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Spliced laminate for aircraft fuselage 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/00
출원번호 US-0910938 (1992-07-09)
발명자 / 주소
  • Garesch Carl E. (New Kensington PA) Roebroeks Gerandus H. J. J. (Den Bommel NLX) Greidanus Buwe V. W. (Delft NLX) Oost Rob C. V. (Heerjansdam NLX) Gunnink Jan W. (Nieuwerkerk a/d Ijssel NLX)
출원인 / 주소
  • Structural Laminates Company (New Kensington PA 02)
인용정보 피인용 횟수 : 77  인용 특허 : 0

초록 ▼

A laminated body panel for aircraft applications comprises first and second metal layers and an adhesive layer. First and second sections in each metal layer are generally coplanar and separated by a splice line. A first splice line in a first metal layer is generally parallel to a second splice lin

대표청구항 ▼

A laminated panel comprising at least: (a) a first metal layer having a thickness of less than about 1 mm and comprising a first section, a second section generally coplanar with the first section and a first splice line between the first and second sections; (b) a second metal layer having a thickn

이 특허를 인용한 특허 (77)

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