
公开(公告)日：2018-04-26
申请号：US15787911
申请日：2017-10-19
Applicant: Top Flight Technologies, Inc.
Inventor： Samir Nayfeh , Julian Lemus , Soojae Jung , Matthew Sweetland , Long N. Phan
IPC: H02P6/34 , H02P9/04 , H02K11/24 , B64C39/02 , B64D27/24 , B64F5/60 , B60K6/26 , B60K6/24 , B60K6/40 , B60W20/10
CPC classification number: 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
Abstract: 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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公开(公告)号：US20180069254A1
公开(公告)日：2018-03-08
申请号：US15378755
申请日：2016-12-14
Applicant: Hyundai Motor Company
Inventor： Kyu Il Lee , Jae Yeong Yoo , Sung Suk Ok
IPC: H01M8/04858 , H01M16/00 , H01M8/04303 , H01M8/04955 , H01M8/04992 , B60L11/18
CPC classification number: H01M8/04873 , B60L11/1812 , B60L11/1885 , B60L11/1887 , B60L2240/527 , B60Y2200/11 , B60Y2200/143 , B60Y2200/50 , B60Y2200/91 , B60Y2200/92 , H01M8/04302 , H01M8/04303 , H01M8/04955 , H01M8/04992 , H01M16/003 , H01M16/006 , H01M2250/20
Abstract: A shut down system of a fuel cell vehicle includes: a fuel cell configured to output a high voltage; a rechargeable high voltage battery; a bidirectional converter arranged between an output terminal of the fuel cell and the high voltage battery; a first relay arranged between the fuel cell and the bidirectional converter; and a controller configured to control a voltage of the bidirectional converter when the fuel cell vehicle stalls to reduce a voltage of the output terminal of the fuel cell and turn off the first relay when a voltage value of the output terminal of the fuel cell is below a preset voltage reference value.
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公开(公告)号：US20180034912A1
公开(公告)日：2018-02-01
申请号：US15716881
申请日：2017-09-27
Applicant: May Patents Ltd.
Inventor： Yehuda BINDER , Benjamin MAYTAL
IPC: H04L29/08
CPC classification number: 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
Abstract: 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.
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7.发明申请
公开(公告)号：US20170349268A1
公开(公告)日：2017-12-07
申请号：US15169879
申请日：2016-06-01
Applicant: The Boeing Company
Inventor： Michael J. Duffy , Rene Woszidlo
CPC classification number: B64C21/04 , B60Y2200/11 , B60Y2200/114 , B60Y2200/14 , B60Y2200/143 , B60Y2200/30 , B60Y2200/50 , B62D35/00 , B63B1/32 , B63G8/00 , B64C5/02 , B64C9/14 , B64C21/06 , B64C21/08 , B64C2009/005 , B64C2230/04 , B64C2230/06 , Y02T50/166
Abstract: A method and apparatus for controlling an airflow. The method draws air through a group of inlets. The group of inlets is located in a group of locations on the vehicle such that the group of inlets actively controls the airflow relative to an aircraft when drawing the air. The method compresses the air drawn by the group of inlets in a group of air compressor units located in an aircraft structure to form pressurized air. Further, the method sends the pressurized air through a group of exit ports in the aircraft structure. The pressurized air flowing out of the group of exit ports actively controls the airflow for an aircraft, enabling an improved performance of the aircraft.
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公开(公告)号：US20130229047A1
公开(公告)日：2013-09-05
申请号：US13774219
申请日：2013-02-22
Applicant: JTEKT CORPORATION
Inventor： Katsuyuki HARADA , Hiroshi ANNO
IPC: B60B27/06
CPC classification number: B60B27/065 , B60B3/008 , B60B3/087 , B60B27/00 , B60B27/0005 , B60B27/0031 , B60B27/0036 , B60B2310/305 , B60B2310/306 , B60B2360/10 , B60Y2200/10 , B60Y2200/20 , B60Y2200/50 , F16C19/186 , F16C33/586 , F16C35/063 , F16C2326/02 , F16D1/076
Abstract: A rotary ring of a hub unit has an annular end face on one side in the axial direction, and a tapered outer periphery in a radially outer region of the end face. The diameter of the tapered outer periphery increases toward the other side in the axial direction. An outer ring of a joint has an annular end face on the other side in the axial direction, and had a tapered inner periphery in a radially outer region of the end face. The diameter of the tapered inner periphery increases toward the other side in the axial direction, and the tapered inner periphery faces the tapered outer periphery. Splines are formed in the tapered outer periphery and splines are formed in the tapered inner periphery, and the splines of the tapered outer periphery and the splines of the tapered inner periphery mesh with each other.
Abstract translation: 毂单元的旋转环在轴向一侧具有环形端面，在端面的径向外侧区域具有锥形的外周。 锥形外周的直径朝轴向另一侧增加。 接头的外圈在轴向的另一侧具有环形端面，并且在端面的径向外侧区域具有锥形的内周。 锥形内周的直径朝向轴向的另一侧增加，锥形内周面向锥形外周。 花键形成在锥形外周中，花键形成在锥形内周中，锥形外周的花键和锥形内周的花键彼此啮合。
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公开(公告)号：US20240300323A1
公开(公告)日：2024-09-12
申请号：US18668009
申请日：2024-05-17
Applicant: Orbit Fab, Inc.
Inventor： Daniel Faber , James Bultitude , Jeremy Schiel , Eric Weinhoffer , Andrew Witte , Tyler Mincey
CPC classification number: B60K15/03006 , B60K15/03 , B64G1/22 , B60K2015/03085 , B60K2015/03171 , B60K2015/03309 , B60Y2200/46 , B60Y2200/50
Abstract: An enclosed volume is provided for performing operations in space, or on any astronomical object, in a manner separated from aspects of the external environment. The enclosed volume can be a flexible container for a satellite. The enclosed volume can include a membrane having a fluid barrier layer and being configured to contain a propellant gas or fluid; and an expulsion device configured to expel material from the membrane. In a stowed configuration, the flexible container is contained within the satellite, and in a deployed configuration, the flexible container extends away from the satellite. The flexible container can inflate from one shape, in the undeployed configuration, to another shape, in a deployed configuration. The other shape can be toroidal or other appropriate shapes. The flexible container can provide bipropellant, blowdown, and gas/fluid metering functionality. Entertainment and game play can be enabled by the enclosed volume involving robots and other devices.
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公开(公告)号：US12081620B2
公开(公告)日：2024-09-03
申请号：US17408541
申请日：2021-08-23
Applicant: May Patents Ltd.
Inventor： Yehuda Binder , Benjamin Maytal
CPC classification number: H04L67/12 , G07C3/02 , B60K31/00 , B60K31/18 , B60Y2200/11 , B60Y2200/12 , B60Y2200/126 , B60Y2200/13 , B60Y2200/30 , B60Y2200/40 , B60Y2200/50 , B60Y2200/90 , G06Q2240/00 , G07C5/008 , G08G1/00 , Y04S40/18
Abstract: 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.
