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1. 发明公开

EP4393815A1 AIRCRAFT FLAP SYSTEM 审中-公开
公开(公告)号：EP4393815A1
公开(公告)日：2024-07-03
申请号：EP22217421.1
申请日：2022-12-30
申请人： Airbus Operations GmbH
发明人： Schlipf, Bernhard , Winkelmann, Christoph
IPC分类号： B64C13/30 , B64C9/16 , B64C9/22
CPC分类号： B64C9/16 , B64C9/22 , B64C13/30
摘要： An aircraft wing (101) comprising a flap system (103) that is mounted at a leading or trailing edge (105, 107) of the wing (101) and comprises at least two movable flap devices (109, 111) spaced apart in a spanwise direction Y from each other, wherein each movable flap device (109, 111) is supported by at least one support station (203, 205) and is driven about a hinge axis (119) by at least one drive system (115), wherein the flap system (103) further comprises a synchronising torque element (113) connected to the movable flap devices (109, 111), wherein the synchronising torque element (113) is configured to transmit a torque between the movable flap devices (109, 111) in order to actuate a rotational movement of the movable flap devices (109, 111), and wherein the synchronising torque element (113) is positioned between the movable flap devices (109, 111) and around an adjacent system or structural component (116) that is also positioned between the movable flap devices (109, 111).

2. 发明公开

EP4311766A1 WING FOR AN AIRCRAFT 审中-公开
公开(公告)号：EP4311766A1
公开(公告)日：2024-01-31
申请号：EP22187881.2
申请日：2022-07-29
申请人： Airbus Operations GmbH
发明人： Schlipf, Bernhard , Haunert, Jan
IPC分类号： B64C9/02 , B64C9/06 , B64C9/20 , B64C13/30 , B64C13/50
摘要： Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a trailing edge high lift assembly (9) movably arranged at a trailing edge of the main wing (5), the trailing edge high lift assembly (9) comprising a flap (11) and a connection assembly (13) movably mounting the flap (11) to the main wing (5), wherein the connection assembly (13) comprises an actuator unit (35) for moving the flap (11) between a retracted position and at least one extended position, wherein the flap (11) comprises a leading edge part (23) and a trailing edge part (27) mounted to the leading edge part (23) in a manner pivotable about a pivot axis (31). The object to provide a wing having a simplified trailing edge high lift assembly that allows to reduce weight and costs of the wing, is achieved in that the actuator unit (35) is configured for moving the trailing edge part (27) relative to the leading edge part (23) in a way independent from moving the flap (11) between the retracted position and the at least one extended position, and/or in that the actuator unit (35) is configured for moving the flap (11) between the retracted position and the at least one extended position in a way independent from moving the trailing edge part (27) relative to the leading edge part (23)

3. 发明公开

EP4190687A1 AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS 审中-实审
公开(公告)号：EP4190687A1
公开(公告)日：2023-06-07
申请号：EP23152519.7
申请日：2016-04-21
申请人： Anduril Industries, Inc.
发明人： ALLEY, Nicholas Robert , STEELE, Joshua Lemming , WILLIAMS, Jesse Owen , KUEHME, Daniel , PHILLIPS, Jonathan Caleb
IPC分类号： B64C3/56 , B64C1/36 , B64C3/40 , B64C3/54 , B64C5/02 , B64C5/12 , B64C5/16 , B64C11/28 , B64C13/24 , B64C13/30 , B64C39/02 , B64U20/40 , B64U30/12
摘要： A telescoping wing system for an aerial vehicle comprising:
an inner section configured to be stowed within an interior of an outer section in a first configuration,
wherein the inner section is attached to a fuselage of the aerial vehicle; and
a telescoping mechanism configured to, after satisfaction of a pre-set condition, extend the outer section along a length of the inner section to increase a wingspan in a second configuration.

4. 发明授权

EP3663194B1 FLIGHT CONTROL CABLE SENSOR FOR AN AIRCRAFT 有权
公开(公告)号：EP3663194B1
公开(公告)日：2022-01-05
申请号：EP19210599.7
申请日：2019-11-21
发明人： CALLAHAN, Kevin S , YOO, Jeff
IPC分类号： B64C13/30 , G01B1/00 , G01P1/00 , G01L1/00 , G01D5/244 , G01D3/08 , B64D45/00

