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1. 发明授权

EP3684688B1 WING TILT ACTUATION SYSTEM FOR ELECTRIC VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT 有权
公开(公告)号：EP3684688B1
公开(公告)日：2024-06-26
申请号：EP18859571.4
申请日：2018-09-06
IPC分类号： B64C9/18 , B64C29/00 , B64C39/06 , B64D27/24 , B64D27/40 , B64C15/00
CPC分类号： B64C29/0033 , B64C39/068 , Y02T50/40 , Y02T10/72 , B64C9/18 , Y02T50/60 , B64D27/24 , B64D27/40 , B64C15/00

2. 发明授权

EP3998687B1 ELECTRICAL FAULT ISOLATION IN A POWER DISTRIBUTION NETWORK OF AN AIRCRAFT 有权
公开(公告)号：EP3998687B1
公开(公告)日：2024-05-15
申请号：EP21174719.1
申请日：2021-05-19
IPC分类号： H02H7/26 , B64D27/24 , B64C29/00 , B64C13/50 , H02J1/10 , B64C9/16 , B64C9/18 , B64D31/14 , B64C9/08 , B64C39/12 , B64C15/12
CPC分类号： H02J2310/4420200101 , H02H7/26 , B64D27/24 , B64D2221/0020130101 , B64C29/0033 , B64C13/50 , H02J1/106 , B64D31/14 , B64C39/12 , B64C15/12 , Y02T50/60 , B64C9/16 , B64C9/18

3. 发明公开

EP4361026A1 WING 审中-实审
公开(公告)号：EP4361026A1
公开(公告)日：2024-05-01
申请号：EP22204194.9
申请日：2022-10-27
申请人： Lilium eAircraft GmbH
发明人： Bunk, Yannick
IPC分类号： B64C9/18 , B64C9/38 , B64C29/00 , B64C39/12 , B64C23/06
CPC分类号： B64C9/38 , B64C9/18 , B64C29/0033 , B64C39/12 , B64C23/069
摘要： A wing (1) comprises: a fixed lift generating portion (2) extending along an extension direction of the wing (1); a moveable lift modifying portion (3) which is moveably, preferably pivotably, more preferably about a pivot axis (P) along the extension direction of the wing (1), connected to the fixed lift modifying portion (2), wherein the moveable lift modifying portion (3) comprises at least one propulsion device (31) configured to generate a thrust force along a thrust direction for powering the aerial vehicle, preferably a plurality of propulsion devices (31) arranged along the extension direction. In order to enhance the aerodynamic performance, the at least one propulsion device (31) forms a moveable wing tip end portion (4) located at a tip side along the extension direction of the wing (1), the moveable wing tip end portion (4) comprising an aerodynamic profile, which is in particular part of a winglet.

4. 发明授权

EP2578489B1 Flap support 有权
公开(公告)号：EP2578489B1
公开(公告)日：2018-12-12
申请号：EP12186927.5
申请日：2012-10-02
申请人： Airbus Operations Limited
发明人： Soenarjo, Mochamad Agoes
IPC分类号： B64C9/02 , B64C9/18 , B64C9/16
CPC分类号： B64C9/18 , B64C3/50 , B64C9/02 , B64C9/16 , Y02T50/32 , Y02T50/44
摘要： A flap support structure (6) for an aircraft wing (3) having a trailing edge flap (5), the flap support structure comprising: a flap support beam (10) including an aerodynamic fairing (17); and a drive unit (13) including a universal support structure (18) which rotatably receives a drive shaft (25) connected to a drive arm (14a) for moving the trailing edge flap, wherein the universal support structure also forms part of the flap support beam and supports the aerodynamic fairing.

