RU2016109108A - Three-chamber rotary internal combustion engine - Google Patents

Three-chamber rotary internal combustion engine Download PDF

Info

Publication number
RU2016109108A
RU2016109108A RU2016109108A RU2016109108A RU2016109108A RU 2016109108 A RU2016109108 A RU 2016109108A RU 2016109108 A RU2016109108 A RU 2016109108A RU 2016109108 A RU2016109108 A RU 2016109108A RU 2016109108 A RU2016109108 A RU 2016109108A
Authority
RU
Russia
Prior art keywords
chamber
rotor
combustion
expansion
compression
Prior art date
Application number
RU2016109108A
Other languages
Russian (ru)
Other versions
RU2663702C2 (en
Inventor
Алексей Маратович Рогульченко
Original Assignee
Алексей Маратович Рогульченко
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 Алексей Маратович Рогульченко filed Critical Алексей Маратович Рогульченко
Priority to RU2016109108A priority Critical patent/RU2663702C2/en
Publication of RU2016109108A publication Critical patent/RU2016109108A/en
Application granted granted Critical
Publication of RU2663702C2 publication Critical patent/RU2663702C2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04Charge admission or combustion-gas discharge
    • F02B53/08Charging, e.g. by means of rotary-piston pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/006Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle
    • F01C11/008Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle and of complementary function, e.g. internal combustion engine with supercharger
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Claims (4)

1. Роторный двигатель внутреннего сгорания, состоящий из камеры сжатия, камеры расширения и камеры сгорания, ротора, задвижек камеры сжатия, расширения и сгорания, канала между камерой сжатия и камерой сгорания, по которому топливная смесь перетекает из камеры сжатия в камеру сгорания, отличающийся тем, что камеры сжатия, расширения и сгорания имеют независимые объемы, ротор двигателя проходит через камеру сжатия, камеру расширения и входит в камеру сгорания, газы сгорания перетекают из камеры сгорания в камеру расширения, где совершают полезную работу, через тело ротора.1. A rotary internal combustion engine, consisting of a compression chamber, an expansion chamber and a combustion chamber, a rotor, shutters of a compression chamber, expansion and combustion, a channel between the compression chamber and the combustion chamber, through which the fuel mixture flows from the compression chamber into the combustion chamber, characterized in that the compression, expansion and combustion chambers have independent volumes, the engine rotor passes through the compression chamber, the expansion chamber enters the combustion chamber, the combustion gases flow from the combustion chamber to the expansion chamber, where work through the rotor body. 2. Двигатель по п. 1, отличающийся тем, что ротор двигателя состоит из: цилиндра ротора, который проходит через камеру сжатия, камеру расширения и входит в камеру сгорания, крыла ротора камеры сжатия, входящего в камеру сжатия и вращающегося в ней, крыла ротора камеры расширения, входящего в камеру расширения и вращающегося в ней, крыла ротора камеры сгорания, входящего в камеру сгорания и вращающегося в ней, дисков управления задвижками камер сжатия, расширения и сгорания.2. The engine according to claim 1, characterized in that the rotor of the engine consists of: a rotor cylinder that passes through the compression chamber, an expansion chamber and enters the combustion chamber, the wing of the rotor of the compression chamber included in the compression chamber and rotating in it, the wing of the rotor the expansion chamber, which is included in the expansion chamber and rotates in it, the wing of the rotor of the combustion chamber, which enters and rotates in the combustion chamber, and the control disks of the valves of the compression, expansion, and combustion chambers. 3. Двигатель по п. 2, отличающийся тем, что внутри цилиндра ротора и крыла ротора камеры расширения проходит канал, по которому газы горения перетекают из камеры сгорания в камеру расширения, где выходят из сопла крыла ротора камеры расширения в камеру расширения, в которой совершают полезную работу, вращая ротор.3. The engine according to claim 2, characterized in that a channel passes through the rotor cylinder and the wing of the rotor of the expansion chamber, through which combustion gases flow from the combustion chamber to the expansion chamber, where they exit from the nozzle of the wing of the rotor of the expansion chamber to the expansion chamber, in which useful work by rotating the rotor. 4. Двигатель по п. 1, отличающийся тем, что рабочие зоны в камерах сжатия, расширения и сгорания образуют вращающиеся в них крылья ротора и входящие/выходящие в них задвижки, положением которых управляют вращающиеся вместе с ротором управляющие задвижками диски ротора за пределами этих камер.4. The engine according to claim 1, characterized in that the working areas in the compression, expansion, and combustion chambers form the rotor wings rotating in them and the gate valves entering / leaving them, the position of which is controlled by the rotor discs controlling the gate valves rotating together with the rotor outside these chambers .
RU2016109108A 2016-03-15 2016-03-15 Three-chamber rotary engine of internal combustion RU2663702C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016109108A RU2663702C2 (en) 2016-03-15 2016-03-15 Three-chamber rotary engine of internal combustion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016109108A RU2663702C2 (en) 2016-03-15 2016-03-15 Three-chamber rotary engine of internal combustion

