发明公开
- 专利标题： FUSELAGE STRUCTURE FOR ACCOMODATING TAILS AND CANARDS OF DIFFERENT SIZES AND SHAPES
- 专利标题（中）： 革命武装组织联合国维和部队
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申请号： EP16190299.4申请日： 2016-09-23
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公开(公告)号： EP3181443A1公开(公告)日： 2017-06-21
- 发明人: Schmidt, Gregory M. , Walton, Samuel Thomas
- 申请人： The Boeing Company
- 申请人地址： 100 North Riverside Plaza Chicago, IL 60606-1596 US
- 专利权人： The Boeing Company
- 当前专利权人： The Boeing Company
- 当前专利权人地址： 100 North Riverside Plaza Chicago, IL 60606-1596 US
- 代理机构： Witte, Weller & Partner Patentanwälte mbB
- 优先权： US201514975115 20151218
- 主分类号： B64C1/26
- IPC分类号： B64C1/26 ; B64C5/02 ; B64C5/04 ; B64C39/12
摘要：
An aircraft (10) includes a fuselage (17) with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage (17) without changing the structural layout or configuration of the fuselage (17) structural interfaces.
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