Title:
共鳴離調させるようになった回転空気弁発火パターン
Document Type and Number:
Japanese Patent JP5576683
Kind Code:
B2
Abstract:
An engine (100) contains a compressor stage (101), a plurality of pulse detonation combustors (103) and a rotary inlet valve structure (105) having a plurality of inlet ports through which at least air flows to enter the pulse detonation combustors during operation of the engine. Downstream of the pulse detonation combustors is a turbine stage (111). Further, the ratio of the pulse detonation combustors to the inlet ports is a non-integer.
Inventors:
James Frederick ウィーデン Hofer
Adam Rashid
Adam Rashid
Application Number:
JP2010055240A
Publication Date:
August 20, 2014
Filing Date:
March 12, 2010
Export Citation:
Assignee:
General Electric Co.
International Classes:
F02C5/12; F02C5/02; F02K7/06
Attorney, Agent or Firm:
Satoshi Arakawa
Hiroshi Ogura
Toshihisa Kurokawa
Hiroshi Ogura
Toshihisa Kurokawa