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1. 发明申请

US20100155529A1 Landing gear with noise reduction fairing 有权
标题翻译：起落架减噪整流罩
公开(公告)号：US20100155529A1
公开(公告)日：2010-06-24
申请号：US12458407
申请日：2009-07-10
申请人： Leung Choi Chow , Philip Campbell , Christopher Wood , Andrew John Dyer
发明人： Leung Choi Chow , Philip Campbell , Christopher Wood , Andrew John Dyer
IPC分类号： B64C23/00 , B64C1/40 , B64C25/10
CPC分类号： B64C25/001 , B64C7/00 , B64C2025/003
摘要： An aircraft noise reduction apparatus is provided which includes an aircraft landing gear assembly and a noise reduction fairing 12. The landing gear assembly comprises a landing gear 10 arranged to be moveable between a stowed position and a fully deployed position. The noise reduction fairing 12 may comprise a wrap-around fairing which, when the landing gear 10 is in its fully deployed position, wraps around the landing gear 10 and extends along the majority of the length of a landing gear leg 11. A landing gear bay door assembly 16, 17 comprising at least one door may also be provided. The fairing 12 may have a recess 24 for accommodating one of landing gear bay doors when the door 16 is in its fully open position.
摘要翻译：提供了一种包括飞机起落架组件和降噪整流罩12的飞机降噪装置。起落架组件包括起落架10，起落架10布置成可在收起位置和完全展开位置之间移动。减噪整流罩12可以包括一个环绕整流罩，当起落架10处于其完全展开位置时，环绕整流罩围绕起落架10卷绕并沿起落架脚11的大部分长度延伸。起落架还可以设置包括至少一个门的舱门组件16,17。当门16处于其完全打开位置时，整流罩12可以具有用于容纳一个起落架舱门的凹部24。

2. 发明授权

US08490914B2 Landing gear with noise reduction fairing 有权
标题翻译：起落架减噪整流罩
公开(公告)号：US08490914B2
公开(公告)日：2013-07-23
申请号：US12458407
申请日：2009-07-10
申请人： Leung Choi Chow , Philip Campbell , Christopher Wood , Andrew John Dyer
发明人： Leung Choi Chow , Philip Campbell , Christopher Wood , Andrew John Dyer
IPC分类号： B64C23/00
CPC分类号： B64C25/001 , B64C7/00 , B64C2025/003
摘要： An aircraft noise reduction apparatus includes an aircraft landing gear assembly and a noise reduction fairing 12. The landing gear assembly includes a landing gear 10 arranged to be moveable between a stowed position and a fully deployed position. The noise reduction fairing 12 may include a wrap-around fairing which, when the landing gear 10 is in its fully deployed position, wraps around the landing gear 10 and extends along the majority of the length of a landing gear leg 11. A landing gear bay door assembly 16, 17 including at least one door may also be provided. The fairing 12 may have a recess 24 for accommodating one of landing gear bay doors when the door 16 is in its fully open position.
摘要翻译：飞机降噪装置包括飞机起落架组件和降噪整流罩12.起落架组件包括起落架10，起落架10设置成可在收起位置和完全展开位置之间移动。减噪整流罩12可以包括一个环绕整流罩，当起落架10处于其完全展开位置时，环绕整流罩围绕起落架10卷绕并沿起落架脚11的大部分长度延伸。起落架还可以提供包括至少一个门的舱门组件16,17。当门16处于其完全打开位置时，整流罩12可以具有用于容纳一个起落架舱门的凹部24。

3. 发明申请

US20100006696A1 Landing gear noise reduction assembly 审中-公开
标题翻译：起落架降噪装置
公开(公告)号：US20100006696A1
公开(公告)日：2010-01-14
申请号：US12458243
申请日：2009-07-06
申请人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
发明人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
IPC分类号： B64C25/16 , B64C23/00
CPC分类号： B64C25/16 , B64C2025/003
摘要： An aircraft noise reduction apparatus including an aircraft landing gear assembly (10) and a noise reduction fairing (12) is described. The landing gear assembly comprises (10) a landing gear bay having an aperture (14), a landing gear moveable between a stowed position and a fully deployed position, and at least one landing gear bay door (16) moveable to close and open the aperture. The noise reduction fairing (12) is positioned fore of the landing gear bay door assembly. The noise reduction fairing (12) is moveable between a stowed position and a fully deployed position such that in the fully deployed position, the noise reduction fairing (12) acts to reduce noise that would otherwise be generated by the interaction of the landing gear assembly when deployed and the air flowing past it.
摘要翻译：描述了包括飞机起落架组件（10）和降噪整流装置（12）的飞机降噪装置。起落架组件包括（10）具有孔（14）的起落架舱，可在收起位置和完全展开位置之间移动的起落架，以及至少一个起落架舱门（16），其可移动以关闭和打开光圈。降噪整流罩（12）位于起落架舱门组件的前方。降噪整流罩（12）可在收起位置和完全展开位置之间移动，使得在完全展开位置中，降噪整流罩（12）用于减少否则将由起落架组件的相互作用产生的噪音当部署和空气流过它。

