Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle [electronic resource]

• Ngôn ngữ: eng
• Ký hiệu phân loại: 629.4 Astronautics
• Thông tin xuất bản: Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2013
• Mô tả vật lý: Medium: ED : , digital, PDF file.
• Bộ sưu tập: Metadata
• ID: 267211
• Chủ đề: 1. 33 advanced propulsion systems

Tóm tắt

A combustion system includes a first combustion chamber and a second combustion chamber. The second combustion chamber is positioned downstream of the first combustion chamber. The combustion system also includes a pre-mixed, direct-injection secondary fuel nozzle. The pre-mixed, direct-injection secondary fuel nozzle extends through the first combustion chamber into the second combustion chamber.