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公开(公告)号：US20050269445A1
公开(公告)日：2005-12-08
申请号：US11073646
申请日：2005-03-08
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266 , F16C23/10 , F16C2326/43
摘要： The invention pertains to an engine mount onto an aircraft structure comprising at least one connection means between a first and a second element such as an engine case and said structure, characterized by the fact that said connection means comprises an eccentric member housed in a bore of the first element, being rotational about a first axis, the eccentric member comprising a trunnion attached to the second element and of axis off-centred with respect to the first axis of rotation, the eccentric member being rotational about said off-centred axis. The solution of the invention has the advantage of allowing a compact assembly.
摘要翻译： 本发明涉及一种在飞机结构上的发动机支架，其包括在诸如发动机壳体和所述结构的第一和第二元件之间的至少一个连接装置，其特征在于，所述连接装置包括容纳在 所述第一元件围绕第一轴线旋转，所述偏心构件包括附接到所述第二元件的耳轴和相对于所述第一旋转轴线偏心的所述偏心构件，所述偏心构件围绕所述偏心轴线旋转。 本发明的解决方案具有允许紧凑的组装的优点。
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公开(公告)号：US07325770B2
公开(公告)日：2008-02-05
申请号：US11073646
申请日：2005-03-08
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266 , F16C23/10 , F16C2326/43
摘要： The invention pertains to an engine mount onto an aircraft structure comprising at least one connection means between a first and a second element such as an engine case and said structure, characterized by the fact that said connection means comprises an eccentric member housed in a bore of the first element, being rotational about a first axis, the eccentric member comprising a trunnion attached to the second element and of axis off-centred with respect to the first axis of rotation, the eccentric member being rotational about said off-centred axis.The solution of the invention has the advantage of allowing a compact assembly.
摘要翻译： 本发明涉及一种在飞机结构上的发动机支架，其包括在诸如发动机壳体和所述结构的第一和第二元件之间的至少一个连接装置，其特征在于，所述连接装置包括容纳在 所述第一元件围绕第一轴线旋转，所述偏心构件包括附接到所述第二元件的耳轴和相对于所述第一旋转轴线偏心的所述偏心构件，所述偏心构件围绕所述偏心轴线旋转。 本发明的解决方案具有允许紧凑的组装的优点。
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