[go: up one dir, main page]

RU2013114637A - ROTARY-TURBINE INTERNAL COMBUSTION ENGINE WITH EXTERNAL COMBUSTION CHAMBER, STEAM PHASE AND WITH OPPORTUNITY TO WORK ON THE HYDROGEN-OXYGEN MIXTURE, UNDER THE CLOSED CYCLE IN MODE OF THE MODE - Google Patents

ROTARY-TURBINE INTERNAL COMBUSTION ENGINE WITH EXTERNAL COMBUSTION CHAMBER, STEAM PHASE AND WITH OPPORTUNITY TO WORK ON THE HYDROGEN-OXYGEN MIXTURE, UNDER THE CLOSED CYCLE IN MODE OF THE MODE Download PDF

Info

Publication number
RU2013114637A
RU2013114637A RU2013114637/06A RU2013114637A RU2013114637A RU 2013114637 A RU2013114637 A RU 2013114637A RU 2013114637/06 A RU2013114637/06 A RU 2013114637/06A RU 2013114637 A RU2013114637 A RU 2013114637A RU 2013114637 A RU2013114637 A RU 2013114637A
Authority
RU
Russia
Prior art keywords
combustion chamber
well
housing
section
compressor
Prior art date
Application number
RU2013114637/06A
Other languages
Russian (ru)
Other versions
RU2551718C2 (en
Inventor
Евгений Алексеевич Несмеев
Original Assignee
Евгений Алексеевич Несмеев
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Евгений Алексеевич Несмеев filed Critical Евгений Алексеевич Несмеев
Priority to RU2013114637/06A priority Critical patent/RU2551718C2/en
Publication of RU2013114637A publication Critical patent/RU2013114637A/en
Application granted granted Critical
Publication of RU2551718C2 publication Critical patent/RU2551718C2/en

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels

Landscapes

  • Supercharger (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

Роторно-турбинный двигатель внутреннего сгорания с внешней камерой сгорания, паровой фазой и с возможностью работы на водородно-кислородной смеси, по замкнутому циклу в режиме самогенерации представляет собой корпус, состоящий из секции мотора, секции компрессора и секции связующих шестерен, которые жестко посажены на соответствующие им валы и внешней камеры сгорания, причем секции мотора и компрессора имеют сходные по конструкции роторы, расположенные с зазором к корпусу и между собой, при этом малый ротор представляет собой цилиндр с полостью и выполняет роль золотника между камерой сгорания и каналом, предназначенным для пропуска горячих газов от камеры сгорания в область вращения ротора, который представляет собой цилиндр с лопастями, помимо этого, двигатель имеет системы: подачи воды, воздуха в камеру сгорания, впрыска топлива, воспламенения топливной смеси, отвода выхлопных газов, смазки подшипников и шестерен, а также систему охлаждения корпуса и роторов и отличающийся наличием секции компрессора, расположенного на том же валу что и секция мотора, а так же тем, что камера сгорания находится вне корпуса, в которую компрессор нагнетает воздух, непосредственным впрыском топлива, воспламеняемым от стандартной свечи зажигания, а так же наличием в малом роторе секции мотора, канала, используемого при газораспределении, в зависимости от такта работы РТД в качестве проводника либо рабочего тела, либо выхлопных газов, а так же возможностью применения водяной фазы и работы в режиме самогенерации на водородно-кислородной смеси.A rotary-turbine internal combustion engine with an external combustion chamber, a vapor phase and with the ability to operate on a hydrogen-oxygen mixture, in a closed cycle in self-generation mode, is a housing consisting of a motor section, a compressor section and a section of connecting gears, which are rigidly mounted on the corresponding them the shafts and the external combustion chamber, and the sections of the motor and compressor have rotors similar in design, located with a gap to the housing and to each other, while the small rotor is a cylinder with a cavity and acts as a spool between the combustion chamber and the channel designed to pass hot gases from the combustion chamber to the area of rotation of the rotor, which is a cylinder with blades, in addition, the engine has systems: water supply, air to the combustion chamber, fuel injection, ignition of the fuel mixture, exhaust gas removal, lubrication of bearings and gears, as well as a system cooling the housing and rotors and characterized by the presence compressor section located on the same shaft as the motor section, as well as the fact that the combustion chamber is outside the housing, into which the compressor pumps air, direct fuel injection, ignited from a standard spark plug, as well as the presence of a motor section in the small rotor , the channel used in gas distribution, depending on the operating cycle of the RTD as a conductor of either the working fluid or exhaust gases, as well as the possibility of using the water phase and operating in the self-generation mode on a hydrogen-oxygen mixture.

