-
-
-
公开(公告)号:EP3878739B1
公开(公告)日:2023-04-12
申请号:EP21167220.9
申请日:2018-12-13
IPC分类号: B64C27/82 , B63H1/14 , B64C27/46 , B64C27/467
-
公开(公告)号:EP3894198A1
公开(公告)日:2021-10-20
申请号:EP19839381.1
申请日:2019-12-11
-
5.
公开(公告)号:EP3766786A1
公开(公告)日:2021-01-20
申请号:EP19186181.4
申请日:2019-07-14
发明人: PAWLICZEK, Carsten
摘要: A flight direction indication system (2) for an aerial vehicle (100) having a plurality of rotors (110) includes: for each of the plurality of rotors (110), at least one rotor blade (10) having a plurality of light sources (20) arranged along a radial extension of the rotor blade (10); and a control unit (30), coupled to the plurality of light sources (20) of the rotor blades (10) of the plurality of rotors (110); wherein the control unit (30) is configured to effect a coordinated control of the plurality of light sources (20) of the rotor blades (10) of the plurality of rotors (110), with the coordinated control yielding an image (80) or a sequence of images across the plurality of rotors (10) to an observer of the aerial vehicle (100); and wherein the control unit (30) is configured to control the plurality of light sources (20) of the rotor blades (10) of the plurality of rotors (110) on the basis of a momentary flight direction (70) of the aerial vehicle (100), with said image (80) or said sequence of images comprising a flight direction indication, indicative of the momentary flight direction (70) of the aerial vehicle (100).
-
-
公开(公告)号:EP3142923B1
公开(公告)日:2020-05-06
申请号:EP15802653.4
申请日:2015-03-12
-
公开(公告)号:EP3372497B1
公开(公告)日:2019-08-28
申请号:EP18157737.0
申请日:2018-02-20
-
公开(公告)号:EP3374262A1
公开(公告)日:2018-09-19
申请号:EP16864758.4
申请日:2016-10-25
CPC分类号: B64C27/72 , B64C27/473 , B64C27/54 , B64C27/64 , B64C2027/7272 , Y02T50/34
摘要: A closeout structure for a rotor blade includes a first fluid channel for supplying a first pressure to a first port of a trailing edge (TE) device, a second fluid channel for supplying a second pressure to a second port of the TE de vice, and a trough disposed between the first fluid channel and the second fluid channel. The closeout structure forms a double-W shape.
-
公开(公告)号:EP3372497A1
公开(公告)日:2018-09-12
申请号:EP18157737.0
申请日:2018-02-20
CPC分类号: B64C27/463 , B64C27/37 , B64C27/39 , B64C27/473
摘要: A helicopter has a mast axis and a rotorcraft blade assembly (100). The rotorcraft blade assembly (100) has a main body (102) and a blade tip (104) movable relative to the main body (102). The rotorcraft blade assembly (100) is selectively rotatable about the mast axis.
-
-
-
-
-
-
-
-
-