MD4390C1 - Power plant with discrete jet-rotary engine - Google Patents

Power plant with discrete jet-rotary engine

Info

Publication number
MD4390C1
MD4390C1 MDA20140118A MD20140118A MD4390C1 MD 4390 C1 MD4390 C1 MD 4390C1 MD A20140118 A MDA20140118 A MD A20140118A MD 20140118 A MD20140118 A MD 20140118A MD 4390 C1 MD4390 C1 MD 4390C1
Authority
MD
Moldova
Prior art keywords
compressed air
fuel
combustion chambers
fixed
power plant
Prior art date
Application number
MDA20140118A
Other languages
Romanian (ro)
Russian (ru)
Other versions
MD4390B1 (en
Inventor
Юрий ЩИГОРЕВ
Original Assignee
Юрий ЩИГОРЕВ
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 Юрий ЩИГОРЕВ filed Critical Юрий ЩИГОРЕВ
Priority to MDA20140118A priority Critical patent/MD4390C1/en
Priority to PCT/MD2015/000005 priority patent/WO2016076693A1/en
Priority to EA201700206A priority patent/EA032399B1/en
Publication of MD4390B1 publication Critical patent/MD4390B1/en
Publication of MD4390C1 publication Critical patent/MD4390C1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • 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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Abstract

The invention relates to mechanical engineering, namely to propulsion engineering and may be used in vehicles.The power plant with discrete jet-rotary engine comprises said engine, a lubrication system, a compressed air and fuel supply system and an electronic control system. The engine consists of a guide casing (14) for the exhaust gases with a lateral inlet port and a socket for the exhaust gases, inside which are placed a shaft (6), wherein are made channels for the fuel, and on the surface of the shaft (6) is fixed with a gap for compressed air a sleeve with a flange with connector for compressed air supply. On the sleeve are fixed at least two actuating levers (5), at the ends of which are made combustion chambers (1), which communicate with compressed air and fuel feeding channels (7). The combustion chambers (1) are provided with caps (4) with automatic locking devices (3), spark plugs (2) and electric valves (8) for the supply of compressed air and fuel into the combustion chambers (1). In the casing (14) is also placed an end plate (16) with return pushers (15) and a propeller (13), fixed on a bush with a drive pulley.
MDA20140118A 2014-11-10 2014-11-10 Power plant with discrete jet-rotary engine MD4390C1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
MDA20140118A MD4390C1 (en) 2014-11-10 2014-11-10 Power plant with discrete jet-rotary engine
PCT/MD2015/000005 WO2016076693A1 (en) 2014-11-10 2015-10-29 Power unit with discrete rotary jet engine
EA201700206A EA032399B1 (en) 2014-11-10 2015-10-29 Power unit with discrete rotary jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MDA20140118A MD4390C1 (en) 2014-11-10 2014-11-10 Power plant with discrete jet-rotary engine

Publications (2)

Publication Number Publication Date
MD4390B1 MD4390B1 (en) 2015-12-31
MD4390C1 true MD4390C1 (en) 2016-07-31

Family

ID=55068710

Family Applications (1)

Application Number Title Priority Date Filing Date
MDA20140118A MD4390C1 (en) 2014-11-10 2014-11-10 Power plant with discrete jet-rotary engine

Country Status (3)

Country Link
EA (1) EA032399B1 (en)
MD (1) MD4390C1 (en)
WO (1) WO2016076693A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2667847C1 (en) * 2017-04-24 2018-09-24 Алексей Маратович Рогульченко Combined wankel engine with jet effect
RU2738193C1 (en) * 2020-03-16 2020-12-09 Алексей Маратович Рогульченко Combined rotary-piston engine with working chambers in rotor discs

