RU2002130426A - ROTARY-TURBINE INTERNAL COMBUSTION ENGINE - Google Patents

ROTARY-TURBINE INTERNAL COMBUSTION ENGINE

Info

Publication number
RU2002130426A
RU2002130426A RU2002130426/06A RU2002130426A RU2002130426A RU 2002130426 A RU2002130426 A RU 2002130426A RU 2002130426/06 A RU2002130426/06 A RU 2002130426/06A RU 2002130426 A RU2002130426 A RU 2002130426A RU 2002130426 A RU2002130426 A RU 2002130426A
Authority
RU
Russia
Prior art keywords
rotary
combustion engine
internal combustion
turbine internal
exhaust
Prior art date
Application number
RU2002130426/06A
Other languages
Russian (ru)
Other versions
RU2289698C2 (en
Inventor
Евгений Алексеевич Несмеев
Original Assignee
Евгений Алексеевич Несмеев
Filing date
Publication date
Application filed by Евгений Алексеевич Несмеев filed Critical Евгений Алексеевич Несмеев
Priority to RU2002130426/06A priority Critical patent/RU2289698C2/en
Priority claimed from RU2002130426/06A external-priority patent/RU2289698C2/en
Publication of RU2002130426A publication Critical patent/RU2002130426A/en
Application granted granted Critical
Publication of RU2289698C2 publication Critical patent/RU2289698C2/en

Links

Claims (1)

Роторно-турбинный двигатель внутреннего сгорания состоит из блока, роторов, системы воспламенения топливной смеси, впрыска топлива, подачи воздуха в камеру сгорания, отвода выхлопных газов, системы охлаждения и отличается от аналога количеством вращающихся роторов, большим числом камер сгорания, формой камер сгорания, наличием шестерен в собственном картере с маслом, самопроизвольным выхлопом, способом воспламенения топливной смеси, отсутствием системы смазки внутренних узлов двигателя, способом контроля компрессии.The rotary-turbine internal combustion engine consists of a block, rotors, a fuel mixture ignition system, fuel injection, air supply to the combustion chamber, exhaust gas exhaust, cooling system and differs from the analogue in the number of rotating rotors, a large number of combustion chambers, the shape of the combustion chambers, the presence gears in own crankcase with oil, spontaneous exhaust, method of ignition of the fuel mixture, lack of lubrication system of internal engine components, method of compression control.
RU2002130426/06A 2002-11-12 2002-11-12 Rotary-turbine internal combustion engine RU2289698C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2002130426/06A RU2289698C2 (en) 2002-11-12 2002-11-12 Rotary-turbine internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2002130426/06A RU2289698C2 (en) 2002-11-12 2002-11-12 Rotary-turbine internal combustion engine

Publications (2)

Publication Number Publication Date
RU2002130426A true RU2002130426A (en) 2004-05-10
RU2289698C2 RU2289698C2 (en) 2006-12-20

Family

ID=37666980

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002130426/06A RU2289698C2 (en) 2002-11-12 2002-11-12 Rotary-turbine internal combustion engine

Country Status (1)

Country Link
RU (1) RU2289698C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090199812A1 (en) * 2003-03-21 2009-08-13 Jung Kuang Chou Structure of the rotary engine
US7637243B2 (en) * 2007-07-10 2009-12-29 Qamhiyeh Ziyad A Rotary internal combustion engine
US8056529B2 (en) 2007-07-10 2011-11-15 Qamhiyeh Ziyad A Rotary internal combustion engine for combusting low cetane fuels

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