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    • 1. 发明授权
    • Hold layout device for an aircraft for crew-member rest and aircraft comprising same
    • 保持用于机组人员休息的飞机的布置装置和包括其的飞机
    • US08727277B2
    • 2014-05-20
    • US12664411
    • 2008-06-13
    • Bernard GueringJonathan Guering
    • Bernard GueringJonathan Guering
    • B64C1/20B64C1/22B64D47/00
    • B64D11/00B64D2011/0076Y02T50/46
    • The invention relates to a device for developing an aircraft hold located under the floor of the passenger cabin and the cockpit and including a so-called commercial area in which freight can be transported and a technical area including technical equipment and located at the front of the commercial area an at least partially under the cockpit, wherein said device includes: at least one compartment sealed relative to the hold located at the front of said commercial area and at the back of a portion at least of the technical area; a staircase connecting each compartment to a portion of the intermediate floor between the passenger cabin and the cockpit; and a sealed corridor extending from said staircase to each of said sealed compartments.
    • 本发明涉及一种用于开发位于客舱和驾驶舱的地板下方的飞机座架的装置,并且包括可以运输货物的所谓的商业区域和包括技术设备在内的技术区域,并且位于 商业区域至少部分地位于驾驶舱之下,其中所述装置包括:至少一个隔室,其相对于位于所​​述商业区域前方和所述技术区域的至少一部分的后部处的所述保持器密封; 将每个隔间连接到客舱和驾驶舱之间的中间地板的一部分的楼梯; 以及从所述楼梯延伸到每个所述密封隔间的密封走廊。
    • 2. 发明授权
    • Casing and front landing gear assembly for an aircraft
    • 用于飞机的外壳和前起落架组件
    • US08262020B2
    • 2012-09-11
    • US12336988
    • 2008-12-17
    • Bernard GueringJonathan Guering
    • Bernard GueringJonathan Guering
    • B64C25/58
    • B64C25/14B64C25/16
    • A casing including a wall defining an internal housing which allows retraction of a corresponding landing gear into the interior of the housing. The wall separates the non-pressurized internal housing from a surrounding pressurized zone of the aircraft. The separation wall is a shell which envelops the shape of the landing gear, on the side opposite the opening of the internal housing, and the reinforcement structure includes on 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.
    • 壳体包括限定内部壳体的壁,其允许将相应的起落架收回到壳体的内部。 该墙将非加压内部壳体与飞行器的周围加压区域分开。 分隔壁是包围起落架形状的壳体,其在与内部壳体的开口相对的一侧上,并且加强结构一方面包括在壳体两侧延伸的纵向加强元件,另一方面横向 连接纵向加强件的加强件。 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。
    • 5. 发明申请
    • HOLD LAYOUT DEVICE FOR AN AIRCRAFT FOR CREW-MEMBER REST AND AIRCRAFT COMPRISING SAME
    • 保留用于CREW会员休息的飞机的保持布置设备和包含相同的飞机
    • US20100187355A1
    • 2010-07-29
    • US12664411
    • 2008-06-13
    • Bernard GueringJonathan Guering
    • Bernard GueringJonathan Guering
    • B64D11/00
    • B64D11/00B64D2011/0076Y02T50/46
    • The invention relates to a device for developing an aircraft hold located under the floor of the passenger cabin and the cockpit and including a so-called commercial area in which freight can be transported and a technical area including technical equipment and located at the front of the commercial area an at least partially under the cockpit, wherein said device includes: at least one compartment sealed relative to the hold located at the front of said commercial area and at the back of a portion at least of the technical area; a staircase connecting each compartment to a portion of the intermediate floor between the passenger cabin and the cockpit; and a sealed corridor extending from said staircase to each of said sealed compartments.
    • 本发明涉及一种用于开发位于客舱和驾驶舱的地板下方的飞机座架的装置,并且包括可以运输货物的所谓的商业区域和包括技术设备在内的技术区域,并且位于 商业区域至少部分地位于驾驶舱之下,其中所述装置包括:至少一个隔室,其相对于位于所​​述商业区域前方和所述技术区域的至少一部分的后部处的所述保持器密封; 将每个隔间连接到客舱和驾驶舱之间的中间地板的一部分的楼梯; 以及从所述楼梯延伸到每个所述密封隔间的密封走廊。
    • 9. 发明申请
    • Airplane Protected Against Projections of Tire Debris
    • 飞机保护轮胎碎片预测
    • US20080006742A1
    • 2008-01-10
    • US11774135
    • 2007-07-06
    • Bernard GueringJonathan Guering
    • Bernard GueringJonathan Guering
    • B64C1/00
    • B62D25/168B64C25/32
    • 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.
    • 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。