公开(公告)号：US20060049309A1

公开(公告)日：2006-03-09

申请号：US10933962

申请日：2004-09-03

申请人： Brian Hershberger ,  David Devine ,  Axel Sehic

发明人： Brian Hershberger ,  David Devine ,  Axel Sehic

IPC分类号： B64C25/14

CPC分类号： B64C25/14 ,  B64C25/50

摘要： A landing gear assembly comprises a landing gear strut assembly further comprising a landing gear strut having a longitudinal axis and extending from an inboard end to an outboard end capable of attaching to a wheel, and a landing gear housing. The landing gear housing has a longitudinal axis coincident with the landing gear strut longitudinal axis and having an interior chamber capable of accepting a portion of the landing gear strut. The landing gear housing is capable of pivotably coupling to an aircraft. The landing gear assembly further comprises a retraction linkage having an inboard end capable of coupling to the aircraft and an outboard end coupled to the landing gear housing. The retraction linkage is moveable to retract the landing gear strut assembly into an aircraft landing gear compartment about the landing gear housing pivotable aircraft coupling. The landing gear assembly further comprises a steering linkage capable of coupling and decoupling to the landing gear strut and, when coupled, capable of steerably rotating the landing gear strut with respect to the landing gear housing about the coincident longitudinal axis. The landing gear assembly further comprises a planing linkage that can gradually rotate the landing gear strut into a planar position as the landing gear strut assembly is retracted and decoupled from the steering linkage.

公开(公告)号：US07621481B2

公开(公告)日：2009-11-24

申请号：US10933962

申请日：2004-09-03

申请人： Brian Keith Hershberger ,  David J. Devine ,  Axel Sehic

发明人： Brian Keith Hershberger ,  David J. Devine ,  Axel Sehic

IPC分类号： B64C25/10 ,  B64C25/20

CPC分类号： B64C25/14 ,  B64C25/50

摘要： A landing gear assembly comprises a landing gear strut assembly further comprising a landing gear strut having a longitudinal axis and extending from an inboard end to an outboard end capable of attaching to a wheel, and a landing gear housing. The landing gear housing has a longitudinal axis coincident with the landing gear strut longitudinal axis and having an interior chamber capable of accepting a portion of the landing gear strut. The landing gear housing is capable of pivotably coupling to an aircraft. The landing gear assembly further comprises a retraction linkage having an inboard end capable of coupling to the aircraft and an outboard end coupled to the landing gear housing. The retraction linkage is moveable to retract the landing gear strut assembly into an aircraft landing gear compartment about the landing gear housing pivotable aircraft coupling. The landing gear assembly further comprises a steering linkage capable of coupling and decoupling to the landing gear strut and, when coupled, capable of steerably rotating the landing gear strut with respect to the landing gear housing about the coincident longitudinal axis. The landing gear assembly further comprises a planing linkage that can gradually rotate the landing gear strut into a planar position as the landing gear strut assembly is retracted and decoupled from the steering linkage.

摘要翻译： 起落架组件包括起落架支柱组件，其还包括具有纵向轴线并从内侧端延伸到能够附接到车轮的外侧端部的起落架支柱和起落架壳体。 起落架壳体具有与起落架支柱纵向轴线重合的纵向轴线，并且具有能够接收起落架支柱的一部分的内部室。 起落架壳体能够可枢转地联接到飞行器。 起落架组件还包括具有能够联接到飞行器的内侧端部和联接到起落架壳体的外侧端部的缩回连杆。 回缩联动装置可移动以将起落架支柱组件缩回到起落架壳体可枢转的飞机联轴器内的飞机起落架舱内。 起落架组件还包括能够联接和解耦到起落架支柱的转向连杆，并且当被联接时，能够使起落架支柱相对于起落架壳体围绕重合的纵向轴线可转动地旋转。 起落架组件还包括一个平面连接件，当起落架支柱组件缩回并与转向连杆分离时，该平面连接件可逐渐地将起落架支柱旋转到平面位置。

公开(公告)号：US06622967B2

公开(公告)日：2003-09-23

申请号：US10041042

申请日：2002-01-09

申请人： Scott Van Weelden ,  Axel Sehic ,  Kevin Kelly ,  Tom Pugh ,  Steve Ericson

发明人： Scott Van Weelden ,  Axel Sehic ,  Kevin Kelly ,  Tom Pugh ,  Steve Ericson

IPC分类号： B64D100

CPC分类号： B64D1/06 ,  B64D1/12

摘要： Apparatus for separating aerodynamic objects from an aerodynamic vehicle includes a first element, aerodynamically configured to create nose-down pitching moment, mounted to the object surface, a second element mounted to the first element and projecting into an oncoming airstream such that when enabled, the passing air tears the apparatus from the surface which otherwise supports it. The first element is a body designed to be conformal with the object surface to which it is mounted, and includes a forward end projecting into the oncoming airstream and a rearward end, and is secured to said object surface at the rearward end thereof. A flexible gasket is interposed between the first element and the object surface. The second element comprises a forward end directed toward the oncoming airstream and a rearward end, with the second element being mounted to the first element at the rearward end of the second element.

摘要翻译： 用于将空气动力学物体与空气动力学车辆分离的装置包括第一元件，空气动力学构造以产生安装到物体表面的下降俯仰力矩，安装到第一元件并投影到迎面而来的气流中的第二元件，使得当启动时， 通风的空气从表面撕裂装置，否则支撑它。 第一元件是设计成与其安装的物体表面共形的主体，并且包括突出到迎面而来的气流中的前端和后端，并且在其后端固定到所述物体表面。 在第一元件和物体表面之间插入柔性衬垫。 第二元件包括指向迎面而来的气流的前端和后端，第二元件在第二元件的后端安装到第一元件。