Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans [electronic resource]

• Ngôn ngữ: eng
• Ký hiệu phân loại: 629.117 Other branches of engineering
• Thông tin xuất bản: Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2015
• Mô tả vật lý: Medium: ED : , digital, PDF file.
• Bộ sưu tập: Metadata
• ID: 266033
• Chủ đề: 1. 33 advanced propulsion systems

Tóm tắt

 A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet
  an outer casing (24) defining a plenum (22) in which the combustor can is disposed
  and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.