Title:
The flight vehicles equipped with the turbo organization having a detonation chamber, and a turbo organization
Document Type and Number:
Japanese Patent JP5985613
Kind Code:
B2
Abstract:
The turbomachine (1) has a continuous detonation wave engine (6) provided with an annular detonation chamber (7), and a fuel injection system (8) and a priming unit (9) for continuous production of hot gas (F3) from a detonation mixture of fuel and air. A turbine (5) is rotatably driven by the hot gas, and drives a compressor (3). An ejector/mixer system (10) mixes the gas from the chamber with air flow (F2) before directing the gas toward the turbine. The chamber is arranged with another detonation chamber in a concentric manner relative to an axis (2) of the turbomachine.
Inventors:
Fallenpan, Francois
Luna Wool, Bruno
Luna Wool, Bruno
Application Number:
JP2014510850A
Publication Date:
September 06, 2016
Filing Date:
May 09, 2012
Export Citation:
Assignee:
MBDA FRANCE
International Classes:
F02K3/06; F23R7/00
Domestic Patent References:
| JP2006029325A | ||||
| JP8135503A | ||||
| JP2009057955A |
Foreign References:
| US20090193786 | ||||
| US20100050592 | ||||
| GB1069217A | ||||
| WO2011037597A1 | ||||
| US3777488 |
Attorney, Agent or Firm:
Hiroe Associates Patent Office