Combustion chamber for gas turbines
US4202170A · kind A · utility
6Cited by
5References
8Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 29, 1977 |
| Grant date | May 13, 1980 |
| Priority date | — |
| Expiry date | Dec 29, 1997 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/26
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A combustion chamber for gas turbines with a variable inlet cross section for the primary air, whereby the inlet cross section is so varied in dependence on the fuel pressure determining the injection quantity that with an increasing or decreasing fuel pressure, the inlet cross section is increased or decreased.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.