Method for assembling elements of composite material for aircrafts, with stress relaxation in the elements
US9321219B2 · kind B2 · utility
1Cited by
0References
18Claims
0Family size
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Key dates
| Filing date | Jan 29, 2014 |
| Grant date | Apr 26, 2016 |
| Priority date | — |
| Expiry date | Oct 20, 2034 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB29L2031/3082
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
The invention relates to a method of assembling composite material parts (10, 12). The method makes provision for:
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.