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    • 1. 发明公开
    • AIRCRAFT COMPONENT AND METHOD OF MAKING AN AIRCRAFT COMPONENT
    • FLUGZEUGKOMPONENTE UND VERFAHREN ZUR HERSTELLUNG EINER FLUGZEUGKOMPONENTE
    • EP2969743A4
    • 2016-11-09
    • EP14779670
    • 2014-03-05
    • GULFSTREAM AEROSPACE CORP
    • SAMMONS GUY
    • B64C1/12
    • B32B7/12B32B3/04B32B15/01B32B2307/718B32B2605/18B64C1/061F16B11/006Y10T156/1064Y10T428/24612
    • An aircraft component includes, but is not limited to, a first panel including a first channel and a second panel including a second channel. The second panel is disposed such that the second channel is aligned with the first channel. The aircraft component further includes, but is not limited to, a web section that disposed adjacent the first and second panels. The web section includes a first engagement portion engaged with the first channel and a second engagement portion engaged with the second channel. The aircraft component further includes, but is not limited to an adhesive that is disposed between the first engagement portion and the first channel and between the second engagement portion and the second channel. The first panel and the second panel are joined together by cooperation of the web section and the adhesive.
    • 飞机部件包括但不限于包括第一通道的第一面板和包括第二通道的第二面板。 第二面板被布置成使得第二通道与第一通道对准。 飞机部件还包括但不限于布置在第一和第二面板附近的腹板部分。 腹板部分包括与第一通道接合的第一接合部分和与第二通道接合的第二接合部分。 飞机部件还包括但不限于设置在第一接合部分和第一通道之间以及第二接合部分和第二通道之间的粘合剂。 第一面板和第二面板通过腹板部分和粘合剂的协作而连接在一起。
    • 4. 发明公开
    • VIBRATION ISOLATION SYSTEM
    • SCHWINGUNGSISOLATIONSSYSTEM
    • EP2697534A4
    • 2015-01-14
    • EP12771281
    • 2012-04-11
    • GULFSTREAM AEROSPACE CORP
    • WANG TONGANHORNICK DAVID CMAXON JR JOHN WFOOSE ANDREW SFILA JOSEF A
    • F16F7/104B64C1/40
    • B64C1/40B64C1/406
    • A vibration isolation system for attenuating vibration energy between two aircraft structures, such as between the aircraft's fuselage and interior cabin. The vibration isolation system includes a first isolator attached to the first structure, a second isolator attached to the second structure, and an intermediate mass attached between the first and second isolators. The intermediate mass may be electrical cables, wiring bundles, a cable holder, or other component disposed between the two structures. Cable holder intermediate masses can be fabricated from an electrically conductive material to provide electromagnetic interference shielding for cables disposed therein. Multiple vibration isolation systems can be disposed between the fuselage and interior cabin to provide a less noisy cabin. Additional noise and vibration suppressors, such as skin damping material and acoustic blankets, also can be disposed between the fuselage and interior cabin to further reduce noise in the interior cabin.
    • 一种用于衰减两架飞机结构之间的振动能量的振动隔离系统,例如在飞机的机身和内部舱室之间。 隔振系统包括附接到第一结构的第一隔离器,附接到第二结构的第二隔离器和附接在第一和第二隔离器之间的中间物质。 中间质量体可以是设置在两个结构之间的电缆,布线束,电缆夹或其他部件。 电缆架中间质量可以由导电材料制成,以为设置在其中的电缆提供电磁干扰屏蔽。 多个隔振系统可以放置在机身和内部舱室之间,以提供一个较不嘈杂的舱室。 还可以在机身和内部舱室之间设置附加的噪声和振动抑制器,例如皮肤阻尼材料和声学毯,以进一步降低内部舱室的噪音。