公开(公告)号：US20100187356A1

公开(公告)日：2010-07-29

申请号：US12664473

申请日：2008-06-12

申请人： Bernard Guering ,  Jonathan Guering

发明人： Bernard Guering ,  Jonathan Guering

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  B66B9/00 ,  B66B11/008 ,  B66B11/0438

摘要： An aircraft with at least two levels situated one above the other, including: a platform that can be moved between a first position and a second position, the first of these positions, as a lower position, being situated at a first level of the aircraft and the second position, as a higher position, being situated at a second level higher than that of the first level; an assembly of traction cables connected on the platform and a mechanism operating the cables for raising and lowering the platform; and an assembly of walls surrounding at least partially the platform and along which the platform moves.

摘要翻译： 一种具有至少两个级别位于另一级的飞机，包括：可在第一位置和第二位置之间移动的平台，作为较低位置的这些位置中的第一位置位于飞行器的第一级 作为较高职位的第二职位位于比第一级高的第二级; 连接在平台上的牵引电缆的组件和操作用于升高和降低平台的电缆的机构; 以及围绕至少部分地平台并且平台移动的壁的组合件。

公开(公告)号：US07669798B2

公开(公告)日：2010-03-02

申请号：US11774135

申请日：2007-07-06

申请人： Bernard Guering ,  Jonathan Guering

发明人： Bernard Guering ,  Jonathan Guering

IPC分类号： B64C25/00

CPC分类号： B62D25/168 ,  B64C25/32

摘要： The tires that equip airplane wheels have elastomer treads from which a piece may detach and damage a zone of the airplane. Shredding means, situated between wheel and another part of the airplane, shred the piece of tread, which detaches from the tire and is projected onto the other part of the airplane, into several small pieces. These shredding means, such as a grid with blades that can cut the tread material, are arranged so as to disperse the pieces. A process reinforces the tolerance of an airplane to impacts of a detached piece of the tread, by shredding the piece into several small pieces between the instant when the piece is detached and the instant when the piece would have struck airplane.

摘要翻译： 配备飞机车轮的轮胎具有弹性体胎面，一块可以从其中分离并损坏飞机的区域。 位于车轮和飞机另一部分之间的切碎装置将从轮胎分离并投影到飞机的另一部分上的胎面碎片分割成若干小块。 这些切碎装置，例如具有可切割胎面材料的具有叶片的格栅，被布置成分散碎片。 一个过程加强了一个飞机对一个分离的踏板的冲击的公差，通过将碎片从零件分离出来的瞬间和当该部件撞击飞机的瞬间将碎片切碎成若干小块。

公开(公告)号：US20090159743A1

公开(公告)日：2009-06-25

申请号：US12336988

申请日：2008-12-17

申请人： Bernard GUERING ,  Jonathan Guering

发明人： Bernard GUERING ,  Jonathan Guering

IPC分类号： B64C25/16

CPC分类号： B64C25/14 ,  B64C25/16

摘要： The casing comprises a wall defining an internal housing open on the bottom in order to allow the retraction of a corresponding front landing gear into the interior of the housing. The said wall separates the said non-pressurized internal housing from a surrounding pressurized zone of the aircraft. A reinforcement structure is provided around the wall on the side of the surrounding pressurized zone. The separation wall is a shell coming to envelop the shape of the front landing gear, on the side opposite the opening of the internal housing, and the reinforcement structure comprises on the one hand longitudinal reinforcement elements extending on both sides of the shell and on the other hand transverse reinforcement elements connecting the longitudinal reinforcement elements. The shell has a first zone of considerable width accommodating the wheels of the landing gear, a second zone of lesser width accommodating the rod of the landing gear, and a third zone running from the second zone of lesser width, becoming wider and accommodating a portion of the mechanism for deployment/retraction of the landing gear. As a variant or in combination, the shell has on the one hand a front area of considerable height accommodating the wheels of the landing gear and on the other hand a rear area of lesser height accommodating the rod and a portion of the mechanism for deployment/retraction of the said landing gear and above which there extends at least one transverse reinforcement element making it possible to provide support for an equipment item of the aircraft.

摘要翻译： 壳体包括限定在底部上敞开的内部壳体的壁，以允许将相应的前起落架收回到壳体的内部。 所述壁将所述非加压内部壳体与飞行器的周围加压区域分开。 在围绕加压区侧面的壁周围设置加强结构。 分隔壁是在与内部壳体的开口相对的一侧上包围前起落架的形状的壳体，并且加强结构一方面包括在壳体的两侧上延伸的纵向加强元件 连接纵向加强件的其他手横向加强件。 壳体具有容纳起落架的轮的相当大的宽度的第一区域，容纳起落架的杆的较小宽度的第二区域和从较小宽度的第二区域延伸的第三区域变得更宽并且容纳部分 的起落架的部署/缩回机制。 作为变型或组合，壳体一方面具有容纳起落架的车轮的相当高的前部区域，另一方面具有容纳杆的较小高度的后部区域和一部分用于展开/ 所述起落架的后退，并且其上延伸有至少一个横向加强元件，使得可以为飞行器的设备项提供支撑。