5. 发明授权

EP3043067B1 INTEGRATED HIGH THERMAL CONDUCTIVE FIBER AS COOLING FIN FOR SMA ACTUATOR WITH EXPANDABLE SLEEVE 有权
公开(公告)号：EP3043067B1
公开(公告)日：2021-03-10
申请号：EP15194126.7
申请日：2015-11-11
发明人： Apdalhaliem, Sahrudine , SHOME, Moushumi , Meredith, Kimberly D. , Ashmawi, Waeil M. , Safai, Morteza , CALKINS, Frederick T.
IPC分类号： F03G7/06 , B64C13/30

6. 发明授权

EP3056749B1 COMBINATION SPHERICAL AND LAMINATED BEARING ASSEMBLY 有权
公开(公告)号：EP3056749B1
公开(公告)日：2020-04-08
申请号：EP16155401.9
申请日：2016-02-12
申请人： Aktiebolaget SKF
发明人： Bohm, Anthony C.
IPC分类号： F16C11/06 , F16C23/04 , B64C13/30

7. 发明授权

EP3115625B1 ZUG-DRUCK-STANGE MIT VERBINDUNGSBOLZEN 有权
标题翻译： ZUG带连接销的压力杆
公开(公告)号：EP3115625B1
公开(公告)日：2018-04-18
申请号：EP16178335.2
申请日：2016-07-07
申请人： Fellinger, Josef , Haller, Matthias
发明人： Fellinger, Josef , Haller, Matthias
IPC分类号： F16B7/06 , B64C13/30 , F16B21/12 , F16C7/06
CPC分类号： F16B7/06 , F16B21/125 , F16C7/06

8. 发明公开

EP2729362A1 ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM 审中-公开
标题翻译： ELEKTRONISCH SYNCHRONISIERTES KLAPPENSYSTEM
公开(公告)号：EP2729362A1
公开(公告)日：2014-05-14
申请号：EP12740761.7
申请日：2012-06-27
申请人： Eaton Corporation
发明人： THOMPSON, Andrew , BAKER, Jeffrey, A. , NEELY, John, D. , TORRES, Peter, A.
IPC分类号： B64C13/28 , B64C13/30
CPC分类号： B64C13/503 , B64D45/00 , B64D2045/001
摘要： An electronically-synchronized flap system for a fixed-wing aircraft including a first wing (120) including a first flap panel (122), the first flap panel (122) being connected with a first in-board actuator (124) and a first out-board actuator(126), and a second wing (130) including a second flap panel(132), the second flap panel (132) being connected with a second in-board actuator (134) and a second out-board actuator (136). The system further includes an electronic control unit (ECU) (114) configured to control the first and second in-board and out-board actuators to electronically synchronize the positions of the first and second flap panels.
摘要翻译：一种用于固定翼飞行器的电子同步翼片系统，其包括第一翼片，所述第一翼片包括第一翼片板，所述第一翼板板与第一板载致动器连接，第二翼片包括第二翼片，翼片板，第二翼片板与第二板载致动器和第二外板致动器连接。在一个实施例中，系统还可以包括电子控制单元（ECU），其被配置为控制第一和第二板内和外板致动器以电子同步第一和第二挡板的位置。

9. 发明授权

EP2616332B1 APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES 有权
标题翻译：用于有效地操纵空气动力学表面的装置
公开(公告)号：EP2616332B1
公开(公告)日：2014-05-07
申请号：EP10859373.2
申请日：2010-11-04
申请人： Bell Helicopter Textron Inc.
发明人： SCHANK, Troy, C. , KINTZINGER, Peter, H. , SHERRILL, Paul, B. , PARHAM, Thomas, C. , POPELKA, David, A.
IPC分类号： B64C13/30 , B64C27/00 , B64C27/72 , B64C27/615
CPC分类号： B64C13/26 , B64C13/30 , B64C27/00 , B64C27/001 , B64C27/615 , B64C2027/7266 , F16H21/44 , Y02T50/34 , Y02T50/44

10. 发明授权

EP2616334B1 APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES 有权
标题翻译： DEVICE FOR ACTIVE MANIPULATION空气动力学表面
公开(公告)号：EP2616334B1
公开(公告)日：2014-04-23
申请号：EP10859345.0
申请日：2010-11-01
申请人： Bell Helicopter Textron Inc.
发明人： SCHANK, Troy, C. , KINTZINGER, Peter, H. , SHERRILL, Paul, B. , PARHAM, Thomas
IPC分类号： B64C27/615 , B64C27/00 , B64C13/30
CPC分类号： B64C13/26 , B64C13/30 , B64C27/00 , B64C27/001 , B64C27/615 , B64C2027/7266 , F16H21/44 , Y02T50/34 , Y02T50/44

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