STAIRWAY FOR AN AIRCRAFT
    1.
    发明申请
    STAIRWAY FOR AN AIRCRAFT 审中-公开
    空中客车

    公开(公告)号:US20100301163A1

    公开(公告)日:2010-12-02

    申请号:US12599377

    申请日:2008-05-30

    IPC分类号: B64D11/00 B64C1/24 B64C1/14

    CPC分类号: B64D11/00 B64D2011/0076

    摘要: A stairway used for gaining access from a theoretically horizontal lower level to a theoretically horizontal higher level, and including a succession of intermediate steps between these two levels. A subassembly of intermediate steps corresponding to the steps closest to the lower level is mobile between a first deployed position at which the lower intermediate steps are in the extension of other intermediate steps, and a raised position at which the lower intermediate steps are in a substantially vertical position.

    摘要翻译: 用于从理论上水平的较低水平到理论上水平的较高水平的梯级,并包括这两个层次之间的一系列中间步骤。 对应于最靠近下层的台阶的中间步骤的子组件在第一展开位置之间是可移动的,第一展开位置处下部中间台阶处于其它中间台阶的延伸部分中,并且升高位置使下部中间台阶基本上 垂直位置。

    HOLD LAYOUT DEVICE FOR AN AIRCRAFT FOR CREW-MEMBER REST AND AIRCRAFT COMPRISING SAME
    2.
    发明申请
    HOLD LAYOUT DEVICE FOR AN AIRCRAFT FOR CREW-MEMBER REST AND AIRCRAFT COMPRISING SAME 有权
    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

    公开(公告)号:US20100187355A1

    公开(公告)日:2010-07-29

    申请号:US12664411

    申请日:2008-06-13

    IPC分类号: B64D11/00

    摘要: 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.

    摘要翻译: 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。

    FRONT AIRCRAFT PART COMPRISING A FLAT PARTITION BETWEEN A PRESSURISED ZONE AND A NON-PRESSURISED ZONE HOUSING LANDING GEAR
    3.
    发明申请
    FRONT AIRCRAFT PART COMPRISING A FLAT PARTITION BETWEEN A PRESSURISED ZONE AND A NON-PRESSURISED ZONE HOUSING LANDING GEAR 有权
    包括加压区域和非加压区域住房接地齿轮之间的平面分段的前飞机零件

    公开(公告)号:US20080210813A1

    公开(公告)日:2008-09-04

    申请号:US11964537

    申请日:2007-12-26

    IPC分类号: B64C1/00 B64C25/14

    CPC分类号: B64C1/10 B64C1/36 B64C25/14

    摘要: The present invention relates to a front aircraft part (1) comprising a non-pressurised landing gear housing zone (28) designed to house a front landing gear (30) in a retracted state, as well as a pressurised zone (2) adjacent to the non-pressurised landing gear housing zone. According to the invention, the pressurised zone is delimited by a set of walls among which only a substantially flat-shaped sealed partition wall (10) also participates in delimiting the non-pressurised landing gear housing zone (28).

    摘要翻译: 本发明涉及一种前飞行器部件(1),其包括设计成容纳处于缩回状态的前起落架(30)的非加压起落架壳体区(28)以及邻近 非加压起落架收容区。 根据本发明,加压区由一组壁限定,其中只有基本平坦的密封分隔壁(10)也参与限定非加压起落架容纳区(28)。

    Hold layout device for an aircraft for crew-member rest and aircraft comprising same
    4.
    发明授权
    Hold layout device for an aircraft for crew-member rest and aircraft comprising same 有权
    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

    公开(公告)号:US08727277B2

    公开(公告)日:2014-05-20

    申请号:US12664411

    申请日:2008-06-13

    IPC分类号: B64C1/20 B64C1/22 B64D47/00

    摘要: 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.

    摘要翻译: 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。

    Casing and front landing gear assembly for an aircraft
    5.
    发明授权
    Casing and front landing gear assembly for an aircraft 有权
    用于飞机的外壳和前起落架组件

    公开(公告)号:US08262020B2

    公开(公告)日:2012-09-11

    申请号:US12336988

    申请日:2008-12-17

    IPC分类号: B64C25/58

    CPC分类号: B64C25/14 B64C25/16

    摘要: 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.

