Patent · US Active

Method for joining cured stringers to at least one structural component of an aircraft or spacecraft

US8808493B2 · kind B2 · utility

0Cited by
6References
5Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 19, 2011
Grant dateAug 19, 2014
Priority date
Expiry dateFeb 4, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T156/1089
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

The invention relates to a method for joining cured stringers to at least one structural component of an aircraft or spacecraft, including placing the stringers onto the at least one structural component, depositing and pressing respective vacuum film strips such that each strip is attached to a pair of stringers and present between the pair of stringers with the use of vacuum sealing means in such a manner that a continuous vacuum arrangement, comprising the covering vacuum films and the vacuum film strips, is formed, and pressurized joining of the stringers to the at least one structural component by means of the continuous vacuum arrangement formed.

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