-
公开(公告)号：US20220081100A1
公开(公告)日：2022-03-17
申请号：US17533652
申请日：2021-11-23
摘要： A wing for an aircraft includes a main wing, slat, and connection assembly movably connecting the slat to the main wing, wherein the slat is movable between a retracted position and an extended position. The connection assembly includes a guide rail and an elongate slat track extending along a track longitudinal axis between front and rear ends, the front end of the slat track fixedly mounted to the slat. A first roller unit is mounted to the rear end of the slat track engaging the guide rail. A roller bearing includes a second roller unit mounted to the main wing and engaging an engagement surface of the slat track. The slat track includes a slot extending through the slat track along the track longitudinal axis. The second roller unit includes a first roller element and a second roller element mounted on one common shaft for common rotation, and the common shaft proceeds through the slot.
-
公开(公告)号：US10538309B2
公开(公告)日：2020-01-21
申请号：US15716916
申请日：2017-09-27
发明人： Florian Lorenz
摘要： A system for driving and guiding a trailing edge control surface arranged on a wing of an aircraft includes a first guide device attachable to the wing and coupled with an inboard section of the control surface for guiding the inboard section along a trajectory relative to the trailing edge region of the wing between a retracted position and an extended position, a second guide device attachable to the wing and holding a connecting means of an outboard section of the control surface, and a drive device attachable to the wing and the control surface for moving the control surface. The trajectory is a spatial path at least along one dimension, wherein a distance between the inboard section of the control surface and a fixed part of the wing changes during a motion of the inboard section on the trajectory.
-
公开(公告)号：US20190193837A1
公开(公告)日：2019-06-27
申请号：US16227699
申请日：2018-12-20
发明人： Bernhard Schlipf , Florian Lorenz
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, such that the slat is movable between a retracted position and at least one extended position. The connection assembly includes a first connection station and a second connection station spaced apart from the first connection station in a wing span direction. The object, to prevent the slat from skewing, is achieved in that the connection assembly includes a sync shaft coupling the first connection station to the second connection station for sync movement of the first and second connection stations.
-
公开(公告)号：US20190162232A1
公开(公告)日：2019-05-30
申请号：US16139220
申请日：2018-09-24
发明人： Florian Lorenz , Dustin Shapi
IPC分类号： F16C33/20
摘要： A curable composite bush for an aircraft joint comprising a generally hollow cylindrical body formed from a matrix material impregnated with a reinforcement material substantially composed of fibers, the fibers being oriented in a generally circumferential direction about a longitudinal axis of the bush. The body may define a plurality of corrugations extending between an inner and an outer diameter of the bush to improve the compressibility of the bush in a direction substantially collinear to a longitudinal axis of the bush.
-
25.发明授权公开(公告)号：US12084185B2
公开(公告)日：2024-09-10
申请号：US17580779
申请日：2022-01-21
发明人： Bernhard Schlipf , Florian Lorenz
摘要： In order to provide a track drive device for an aircraft that has zero backlash, a large gear reduction, the ability to self-lock, and a better load transfer and reduced wear, the track drive device drives a track member through a drive device that has at least one drive unit that is arranged adjacent to the track member. Each drive unit comprises a plurality of engaging members that are driven by a cam shaft or a cam gear such that the engaging members are sequentially shifted in a wave-like pattern which results in the track member being moved in a linear manner relative to the drive device along a longitudinal direction.
-
26.发明授权公开(公告)号：US11731755B2
公开(公告)日：2023-08-22
申请号：US17580765
申请日：2022-01-21
发明人： Bernhard Schlipf , Florian Lorenz
摘要： In order to improve linear drives on aircraft with regards to backlash, gear reduction, self-lock capability, load transfer and wear, a linear drive device is provided that has a first member with engaging teeth, such as a tooth rack and a second member which functions as a drive unit. The second member includes a plurality of movable teeth that are actuated by a cam shaft. The cam shaft has a control cam portion that is shaped such that the movable teeth perform a wave-like motion that forces the first member along its longitudinal direction relative to the second member.
-
公开(公告)号：US11565789B2
公开(公告)日：2023-01-31
申请号：US17533652
申请日：2021-11-23
摘要： A wing for an aircraft includes a main wing, slat, and connection assembly movably connecting the slat to the main wing, wherein the slat is movable between a retracted position and an extended position. The connection assembly includes a guide rail and an elongate slat track extending along a track longitudinal axis between front and rear ends, the front end of the slat track fixedly mounted to the slat. A first roller unit is mounted to the rear end of the slat track engaging the guide rail. A roller bearing includes a second roller unit mounted to the main wing and engaging an engagement surface of the slat track. The slat track includes a slot extending through the slat track along the track longitudinal axis. The second roller unit includes a first roller element and a second roller element mounted on one common shaft for common rotation, and the common shaft proceeds through the slot.
-
公开(公告)号：US11352122B2
公开(公告)日：2022-06-07
申请号：US16554963
申请日：2019-08-29
发明人： Markus Gibbert , Florian Lorenz
摘要： A wing system (2) for an aircraft includes a movable flow body (6) and a cover panel (8), wherein the flow body (6) and the cover panel (8) both are movably supported on a main wing body (4). While the flow body (6) is actively driven into upwards or downwards deflected positions, the cover panel (8) is coupled with the flow body (6) to follow its motion. The cover panel covers a part of the flow body (6) and the main wing body (4) in order to provide a substantially continuous, closed outer contour.
-
公开(公告)号：US20220017211A1
公开(公告)日：2022-01-20
申请号：US17490357
申请日：2021-09-30
发明人： Bernhard Schlipf , Florian Lorenz
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, such that the slat is movable between a retracted position and at least one extended position. The connection assembly includes a first connection station and a second connection station spaced apart from the first connection station in a wing span direction. The object, to prevent the slat from skewing, is achieved in that the connection assembly includes a sync shaft coupling the first connection station to the second connection station for sync movement of the first and second connection stations.
-
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.
-
-
-
-
-
-
-
-
-
搜索结果
33 条记录 (耗时 0.017 秒)