    摘要翻译: 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。

    ITEM OF AIRCRAFT GALLEY FURNITURE AND AIRCRAFT COMPRISING SUCH AN ITEM OF FURNITURE
    6.
    发明申请
    ITEM OF AIRCRAFT GALLEY FURNITURE AND AIRCRAFT COMPRISING SUCH AN ITEM OF FURNITURE 有权
    飞机客厅家具及包含这类家具的飞机

    公开(公告)号:US20100181425A1

    公开(公告)日:2010-07-22

    申请号:US12664408

    申请日:2008-06-12

    IPC分类号: B64D11/04

    摘要: The invention relates to an item of aircraft galley furniture separating a cockpit (10) from an insecure zone (22) of the aircraft, characterized in that it comprises two portions separated from one another by a secure wall (24), one of the portions being accessible only from the cockpit, the other being accessible only from the insecure zone, a misalignment (32) being made in the portion of the item of furniture accessible from the cockpit.

    摘要翻译: 本发明涉及一种将驾驶舱(10)与飞机的不安全区(22)分开的飞机厨房家具的一个项目,其特征在于它包括通过一个固定壁(24)彼此分离的两个部分,其中一个部分 只能从驾驶舱进入,另一个只能从不安全区域进行访问,在可从驾驶舱进入的家具部分中进行不对准(32)。

    Item of aircraft galley furniture and aircraft comprising such an item of furniture
    7.
    发明授权
    Item of aircraft galley furniture and aircraft comprising such an item of furniture 有权
    飞机厨房家具和飞机的项目包括这样一件家具

    公开(公告)号:US08544795B2

    公开(公告)日:2013-10-01

    申请号:US12664408

    申请日:2008-06-12

    IPC分类号: B64D11/04

    摘要: An item of aircraft galley unit separating a cockpit from an insecure zone of the aircraft, including two portions separated from one another by a secure wall, one of the portions being accessible only from the cockpit, the other being accessible only from the insecure zone, a recess being made in the portion of the item of unit accessible from the cockpit.

    摘要翻译: 飞机厨房单元的一个单元,其将驾驶舱与飞机的不安全区域分开,包括两个通过安全壁彼此分开的部分,其中一个部分仅可从驾驶舱接近,另一个仅可从不安全区域接近, 在从驾驶舱可接近的单元的部分中制造凹部。

    Airplane Protected Against Projections of Tire Debris
    8.
    发明申请
    Airplane Protected Against Projections of Tire Debris 失效
    飞机保护轮胎碎片预测

    公开(公告)号:US20080006742A1

    公开(公告)日:2008-01-10

    申请号:US11774135

    申请日:2007-07-06

    IPC分类号: B64C1/00

    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。

    Aircraft comprising a platform that can be moved between two levels of the aircraft
    9.
    发明授权
    Aircraft comprising a platform that can be moved between two levels of the aircraft 有权
    飞机包括可以在飞机两级之间移动的平台

    公开(公告)号:US08360364B2

    公开(公告)日:2013-01-29

    申请号:US12664473

    申请日:2008-06-12

    IPC分类号: B64D11/00

    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: 具有至少两个级别位于另一级上的飞机,包括:能够在第一位置和第二位置之间移动的平台,作为下部位置的这些位置中的第一位置位于飞行器的第一级 作为更高职位的第二职位位于高于第一级的第二级; 连接在平台上的牵引电缆的组件和操作电缆以升高和降低平台的机构; 以及围绕至少部分地平台并且平台移动的壁的组合件。

    Front aircraft part comprising a flat partition between a pressurised zone and a non-pressurised zone housing landing gear
    10.
    发明授权
    Front aircraft part comprising a flat partition between a pressurised zone and a non-pressurised zone housing landing gear 有权
    前部飞行器部件包括在加压区域和外部起落架的非加压区域之间的平坦分隔

    公开(公告)号:US07784736B2

    公开(公告)日:2010-08-31

    申请号:US11964537

    申请日:2007-12-26

    IPC分类号: B64C1/00

    CPC分类号: B64C1/10 B64C1/36 B64C25/14

    摘要: The present invention relates to a front aircraft part (1) comprising a non-pressurised landing gear housing zone (28) designed to house a front landing gear (30) in a retracted state, as well as a pressurised zone (2) adjacent to the non-pressurised landing gear housing zone. According to the invention, the pressurised zone is delimited by a set of walls among which only a substantially flat-shaped sealed partition wall (10) also participates in delimiting the non-pressurised landing gear housing zone (28).

    摘要翻译: 本发明涉及一种前飞行器部件(1),其包括设计成容纳处于缩回状态的前起落架(30)的非加压起落架壳体区(28)以及邻近 非加压起落架收容区。 根据本发明,加压区由一组壁限定,其中只有基本平坦的密封分隔壁(10)也参与限定非加压起落架容纳区(28)。