Publications (2)

Publication Number Publication Date
RU2016109108A true RU2016109108A (en) 2017-09-20
RU2663702C2 RU2663702C2 (en) 2018-08-08

Family

ID=59893575

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016109108A RU2663702C2 (en) 2016-03-15 2016-03-15 Three-chamber rotary engine of internal combustion

Country Status (1)

Country Link
RU (1) RU2663702C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2703431C1 (en) * 2018-09-21 2019-10-16 Алексей Маратович Рогульченко Three-zone multiblade centrifugal rotary internal combustion engine with concentric arrangement of working zones in engine rotor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3298331A (en) * 1965-04-15 1967-01-17 James L Butler Rotary heat engine
US3823695A (en) * 1973-06-04 1974-07-16 W Swartz Rotary engine
AU4043078A (en) * 1977-10-20 1980-04-17 Thill E M Sealing and cooling combustion engines with high pressure gas and liquid
US7186101B2 (en) * 1998-07-31 2007-03-06 The Texas A&M University System Gerotor apparatus for a quasi-isothermal Brayton cycle Engine
RU2407899C1 (en) * 2009-04-20 2010-12-27 Александр Дмитриевич Мезин Rotary piston ice
CN102383921B (en) * 2010-12-16 2013-02-20 李钢 Rotor engine and rotor unit thereof

Also Published As

Publication number Publication date
RU2663702C2 (en) 2018-08-08

Similar Documents

Publication Publication Date Title
RU2015115727A (en) FUEL SUPPLY CONTROL DEVICE FOR GAS ENGINE WITH SEPARATE COMBUSTION CAMERA
ATE513982T1 (en) DEVICE FOR VARIABLE ADJUSTMENT OF THE CONTROL TIMES OF GAS EXCHANGE VALVE OF AN INTERNAL COMBUSTION ENGINE
EP2990620A3 (en) Valve timing control apparatus
RU2012134623A (en) DEVICE FOR SUBMITTING A HOT MIXTURE TO THE INTERNAL COMBUSTION ENGINE AND METHOD OF OPERATION OF SUCH DEVICE
RU2015132184A (en) ENGINE SYSTEM
RU2016109108A (en) Three-chamber rotary internal combustion engine
RU2016118435A (en) INTERNAL COMBUSTION ENGINE AND CLOSING KNOT FOR IT
BR112015025105A2 (en) motion control of a moving part
ATE553292T1 (en) INTERNAL COMBUSTION ENGINE
RU2532082C2 (en) Rotary internal combustion engine
RU2012129951A (en) SPARK IGNITION INTERNAL COMBUSTION ENGINE
RU2016140582A (en) TWO-STROKE ENGINE WITH ONE CYLINDER AND A SERIES OF TWO-STROKE ENGINES
JP2015178814A5 (en)
RU2015145717A (en) Turbine of a turbocharger of an internal combustion engine and a turbine control valve assembly (options)
WO2016003182A3 (en) Heat engine
RU2018130793A (en) GAS DISTRIBUTION MECHANISM OF INTERNAL COMBUSTION ENGINE
SE1651366A1 (en) Method and system for controlling an internal combustion engine
JP2020514607A5 (en)
RU2602016C1 (en) Rotary internal combustion engine
WO2016023047A3 (en) Valve arrangement for am internal combustion engine
RU2016102745A (en) GAS TURBINE CONTAINING A COMPRESSOR HOUSING WITH INLET HOLE FOR COOLING A COMPRESSOR HOUSING, AND USING THE SPECIFIED GAS TURBINE
RU2012123512A (en) AERODYNAMIC DEVICE FOR REGULATING TEMPERATURE AND PRESSURE IN THE MEDIA FLOW TRANSPORT LINE
RU152076U1 (en) GAS DISTRIBUTION MECHANISM FOR INTERNAL COMBUSTION ENGINES
RU2581753C1 (en) Internal combustion engine control method
RU2014115327A (en) ROTARY INTERNAL COMBUSTION ENGINE

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20190316