Fuel injector for a turbine engine
US4862693A · kind A · utility
22Cited by
20References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 10, 1987 |
| Grant date | Sep 5, 1989 |
| Priority date | — |
| Expiry date | Dec 10, 2007 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C7/222
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Manifold head effects at low fuel flows in a fuel injected air breathing turbine are minimized by utilizing fuel injectors having fuel injecting tubes 66 with open ends 70 for fuel injection and provided with elongated capillary tubes 99 upstream thereof and connected to receive fuel from a fuel manifold 48.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.