Holder arrangement for an aircraft or a spacecraft and an aircraft or a spacecraft
US8561266B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Oct 26, 2009 |
| Grant date | Oct 22, 2013 |
| Priority date | — |
| Expiry date | Feb 13, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T24/44
- WIPO fieldMechanical elements
- WIPO sectorMechanical engineering
Abstract
In a holder arrangement of an aircraft or spacecraft comprising a structural member, a holder comprising at least one lower part and at least one upper part is provided, and these are formed so as to be able to be clamped together to be attached with a non-positive fit to a fastening portion of the structural member. The fastening portion can be clamped between the lower part and the upper part. The holder arrangement is characterised by at least one fixing strip which can be connected to the fastening portion of the structural member in the longitudinal direction thereof and which comprises a fixing profile for fixing the holder to the structural member in the longitudinal direction of the structural member with a positive fit. An aircraft or spacecraft has at least one holder arrangement of this type.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.