Patent · US Active

Assembly apparatus for the assembly of a fuselage section

US8266778B2 · kind B2 · utility

27Cited by
2References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 7, 2008
Grant dateSep 18, 2012
Priority date
Expiry dateMar 9, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/53961
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The present invention provides an assembly apparatus for supporting a fuselage section of an aircraft or spacecraft in an adjustable assembly position, with at least one stiffening bow for detachably stiffening the fuselage section and a rotational support, which rotatably supports the at least one stiffening bow. Also provided is a method for the assembly of a fuselage section of an aircraft or spacecraft in which an assembly position of the fuselage section is prescribed. In further steps, the fuselage section is reinforced with a stiffening bow and the stiffening bow is rotatably supported. The stiffening bow is then turned in such a way that the fuselage section rotates into the assembly position.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.