Title:
ROCKET ENGINE AND IGNITION SYSTEM
Document Type and Number:
WIPO Patent Application WO/2016/136635
Kind Code:
A1
Abstract:
An ignition system (10) is provided with: a fuel injection opening (30); a fuel reforming device (70); an ignition gas injection opening (50); and an ignition gas supply channel (52). The fuel injection opening (30) injects a hydrocarbon fuel into a combustion chamber (20). The fuel reforming device (70) reforms the hydrocarbon fuel into an ignition gas that self-ignites upon contact with an oxidizing agent. The ignition gas injection opening (50) injects the ignition gas into the combustion chamber (20). The ignition gas supply channel (52) supplies the ignition gas from the fuel reforming device (70) to the ignition gas injection opening (50).
Inventors:
OBASE KIMIHITO (JP)
KAWAMATA YOSHIHIRO (JP)
KAWAMATA YOSHIHIRO (JP)
Application Number:
PCT/JP2016/054924
Publication Date:
September 01, 2016
Filing Date:
February 19, 2016
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
F02K9/95; F02K9/44
Foreign References:
| JPS49101718A | 1974-09-26 | |||
| JP2014159769A | 2014-09-04 | |||
| JP2007016781A | 2007-01-25 | |||
| US20080016846A1 | 2008-01-24 | |||
| US20090266049A1 | 2009-10-29 | |||
| US20130205750A1 | 2013-08-15 | |||
| JP2014145328A | 2014-08-14 |
Attorney, Agent or Firm:
KUDOH Minoru (JP)
Minoru Kudo (JP)
Minoru Kudo (JP)
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