TWO-CYCLE DIESEL ENGINE CONFIGURED FOR OPERATION WITH HIGH TEMPERATURE COMBUSTION CHAMBER SURFACES

A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels is disclosed. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is...

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Bibliographic Details
Main Authors DOERS DOUGLAS A, WEBB DENNIS RAYMOND, GRECO ROBERT A, OLESEN PAUL
Format Patent
LanguageChinese
English
Published 02.04.2019
Subjects
BLASTING
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels is disclosed. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes. 种构造成容纳低十六烷柴油和喷射燃料的双循环直接喷射式柴油发动机。该发动机包括燃烧室，该燃烧室具有在发动机运行期间能够在高温下运行的表面，以提高低十六烷燃料的燃烧速率。发动机还构造成减小寒冷情况和/或低压情况--比如在尝试在相对较高的高度重新启动飞行器发动机期间所经历的那些情况--下的启动时间。
Bibliography:Application Number: CN201680088118