System for injecting fuel in a gas turbine combustor [electronic resource]

• Ngôn ngữ: eng
• Ký hiệu phân loại: 629.135 Aircraft instrumentation (Avionics)
• 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: 266693
• Chủ đề: 1. 33 advanced propulsion systems; 2. 42 engineering

Tóm tắt

A combustion system uses a fuel nozzle with an inner wall having a fuel inlet in fluid communication with a fuel outlet in a fuel cartridge. The inner wall defines a mounting location for inserting the fuel cartridge. A pair of annular lip seals around the cartridge outer wall on both sides of the fuel outlet seals the fuel passage between the fuel inlet and the fuel outlet.