Mounting devices for multiple flow turbojet engines
US4441313A · kind A · utility
21Cited by
4References
3Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 6, 1980 |
| Grant date | Apr 10, 1984 |
| Priority date | — |
| Expiry date | Nov 6, 2000 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T74/20588
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A mounting device for mounting the exhaust casing of a turbojet engine on a rigid support structure connected with an aircraft, there being at least two flows, i.e., a primary flow in the exhaust casing and a secondary flow in a shroud which surrounds the casing and which is fastened to the support structure by a rigid ring. The device consists of a plurality of arms each having means to control its orientation.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.