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公开(公告)号：US11214355B2
公开(公告)日：2022-01-04
申请号：US16967553
申请日：2019-01-30
发明人： Bernhard Schlipf , Florian Lorenz , Dennis Krey , Stefan Bensmann
摘要： A wing for an aircraft is disclosed having a main wing, a slat, and a connection assembly movable connecting the slat to the main wing. The connection assembly includes an elongate slat track, and the front end of the slat track is mounted to the slat. The rear end and the intermediate portion of the slat track are mounted to the main wing by a roller bearing that includes a guide rail mounted to the main wing and a first roller unit mounted to the rear end of the slat track and engaging the guide rail, and wherein the roller bearing having a second roller unit that is mounted to the main wing and that engages an engagement surface of the slat track. The slat track is supported in a wing span direction by a lateral support.
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公开(公告)号：US20200307769A1
公开(公告)日：2020-10-01
申请号：US16830590
申请日：2020-03-26
发明人： Florian Lorenz , Dennis Krey , Bernhard Schlipf , Dustin Shapi
摘要： A wing for an aircraft including a main wing, slat, and connection assembly movable connecting the slat to the main wing and including an elongate slat track. A front end of the slat track is mounted to the slat and a rear end and an intermediate portion of the slat track are mounted to the main wing by a roller bearing that includes a guide rail mounted to the main wing and a first roller unit mounted to the rear end of the slat track and engaging the guide rail. The wing has redundant main load paths as the guide rail includes a guide rail primary structure engaging with the first roller unit, and an additional reinforcement structure additionally reinforcing the guide rail primary structure in a lateral direction, wherein the guide rail primary structure forms a first main load path and the reinforcement structure forms a redundant second main load path.
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公开(公告)号：US20240343381A1
公开(公告)日：2024-10-17
申请号：US18624519
申请日：2024-04-02
发明人： Bernhard Schlipf , Dennis Krey
IPC分类号： B64C9/02
CPC分类号： B64C9/02
摘要： An aircraft system includes a support structure, an aerodynamic component, a first coupling unit and a second coupling unit. The first coupling unit includes a first coupling mechanism movably coupling the aerodynamic component to a first coupling point at the support structure, and a second coupling mechanism coupling the aerodynamic component to a second coupling point at the support structure. The first and second coupling points are spatially separated from each other, wherein the first coupling mechanism and the second coupling mechanism interact with each other to enable a rotational movement of the aerodynamic component with respect to the support structure such that, during the rotational movement of the aerodynamic component, a center of rotation of the aerodynamic component is translated from a neutral position to an adjusted position. The second coupling unit pivotably moves the aerodynamic component about a pivot axis at the support structure.
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公开(公告)号：US11731753B2
公开(公告)日：2023-08-22
申请号：US17208595
申请日：2021-03-22
发明人： Dennis Krey , Alexander Huber , Bernhard Schlipf , Florian Lorenz , Dustin Shapi , Robert Grahs
摘要： A wing for an aircraft, including a main wing, a slat, and a connection assembly movably connecting the slat to the main wing. The connection assembly includes an elongate slat track with a front end mounted to the slat and a rear end and an intermediate portion mounted to the main wing by a roller bearing, and includes a guide rail mounted to the main wing and a first roller unit mounted to the slat track rear end and engaging the guide rail. The roller bearing includes a second roller unit mounted to the main wing and engaging a slat track intermediate portion engagement surface. The slat track has an upper and lower flange and at least one web. The second roller unit is arranged in a recess between the upper and lower flanges and engages the engagement surface provided at the upper and/or lower flange.
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公开(公告)号：US11807365B2
公开(公告)日：2023-11-07
申请号：US17581745
申请日：2022-01-21
发明人： Dennis Krey , Alexander Huber , Bernhard Schlipf , Florian Lorenz
摘要： A wing for an aircraft is disclosed having a main wing, a slat, and a connection assembly movable connecting the slat to the main wing, wherein the connection assembly includes an elongate slat track, wherein the front end of the slat track is mounted to the slat, wherein the rear end and the intermediate portion of the slat track are mounted to the main wing by a roller bearing comprising a guide rail mounted to the main wing and a first roller unit mounted to the rear end of the slat track and engaging the guide rail, and wherein the roller bearing includes a second roller unit mounted to the main wing and engaging an engagement surface at the intermediate portion of the slat track.
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公开(公告)号：US11286033B2
公开(公告)日：2022-03-29
申请号：US16830590
申请日：2020-03-26
发明人： Florian Lorenz , Dennis Krey , Bernhard Schlipf , Dustin Shapi
摘要： A wing for an aircraft including a main wing, slat, and connection assembly movable connecting the slat to the main wing and including an elongate slat track. A front end of the slat track is mounted to the slat. A rear end and an intermediate portion of the slat track are mounted to the main wing by a roller bearing that includes a guide rail mounted to the main wing and a first roller unit mounted to the rear end of the slat track and engaging the guide rail. The wing has redundant main load paths. The guide rail includes a guide rail primary structure engaging with the first roller unit and an additional reinforcement structure additionally reinforcing the guide rail primary structure in a lateral direction. The guide rail primary structure forms a first main load path. The reinforcement structure forms a redundant second main load path.
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公开(公告)号：US11192631B2
公开(公告)日：2021-12-07
申请号：US16442726
申请日：2019-06-17
发明人： Bernhard Schlipf , Florian Lorenz , Dennis Krey
摘要： A C-shaped connection assembly transmits loads in a load plane between a first and a second wing element. The connection assembly comprises a first and a second L-shaped load-bearing device. Each load-bearing device comprises a joint region and two legs extending parallel to the load plane and away from the joint region towards respective end regions. One leg of the first load-bearing device extends parallel to one leg of the second load bearing device. These legs are connected to one another. Two coupling portions which connect the connection assembly to the second wing element are formed in the respective joint regions of the load-bearing devices. Two further coupling portions which connect the connection assembly to the first wing element are formed in respective free end region of the load-bearing device and the joint region of the second load-bearing device.
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