Variable volume combustor with aerodynamic support struts [electronic resource].
- Published
- Washington, D.C. : United States. Dept. of Energy, 2017.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy - Additional Creators
- General Electric Company, United States. Department of Energy, and United States. Department of Energy. Office of Scientific and Technical Information
Access Online
- Restrictions on Access
- Free-to-read Unrestricted online access
- Summary
- The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts supporting the fuel nozzles and providing the flow of fuel therethrough. The support struts may include an aerodynamic contoured shape so as to distribute evenly a flow of air to the micro-mixer fuel nozzles.
- Report Numbers
- E 1.99:9,587,562
9,587,562 - Subject(s)
- Note
- Published through SciTech Connect.
03/07/2017.
"9,587,562"
"13/760,097"
Heath Michael Ostebee; Thomas Edward Johnson; Jason Thurman Stewart; Christopher Paul Keener. - Funding Information
- FC26-05NT42643
View MARC record | catkey: 23491732