发明名称 |
Methods for manufacturing composite aircraft, parts and a family of composite aircraft |
摘要 |
The invention relates to systems and methods for manufacturing composite parts for aircraft. In one innovative aspect, a system and method for adjusting a location of a center of gravity of an aircraft relative to a center of lift of a wing of the aircraft is disclosed, wherein a modular spar tunnel mold is provided and configured to be detachably fixed at a plurality of selected locations within a main mold for a fuselage portion of the aircraft. In another innovative aspect, a movable detail or mold is used for manufacturing complex composite parts for an aircraft. In yet another innovative aspect, a movable detail is used to fabricate a common feature for a plurality of different parts for one or more aircraft or a family of aircraft of similar design.
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申请公布号 |
US2006169400(A1) |
申请公布日期 |
2006.08.03 |
申请号 |
US20050249502 |
申请日期 |
2005.10.14 |
申请人 |
ADAM AIRCRAFT INDUSTRIES, INC. |
发明人 |
WILDING JOSEPH R.;OLCOTT DENNIS D. |
分类号 |
B29C47/00;B29C69/00;B64C1/00;B64C1/06;B64C1/26;B64F5/00 |
主分类号 |
B29C47/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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