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1.
公开(公告)号:US20040118977A1
公开(公告)日:2004-06-24
申请号:US10712041
申请日:2003-11-14
Applicant: Toyota Motor Sales, U.S.A., Inc.
Inventor: Alan H. Anderson , Kathlene K. Bowman , Paul D. Teufel
IPC: B64C001/00
CPC classification number: B64C1/064 , B29C33/505 , B29C70/342 , B29C70/446 , B29L2031/3082 , B64C1/061 , B64C2001/0072 , B64C2211/00 , B64D2011/0046 , Y02T50/43
Abstract: The present invention relates to a one-piece closed-shape structure and a method for manufacturing a one-piece closed-shape structure. In particular, the present invention relates to a one-piece fuselage and a method for manufacturing a one-piece fuselage. One embodiment of the method of the invention involves the use of molding technology, tooling technology, the integration of the molding and tooling technology, and fiber placement to manufacture a one-piece closed shape structure.
Abstract translation: 本发明涉及一体封闭形状结构和一体式封闭形结构的制造方法。 特别地,本发明涉及一体式机身和一体式机身的制造方法。 本发明方法的一个实施例涉及使用成型技术,模具技术,成型和模具技术的集成以及纤维布置以制造一体式闭合形状结构。
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公开(公告)号:US20040188025A1
公开(公告)日:2004-09-30
申请号:US10712042
申请日:2003-11-14
Applicant: Toyota Motor Sales, U.S.A., Inc.
Inventor: Alan H. Anderson , Kathlene K. Bowman , Paul D. Teufel
IPC: B65H081/00
CPC classification number: B64C1/064 , B29C33/505 , B29C70/342 , B29C70/446 , B29L2031/3082 , B64C1/061 , B64C2001/0072 , B64C2211/00 , B64D2011/0046 , Y02T50/43
Abstract: The present invention relates to a one-piece closed-shape structure and a method for manufacturing a one-piece closed-shape structure. In particular, the present invention relates to a one-piece fuselage and a method for manufacturing a one-piece fuselage. One embodiment of the method of the invention involves the use of molding technology, tooling technology, the integration of the molding and tooling technology, and fiber placement to manufacture a one-piece closed shape structure.
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3.
公开(公告)号:US20020056788A1
公开(公告)日:2002-05-16
申请号:US09987612
申请日:2001-11-15
Applicant: Toyota Motor Sales, U.S.A. Inc.
Inventor: Alan H. Anderson , Kathlene K. Bowman , Paul D. Teufel
IPC: B64C001/00
CPC classification number: B64C1/064 , B29C33/505 , B29C70/342 , B29C70/446 , B29L2031/3082 , B64C1/061 , B64C2001/0072 , B64C2211/00 , B64D2011/0046 , Y02T50/43
Abstract: The present invention relates to a one-piece closed-shape structure and a method for manufacturing a one-piece closed-shape structure. In particular, the present invention relates to a one-piece fuselage and a method for manufacturing a one-piece fuselage. One embodiment of the method of the invention involves the use of molding technology, tooling technology, the integration of the molding and tooling technology, and fiber placement to manufacture a one-piece closed shape structure.
Abstract translation: 本发明涉及一体封闭形状结构和一体式封闭形结构的制造方法。 特别地,本发明涉及一体式机身和一体式机身的制造方法。 本发明方法的一个实施例涉及使用成型技术,模具技术,成型和模具技术的集成以及纤维布置以制造一体式闭合形状结构。
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