SUPERCRITICAL FUEL INJECTION SYSTEM
A fuel injection system for gas turbines or the like, which includes a pair of high pressure pumps which provide fuel and a carrier fluid such as air at pressures above the critical pressure of the fuel, was developed. A supercritical mixing chamber mixes the fuel and carrier fluid and the mixture is sprayed into a combustion chamber for burning therein. The use of fuel and a carrier fluid at supercritical pressures promotes rapid mixing of the fuel in the combustion chamber so as to reduce the formation of pollutants and promote cleaner burning.
- This is an application for a U.S. Patent. This Government-owned invention available for U.S. licensing and, possibly, for foreign licensing. Copy of application available NTIS.
Department of the NavyThe Pentagon
Washington, DC United States 20350
- Marek, C J
- Cooper, L P
- Publication Date: 1978-6-19
- Pagination: 10 p.
- TRT Terms: Air quality management; Clean fuels; Combustion chambers; Exhaust gases; Fluids; Fuel injection; Fuel systems; Gas turbines; Internal combustion engines; Mixing; Mixtures; Patent applications; Pressure; Pumps; Turbine engines
- Old TRIS Terms: Supercritical pressures
- Subject Areas: Highways; Vehicles and Equipment;
- Accession Number: 00185757
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: PAT-APPL-916654
- Files: TRIS
- Created Date: Dec 29 1979 12:00AM