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특허 상세정보

Spliced laminate for aircraft fuselage

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/00   
미국특허분류(USC) 244/133 ; 244/119 ; 244/123 ; 428/189
출원번호 US-0910938 (1992-07-09)
발명자 / 주소
출원인 / 주소
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 line in a second metal layer, and spaced laterally from the second splice line. An adhesive layer between the metal layers preferably contains reinforcing fibers bridging across the splice lines. An aircraft fuselage or wing or empennage made with spliced body pa...

대표
청구항

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 thickness of less than about 1 mm and comprising a first section, a second section generally coplanar with the first section and a second splice line between the first and second sections, the second splice line being spaced laterally from the first splice line by a...

이 특허를 인용한 특허 피인용횟수: 77

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