ROCKET ENGINE AND IGNITION SYSTEM

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)...

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Bibliographic Details
Main Authors OBASE Kimihito, KAWAMATA Yoshihiro
Format Patent
LanguageEnglish
Published 25.01.2018
Subjects
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary: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).
Bibliography:Application Number: US201615547995