4. 发明授权

US08376261B2 Landing gear 有权
标题翻译：起落架
公开(公告)号：US08376261B2
公开(公告)日：2013-02-19
申请号：US12255039
申请日：2008-10-21
申请人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
发明人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
IPC分类号： B64C1/40
CPC分类号： B64C7/00 , B64C25/16 , B64C2025/003
摘要： An aircraft landing gear is described including a noise-reducing means. In one embodiment there is a noise-reducing element that includes an air-deflecting surface, in the form of a fairing, and a perforated airflow-reducing region. In use, some air passes through the perforations, while other air is deflected by the fairing away from a noise-generating region of the landing gear. Noise caused by the passing of the landing gear through the air is therefore reduced. In another embodiment a noise-reducing layer in the form of a mesh is supported by a skeleton structure.
摘要翻译：描述了一种飞机起落架，包括减噪装置。在一个实施例中，存在噪声降低元件，其包括整流罩形式的空气偏转表面和穿孔的气流减少区域。在使用中，一些空气穿过穿孔，而其他空气被整流罩偏离起落架的噪声产生区域。因此，通过空气通过起落架引起的噪音降低了。在另一个实施例中，网状形式的降噪层由骨架结构支撑。

5. 发明授权

US08371524B2 Torque link set 有权
标题翻译：扭矩链接集
公开(公告)号：US08371524B2
公开(公告)日：2013-02-12
申请号：US12458242
申请日：2009-07-06
申请人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
发明人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
IPC分类号： B64C25/16
CPC分类号： B64C25/16 , B64C7/00 , B64C25/001 , B64C25/60 , B64C2025/003
摘要： An aircraft landing gear (10) includes a torque link set (12) comprising a first fairing (12a) rotatably connected at a first end (18) to a first end (19) of a second fairing (12b). The fairings (12a), (12b) may be arranged to act as first and second torque links. The fairings may be in the form of noise reduction fairings.
摘要翻译：飞机起落架（10）包括扭矩连杆组（12），其包括在第一整流罩（12b）的第一端（18）处可旋转地连接到第一整流罩（12b）的第一端（19）的第一整流罩（12a）。整流罩（12a），（12b）可以布置成用作第一和第二扭矩连杆。整流罩可以采用降噪整流罩的形式。

6. 发明申请

US20100012778A1 Torque link set 有权
标题翻译：扭矩链接集
公开(公告)号：US20100012778A1
公开(公告)日：2010-01-21
申请号：US12458242
申请日：2009-07-06
申请人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
发明人： Leung Choi Chow , Philip Campbell , Christopher Neil Wood
IPC分类号： B64C25/16 , B64C23/00
CPC分类号： B64C25/16 , B64C7/00 , B64C25/001 , B64C25/60 , B64C2025/003
摘要： An aircraft landing gear (10) includes a torque link set (12) comprising a first fairing (12a) rotatably connected at a first end (18) to a first end (19) of a second fairing (12b). The fairings (12a), (12b) may be arranged to act as first and second torque links. The fairings may be in the form of noise reduction fairings.
摘要翻译：飞机起落架（10）包括扭矩连杆组（12），其包括在第一整流罩（12b）的第一端（18）处可旋转地连接到第一整流罩（12b）的第一端（19）的第一整流罩（12a）。整流罩（12a），（12b）可以布置成用作第一和第二扭矩连杆。整流罩可以采用降噪整流罩的形式。

