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公开(公告)号：US20170066528A1
公开(公告)日：2017-03-09
申请号：US15295262
申请日：2016-10-17
CPC分类号： B64C23/072 , B64C3/56 , Y02T50/164 , Y10T29/49826
摘要： A wing tip device for attachment to a wing tip of a powered aircraft including: a first mounting formation, a second mounting formation spaced apart in a spanwise direction relative to the first mounting formation, a third mounting formation spaced apart in a chordwise direction relative to the first and second mounting formations, wherein each of the first, second and third mounting formations are configured for attachment to at least one of a wing spar and a wing rib, and, at least one of the mounting formations is configured to permit movement of a portion of the wing tip device in the spanwise direction relative to a portion of the wing tip.
摘要翻译： 一种用于附接到动力飞行器的翼尖的翼尖装置，包括：第一安装结构，相对于第一安装结构沿翼展方向间隔开的第二安装结构，相对于第一安装结构沿着弦方向间隔开的第三安装结构 第一和第二安装结构，其中第一，第二和第三安装结构中的每一个被构造成用于附接到翼梁和翼肋中的至少一个，并且至少一个安装结构被构造成允许 所述翼尖装置的翼展方向的一部分相对于所述翼尖的一部分。
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公开(公告)号：US20190225324A1
公开(公告)日：2019-07-25
申请号：US16369075
申请日：2019-03-29
摘要： An aircraft wing subassembly including: a wing skin defining a first outer surface, and, a structural reinforcement member, the structural reinforcement member defining a second outer surface, wherein the structural reinforcement member is arranged within the wing such that the first outer surface and the second outer surface form part of an outer wing surface.
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公开(公告)号：US20180297687A1
公开(公告)日：2018-10-18
申请号：US16014341
申请日：2018-06-21
发明人： Tony FONG , Timothy AXFORD , Julien CHAUSSEE
摘要： A winglet is disclosed having a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap.
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公开(公告)号：US20190225325A1
公开(公告)日：2019-07-25
申请号：US16369222
申请日：2019-03-29
CPC分类号： B64C23/072 , B64C3/56 , Y02T50/164 , Y10T29/49826
摘要： A method of assembling a wing tip device to a wing of a powered aircraft including: providing a wing tip, providing a wing tip device, pivotably attaching the wing tip device to the wing at a first position, pivoting the wing tip device about the first position, and attaching the wing tip device to the wing at a second position spaced from the first position.
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公开(公告)号：US20160075429A1
公开(公告)日：2016-03-17
申请号：US14785114
申请日：2014-04-17
发明人： Tony FONG , Timothy AXFORD , Julien CHAUSSEE
CPC分类号： B64C3/185 , B29C70/222 , B29C70/30 , B29C70/32 , B29L2031/3085 , B32B38/1866 , B32B2305/72 , B64C23/069 , B64F5/10 , Y02T50/164 , Y02T50/43
摘要： A winglet comprising a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap.
摘要翻译： 小翼包括管状主翼梁，其具有通过上和下主翼梁盖连接的前和后主翼梁; 具有前翼梁腹板的前翼梁，上前翼梁盖和下前翼梁盖; 连接到上主翼梁帽和上前翼梁的上皮; 以及连接到下主翼梁帽和下前翼梁帽的下皮。 小翼通过将上皮肤与上主翼梁帽和上前翼梁帽共同固化来制造; 并将下部皮肤共同固化到下部主翼梁帽和下部前翼梁帽上。
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