Convergent flap bearing with integral hold-down device
US4784326A · kind A · utility
5Cited by
2References
1Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jul 24, 1987 |
| Grant date | Nov 15, 1988 |
| Priority date | — |
| Expiry date | Jul 24, 2007 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2250/323
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An exhaust nozzle of the type utilized with high performance supersonic aircraft is disclosed. The exhaust nozzle is variable between convergent and convergent/divergent geometries, as well as in aperture size. A bearing guiding segments of the nozzle is held within a roller track by an integral hold-down bracket.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.