Claims (1)

Роторно-турбинный двигатель внутреннего сгорания с внешней камерой сгорания, паровой фазой и с возможностью работы на водородно-кислородной смеси, по замкнутому циклу в режиме самогенерации представляет собой корпус, состоящий из секции мотора, секции компрессора и секции связующих шестерен, которые жестко посажены на соответствующие им валы и внешней камеры сгорания, причем секции мотора и компрессора имеют сходные по конструкции роторы, расположенные с зазором к корпусу и между собой, при этом малый ротор представляет собой цилиндр с полостью и выполняет роль золотника между камерой сгорания и каналом, предназначенным для пропуска горячих газов от камеры сгорания в область вращения ротора, который представляет собой цилиндр с лопастями, помимо этого, двигатель имеет системы: подачи воды, воздуха в камеру сгорания, впрыска топлива, воспламенения топливной смеси, отвода выхлопных газов, смазки подшипников и шестерен, а также систему охлаждения корпуса и роторов и отличающийся наличием секции компрессора, расположенного на том же валу что и секция мотора, а так же тем, что камера сгорания находится вне корпуса, в которую компрессор нагнетает воздух, непосредственным впрыском топлива, воспламеняемым от стандартной свечи зажигания, а так же наличием в малом роторе секции мотора, канала, используемого при газораспределении, в зависимости от такта работы РТД в качестве проводника либо рабочего тела, либо выхлопных газов, а так же возможностью применения водяной фазы и работы в режиме самогенерации на водородно-кислородной смеси. The rotary-turbine internal combustion engine with an external combustion chamber, a vapor phase and with the possibility of working on a hydrogen-oxygen mixture, in a closed cycle in self-generation mode, is a housing consisting of a motor section, a compressor section and a link gear section, which are rigidly mounted on the corresponding They have shafts and an external combustion chamber, and the sections of the motor and compressor have similar rotors in design, located with a gap to the housing and to each other, while the small rotor is a cylinder with cavity and acts as a spool between the combustion chamber and the channel intended for the passage of hot gases from the combustion chamber to the rotor rotation region, which is a cylinder with blades, in addition, the engine has systems: water, air into the combustion chamber, fuel injection, ignition fuel mixture, exhaust gas, lubrication of bearings and gears, as well as the cooling system of the housing and rotors and characterized by the presence of a compressor section located on the same shaft as the motor section, as well as o the combustion chamber is located outside the housing into which the compressor pumps air, by direct fuel injection, ignited from a standard spark plug, as well as by the presence in the small rotor of the motor section, the channel used for gas distribution, depending on the cycle of the RTD as a conductor or working body, or exhaust gases, as well as the possibility of applying the water phase and working in the mode of self-generation on a hydrogen-oxygen mixture.
RU2013114637/06A 2013-04-01 2013-04-01 Rotary internal combustion engine RU2551718C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2013114637/06A RU2551718C2 (en) 2013-04-01 2013-04-01 Rotary internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2013114637/06A RU2551718C2 (en) 2013-04-01 2013-04-01 Rotary internal combustion engine

Publications (2)

Publication Number Publication Date
RU2013114637A true RU2013114637A (en) 2014-10-10
RU2551718C2 RU2551718C2 (en) 2015-05-27

Family

ID=53294660

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013114637/06A RU2551718C2 (en) 2013-04-01 2013-04-01 Rotary internal combustion engine

Country Status (1)

Country Link
RU (1) RU2551718C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12163461B2 (en) 2019-08-09 2024-12-10 Astron Aerospace Llc Rotary engine, parts thereof, and methods
RU2754834C1 (en) * 2020-09-07 2021-09-07 Юрий Тимофеевич Санько Rotary detonation engine
WO2024191587A2 (en) 2023-02-24 2024-09-19 Astron Aerospace Llc Rotary engine, parts thereof, and methods

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3782340A (en) * 1972-02-04 1974-01-01 J Nam Gear-type rotary engine
US6488004B1 (en) * 1996-11-01 2002-12-03 Medis El Ltd. Toroidal internal combustion engine and method for its thermo-stabilization
RU2325542C2 (en) * 2006-06-13 2008-05-27 Алексей Кадырович Ашмарин Multi rotor internal combustion engine

Also Published As

Publication number Publication date
RU2551718C2 (en) 2015-05-27

Similar Documents

Publication Publication Date Title
US10072559B2 (en) Method of operating an engine having a pilot subchamber at partial load conditions
RU2013114637A (en) ROTARY-TURBINE INTERNAL COMBUSTION ENGINE WITH EXTERNAL COMBUSTION CHAMBER, STEAM PHASE AND WITH OPPORTUNITY TO WORK ON THE HYDROGEN-OXYGEN MIXTURE, UNDER THE CLOSED CYCLE IN MODE OF THE MODE
BR112015022381A2 (en) Rotary engine, gas compressor, and liquid pumps
MX380423B (en) PRESSURE WAVE SUPERCHARGER.
RU2532082C2 (en) Rotary internal combustion engine
TR201619065A2 (en) A MOTOR CYCLE WITH DIRECTIONABLE HEATING
RU2014116382A (en) ROTARY-TURBINE INTERNAL COMBUSTION ENGINE WITH SEPARATE COMBUSTION CHAMBER, STEAM PHASE AND OPPORTUNITY FOR WORKING ON THE HYDROGEN-OXYGEN MIXTURE ON THE CLOSED CYCLE IN THE SAMOGENE MODE
RU2012102432A (en) ROTARY-TURBINE INTERNAL COMBUSTION ENGINE
JP6241814B2 (en) Rotary engine
RU2010135645A (en) EXTERNAL COMBUSTION ROTARY ENGINE
RU2015120865A (en) GORNIK SYSTEM OF THE INTERNAL COMBUSTION OF THE MINER SYSTEM
RU2010135646A (en) ROTARY INTERNAL COMBUSTION ENGINE
GB459808A (en) Internal combustion rotary engine
RU2011130012A (en) ROTARY-REACTIVE INTERNAL COMBUSTION ENGINE
RU2010112735A (en) GEAR LOW PRESSURE ICE
RU2014136489A (en) INTERNAL COMBUSTION ROTARY ENGINE AND FUEL COMBUSTION METHOD
RU2011142930A (en) ROTARY-TURBINE INTERNAL COMBUSTION ENGINE
RU2012121007A (en) ROTARY COMPRESSOR INTERNAL COMBUSTION ENGINE
RU2016100636A (en) VAN COMBUSTION ENGINE
EA201900445A1 (en) FOUR-STROKE SPHERICAL INTERNAL COMBUSTION ENGINE WITH ROTATING MOTOR
RU2010140876A (en) CHAMBER-INJECTOR-TURBINE ENGINE
US20180274513A1 (en) Internal combustion engine with igniter cooling sleeve
GB1180419A (en) Rotary-Piston Internal Combustion Engine
RU2014120361A (en) MULTI-SECTION SINGLE-STROKE ROTOR-COMPRESSOR INTERNAL COMBUSTION ENGINE
RU2011125286A (en) ROTARY-REACTIVE INTERNAL COMBUSTION ENGINE

Legal Events

Date Code Title Description
HE9A Changing address for correspondence with an applicant
MM4A The patent is invalid due to non-payment of fees

Effective date: 20210402