Strut structure for suspending loads under aircraft
US4491292A · kind A · utility
1Cited by
7References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Aug 9, 1983 |
| Grant date | Jan 1, 1985 |
| Priority date | — |
| Expiry date | Aug 9, 2003 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D1/02
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
This strut structure for suspending loads under aircraft comprises essentially a hollow beam comprising at least one element of compound material consisting mainly of mineral fibres embedded in a binder forming setting resin such as expoxide resin, this element extending throughout the length of the beam, and metal members joined to the compound material element or elements for rigidly connecting the beam to the aircraft and to the means from which the load is suspended under the aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.