Title:
ロケットエンジン、および、点火システム
Document Type and Number:
Japanese Patent JP6416015
Kind Code:
B2
Abstract:
An ignition system (10) includes a fuel injection opening (30), a fuel reforming device (70), an ignition gas injection opening (50) and an ignition gas supply passage (52). The fuel injection opening (30) injects the hydrocarbon fuel into the combustion chamber (20). The fuel reforming device (70) reforms the hydrocarbon fuel to the ignition gas which ignites automatically through contact with the oxidizing agent. The ignition gas injection opening (50) injects the ignition gas into the combustion chamber (20). The ignition gas supply passage (52) supplies the ignition gas to the ignition gas injection opening (50) from the fuel reforming device (70).
Inventors:
Obase public official
Yoshihiro Kawamata
Yoshihiro Kawamata
Application Number:
JP2015036540A
Publication Date:
October 31, 2018
Filing Date:
February 26, 2015
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES,LTD.
International Classes:
F02K9/95
Domestic Patent References:
| JP49101718A | ||||
| JP2014159769A | ||||
| JP2007016781A | ||||
| JP2014145328A |
Foreign References:
| US20080016846 | ||||
| US20090266049 | ||||
| US20130205750 |
Attorney, Agent or Firm:
Minoru Kudo
Keisaku Nakao
Keisaku Nakao