5. 发明授权

EP3034393B1 TRAILING EDGE DEVICE WITH BELL CRANK MECHANISM 有权
公开(公告)号：EP3034393B1
公开(公告)日：2018-10-17
申请号：EP15199859.8
申请日：2015-12-14
申请人： The Boeing Company
发明人： Fevergeon, Matthew D M , Kordel, Jan A.
IPC分类号： B64C9/16 , B64C9/02 , B64C9/04 , B64C9/12 , B64C9/10 , B64C9/32
CPC分类号： B64C9/04 , B64C9/02 , B64C9/10 , B64C9/16 , B64C9/18 , B64C9/323 , B64C13/28 , B64C2009/005 , Y02T50/32
摘要： A bell crank mechanism 150 is configured to at least indirectly link any movement of an aircraft wing spoiler-like hinge panel to the movement of an aircraft wing 110 trailing edge flight control device 124. The aircraft wing is configured to be fixed to and to extend from an aircraft fuselage, the wing including a leading edge and a trailing edge. The flight control device is attached to the trailing edge, and any movement of the control device is directly subject to an aircraft input controller. The moveable aerodynamic hinge panel is situated proximally to the control device, and the hinge panel is separately attached to the trailing edge. As configured, the bell crank mechanism assures that any hinge panel motion is slaved to the control device in a manner intended to optimize aerodynamic performance and efficiency.

6. 发明公开

EP3381796A1 AERODYNAMIC CONTROL SURFACE MOVEMENT MONITORING SYSTEM FOR AIRCRAFT 有权
公开(公告)号：EP3381796A1
公开(公告)日：2018-10-03
申请号：EP18163750.5
申请日：2018-03-23
申请人： Hamilton Sundstrand Corporation
发明人： HARRINGTON, Erik , MILLER, Christian , BISHOP, Yuniya S.
IPC分类号： B64C13/50 , B64D45/00 , B64C9/16
CPC分类号： B64D45/0005 , B64C9/16 , B64C9/18 , B64C13/50 , B64D47/02 , Y02T50/44
摘要： Actuator systems and methods for controlling aerodynamic control surfaces of aircraft including a first actuator (226) receiving a first input and a first linear translation element (232) that moves based thereon, the first linear translation element operably connected to a first portion of the control surface. A first sensor assembly (238) is disposed relative to the first actuator that generates an output based on a displacement of the first translation element. A second actuator (228) receives a second input and a second linear translation element (236) moves based on the second input, the second linear translation element operably connected to a second portion of the control surface. A second sensor assembly (240) is disposed relative to the second actuator that generates a second sensor output based on a displacement of the second translation element. A controller (218) generates the inputs and receives the sensor outputs to determine if an error condition exists for the system.

7. 发明公开

EP3271575A1 TRACTION AIR DEVICE, AIR DEVICE FOR A WIND PLANT AND WIND PLANT FOR ELECTRIC POWER PRODUCTION, SHIP PROVIDED WITH A TRACTION AIR DEVICE 有权转让
标题翻译：牵引空气装置，用于电力生产的风力发电厂和风力发电厂的空气装置，提供有牵引空气装置的船舶
公开(公告)号：EP3271575A1
公开(公告)日：2018-01-24
申请号：EP16713291.9
申请日：2016-03-17
申请人： Skypull SAGL
发明人： CATTANO, Aldo
IPC分类号： F03D5/00 , B64C3/16 , B64C9/18 , B64C9/20 , B63H9/04 , B63H9/06 , F03D5/04 , F03D5/06
CPC分类号： B63H9/0685 , B63B2035/446 , B63H2009/0692 , B64C3/16 , B64C9/18 , B64C9/20 , B64C31/06 , B64C39/022 , B64C39/068 , F03D5/005 , F03D5/04 , F03D5/06 , F05B2240/917 , F05B2240/921 , F05B2240/931 , F05B2240/94 , F05B2250/12 , F05B2250/121 , Y02E10/70 , Y02E10/728
摘要： Traction air device with multiple wing contours for a wind power generation plant and wind power generation plant utilizing the air device.

8. 发明公开

EP3118112A1 AERONEF COMBINE MUNI D'UN DISPOSITIF ANTICOUPLE COMPLEMENTAIRE 有权
标题翻译： KOMBINIERTES LUFTFAHRZEUG，DAS MIT EINERZUSÄTZLICHENGEGENDREHMOMENTVORRICHTUNG AUSGESTATTET IST
公开(公告)号：EP3118112A1
公开(公告)日：2017-01-18
申请号：EP16177015.1
申请日：2016-06-29
申请人： Airbus Helicopters
发明人： TOULMAY, François
IPC分类号： B64C27/26 , B64C27/82
CPC分类号： B64C27/26 , B64C3/00 , B64C3/32 , B64C9/18 , B64C27/22 , B64C27/82 , B64C29/0025 , B64C2027/8236
摘要： La présente invention concerne un aéronef combiné (1) comportant un fuselage (2), un rotor principal (3), un dispositif anticouple principal (4) et deux ailes (11,11') positionnées de part et d'autre dudit fuselage (2). Chaque aile (11,11') comporte au moins un volet (12,12') mobile situé au niveau de son bord de fuite. Lesdits volets (12,12') peuvent être orientés de façon dissymétrique vis à vis d'un flux d'air généré en réaction à la portance dudit rotor principal (3) de part et d'autre dudit fuselage (2) afin de créer des efforts aérodynamiques longitudinaux de sens opposés de part et d'autre dudit fuselage (2) et, par suite, un couple complémentaire s'ajoutant au couple principal dudit dispositif anticouple principal (4).
摘要翻译：具有机身，主转子，主抗扭矩装置和位于机身两侧的两个机翼的复合飞机。每个翼片具有位于其后缘的至少一个活动翼片。翼片可相对于机身两侧的主转子升力产生的空气流不对称地偏转，从而在机身两侧产生相反方向的纵向空气动力，从而产生额外的转矩，被加到主反扭矩装置的主扭矩上。

9. 发明授权

EP2878538B1 An aircraft 有权转让
标题翻译：一架飞机
公开(公告)号：EP2878538B1
公开(公告)日：2016-05-18
申请号：EP14192431.6
申请日：2014-11-10
申请人： Rolls-Royce plc
发明人： Moxon, Matthew
IPC分类号： B64D27/12 , B64D27/24
CPC分类号： B64C23/005 , B64C3/00 , B64C3/28 , B64C9/18 , B64C11/00 , B64C39/00 , B64D27/10 , B64D27/12 , B64D27/24 , Y02T50/44 , Y02T50/64

10. 发明公开

EP2917101A1 AN AIRPLANE WING, AN AIRPLANE AND A FLAP SYSTEM 有权
标题翻译：飞机机翼，飞机和折叠系统
公开(公告)号：EP2917101A1
公开(公告)日：2015-09-16
申请号：EP13786556.4
申请日：2013-10-29
申请人： Fokker Aerostructures B.V.
发明人： BASTIAANSEN, Adrianus Marinus Franciscus , SCHOONHOVEN, Michel
IPC分类号： B64C9/20 , B64C9/18
CPC分类号： B64C9/38 , B64C9/16 , B64C9/18 , B64C13/00 , Y02T50/32
摘要： An airplane wing comprises a main wing and a flap system that has a flap at the trailing edge of the main wing. An elongate flap track member is connected to the main wing in such a manner that it can be moved substantially in its longitudinal direction and is guided by supporting bearing elements relative to the main wing between a forward retracted position and a rearward extended position. The flap is rotatably connected to the rear end of the flap track member in such a manner that it can rotate about a rotation axis that extends substantially parallel to the trailing edge of the main wing, so that the flap moves together with the flap track member when the flap track member is moved and so that the flap can be rotated about the rotation axis mechanically independently of the movement of the flap track member. The flap system comprises an actuator system having two actuators. The first actuator is connected to the main wing and has an engagement member that engages the flap or the flap track member for moving the flap together with the flap track member so that the flap track member is move able between its retracted position and its extended position. The second actuator is connected to the flap track member so that the second actuator moves together with the flap track member when the flap track member is moved by means of the first actuator. The second actuator has an engagement member that engages the flap for rotating the flap about the rotation axis.

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