7. 发明授权

US08302906B2 Aircraft noise reduction apparatus 有权
标题翻译：飞机降噪装置
公开(公告)号：US08302906B2
公开(公告)日：2012-11-06
申请号：US12153493
申请日：2008-05-20
申请人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
发明人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
IPC分类号： B64C25/10
CPC分类号： B64C25/001 , B64C7/00 , B64C2025/003
摘要： The invention relates to aircraft noise reduction apparatus, in particular, but not exclusively, to noise reduction apparatus on an aircraft landing gear. The aircraft noise reduction apparatus comprises a noise reduction attachment for a landing gear of an aircraft. The noise reduction apparatus is movable between a first position in which it deflects air away from a noise inducing component of the landing gear and a second position in which it allows access to the noise inducing component. The movement of the noise reduction attachment between the first and second positions is actuated by a part of the landing gear.
摘要翻译：本发明涉及飞机降噪装置，特别地但不排他地涉及飞机起落架上的降噪装置。飞机降噪装置包括用于飞行器的起落架的降噪附件。降噪装置可在第一位置和第二位置之间移动，第一位置使空气偏离起落架的噪声感应部件，而第二位置允许进入噪声感应部件。第一和第二位置之间的降噪附件的运动由起落架的一部分致动。

8. 发明申请

US20110139926A1 Landing gear with noise reduction apparatus 有权
标题翻译：起降装置带降噪装置
公开(公告)号：US20110139926A1
公开(公告)日：2011-06-16
申请号：US12926796
申请日：2010-12-09
申请人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
发明人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
IPC分类号： B64C25/10 , B64C1/40
CPC分类号： B64C25/10 , B64C25/16 , B64C2025/003
摘要： An aircraft landing gear assembly comprises a landing gear (10) arranged to be moveable between a stowed position and a deployed position. The assembly includes a removably mounted cover plate (20) that covers a void (12) defined by a part of the landing gear assembly. The plate (20) may have a substantially constant thickness, one or more fixing elements (22) on one side only of the plate, and a sealing element (34) that extends around substantially the entire perimeter (20a) of the plate (20).
摘要翻译：飞机起落架组件包括起落架（10），该起落架（10）布置成能够在收起位置和展开位置之间移动。组件包括可拆卸地安装的盖板（20），其覆盖由起落架组件的一部分限定的空隙（12）。板（20）可以具有基本上恒定的厚度，仅在板的一侧上的一个或多个固定元件（22）和围绕板（20）的基本上整个周边（20a）延伸的密封元件（34））。

9. 发明申请

US20090321559A1 Aircraft noise reduction apparatus 有权
标题翻译：飞机降噪装置
公开(公告)号：US20090321559A1
公开(公告)日：2009-12-31
申请号：US12153493
申请日：2008-05-20
申请人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
发明人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
IPC分类号： B64C23/00 , B64C1/40 , B64C25/04
CPC分类号： B64C25/001 , B64C7/00 , B64C2025/003
摘要： The invention relates to aircraft noise reduction apparatus, in particular, but not exclusively, to noise reduction apparatus on an aircraft landing gear. The aircraft noise reduction apparatus comprises a noise reduction attachment for a landing gear of an aircraft. The noise reduction apparatus is movable between a first position in which it deflects air away from a noise inducing component of the landing gear and a second position in which it allows access to the noise inducing component. The movement of the noise reduction attachment between the first and second positions is actuated by a part of the landing gear.
摘要翻译：本发明涉及飞机降噪装置，特别地但不排他地涉及飞机起落架上的降噪装置。飞机降噪装置包括用于飞行器的起落架的降噪附件。降噪装置可在第一位置和第二位置之间移动，第一位置使空气偏离起落架的噪声感应部件，而第二位置允许进入噪声感应部件。第一和第二位置之间的降噪附件的运动由起落架的一部分致动。

10. 发明申请

US20090078821A1 LANDING GEAR 有权
标题翻译：起落架
公开(公告)号：US20090078821A1
公开(公告)日：2009-03-26
申请号：US12255039
申请日：2008-10-21
申请人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
发明人： Leung Choi Chow , Christopher Neil Wood , Philip Campbell
IPC分类号： B64C23/00 , B64C25/10
CPC分类号： B64C7/00 , B64C25/16 , B64C2025/003
摘要： An aircraft noise-reduction apparatus (10) for a landing gear (20) comprises a skeleton structure (14), which supports and acts to maintain the profile of a noise-reducing layer. The skeleton structure may comprise blades (16). The noise-reducing layer may have more than 10 apertures through which, in use, air can pass and may be in the form of a deformable mesh (12).
摘要翻译：用于起落架（20）的飞行器降噪装置（10）包括骨架结构（14），其支撑并用于保持降噪层的轮廓。骨架结构可以包括叶片（16）。减噪层可以具有多于10个孔，在使用中，空气可以通过，并且可以是可变形网（12）的形式。

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