Title:
ターボ機械燃焼室に空気/燃料混合物を噴射する発泡性空気力式システム
Document Type and Number:
Japanese Patent JP4695952
Kind Code:
B2
Abstract:
The aerodynamic injection system (2) has an air feed channel (6) to supply air to a tubular structure (4). A fuel passage (8) is connected to a fuel feed channel (10). A gas injection channel (12) injects gas into fuel feed channel at a pressure which is greater than pressure of air supplied to tubular structure and greater than or equal to pressure of fuel flowing in fuel feed channel, to create effervescence in fuel. Independent claims are also included for the following: (1) turbomachine combustion chamber; and (2) turbomachine.
Inventors:
Igor Manchinenkov
Thomas Noel
Alexander Novikov
Vladimir Orlov
Valery Picarov
Jill Lorrain
Thomas Noel
Alexander Novikov
Vladimir Orlov
Valery Picarov
Jill Lorrain
Application Number:
JP2005275038A
Publication Date:
June 08, 2011
Filing Date:
September 22, 2005
Export Citation:
Assignee:
SNECMA
International Classes:
F02C7/22; F02C7/232; F23R3/28
Domestic Patent References:
| JP2003214604A | ||||
| JP51127912A | ||||
| JP61155631A | ||||
| JP5302701A | ||||
| JP2003194338A |
Foreign References:
| US4189914 | ||||
| US3915387 | ||||
| US3937011 |
Attorney, Agent or Firm:
Yoshio Kawaguchi
Makoto Ono
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura
Makoto Ono
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura