Variable volume combustor with pre-nozzle fuel injection system [electronic resource]

• Ngôn ngữ: eng
• Ký hiệu phân loại: 623.851 Military and nautical engineering
• Thông tin xuất bản: Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2016
• Mô tả vật lý: Medium: ED : , digital, PDF file.
• Bộ sưu tập: Metadata
• ID: 265927
• Chủ đề: 1. 33 advanced propulsion systems; 2. 42 engineering

Tóm tắt

The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of fuel nozzles, a pre-nozzle fuel injection system supporting the fuel nozzles, and a linear actuator to maneuver the fuel nozzles and the pre-nozzle fuel injection system.