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1287049A (en) * 1917-12-08 1918-12-10 Benjamin G Kramer Rotary explosion-engine.
US3712060A (en) * 1969-05-13 1973-01-23 A Sorrenti Internal combustion jet engine
US4229938A (en) * 1978-08-28 1980-10-28 Gallagher William A Rotary internal combustion engine
SU1719695A1 (en) * 1989-05-22 1992-03-15 Н.И.Степанов Jet rotor engine
RU2006642C1 (en) * 1990-07-17 1994-01-30 Николай Дмитриевич Павлов Jet engine
RU2008490C1 (en) * 1991-02-13 1994-02-28 Алексей Васильевич Корнеенко Internal combustion engine
US5319926A (en) * 1991-07-10 1994-06-14 Erno Raumfahrttechnik Thruster for spacecraft
DE4441730A1 (en) * 1994-11-23 1996-05-30 Juergen Maeritz Rotary combustion and steam power machine with back thrust and nozzle devices
RU2080469C1 (en) * 1992-03-25 1997-05-27 Иван Александрович Посвенчук Engine
RU2115817C1 (en) * 1996-07-01 1998-07-20 Михаил Иванович Весенгириев Jet rotary engine and its feed system
US6877309B1 (en) * 2001-09-19 2005-04-12 Stephen K. Rhyne Nuclear-fueled power generating system
US20050120704A1 (en) * 2003-12-03 2005-06-09 The Boeing Company System and fabrication method for actively cooling high performance components
EP1632647A1 (en) * 2004-09-01 2006-03-08 C.R.F. Società Consortile per Azioni Rotary combustion engine system and its applications

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1287049A (en) * 1917-12-08 1918-12-10 Benjamin G Kramer Rotary explosion-engine.
US3712060A (en) * 1969-05-13 1973-01-23 A Sorrenti Internal combustion jet engine
US4229938A (en) * 1978-08-28 1980-10-28 Gallagher William A Rotary internal combustion engine
SU1719695A1 (en) * 1989-05-22 1992-03-15 Н.И.Степанов Jet rotor engine
RU2006642C1 (en) * 1990-07-17 1994-01-30 Николай Дмитриевич Павлов Jet engine
RU2008490C1 (en) * 1991-02-13 1994-02-28 Алексей Васильевич Корнеенко Internal combustion engine
US5319926A (en) * 1991-07-10 1994-06-14 Erno Raumfahrttechnik Thruster for spacecraft
RU2080469C1 (en) * 1992-03-25 1997-05-27 Иван Александрович Посвенчук Engine
DE4441730A1 (en) * 1994-11-23 1996-05-30 Juergen Maeritz Rotary combustion and steam power machine with back thrust and nozzle devices
RU2115817C1 (en) * 1996-07-01 1998-07-20 Михаил Иванович Весенгириев Jet rotary engine and its feed system
US6877309B1 (en) * 2001-09-19 2005-04-12 Stephen K. Rhyne Nuclear-fueled power generating system
US20050120704A1 (en) * 2003-12-03 2005-06-09 The Boeing Company System and fabrication method for actively cooling high performance components
EP1632647A1 (en) * 2004-09-01 2006-03-08 C.R.F. Società Consortile per Azioni Rotary combustion engine system and its applications

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Двигатель внутреннего сгорания, Википедия свободная энциклопедия, 2012.05.09 (regăsit în Internet la 2015.09.07, url: https://ru.wikipedia.org/wiki/Двигатель_внутреннего_сгорания) *

Also Published As

Publication number Publication date
WO2016076693A1 (en) 2016-05-19
EA201700206A1 (en) 2017-09-29
EA032399B1 (en) 2019-05-31
MD4390B1 (en) 2015-12-31

Similar Documents

Publication Publication Date Title
GB2573853B (en) Fuel injector assembly for gas turbine engine
SE1600350A1 (en) Ramjet Engine, Hybrid
GB201812791D0 (en) Gas turbine engine system with electrical power extraction
WO2014018130A8 (en) System and method of augmenting low oil pressure in an internal combustion engine
MY172173A (en) Process and apparatus for the preparation of a cylinder oil
BR102016003820A8 (en) engine head
EP3475544A4 (en) Two-cycle diesel engine configured for operation with high temperature combustion chamber surfaces
WO2016153328A3 (en) Self-moving apparatus and components thereof
MD4390B1 (en) Power plant with discrete jet-rotary engine
BR112015032257A2 (en) introducing recirculated inlet and / or exhaust gases into an internal combustion engine cylinder
MX2017003006A (en) Method and system for providing torque-assist.
DK201270034A (en) An internal combustion engine with a combined fuel oil and fuel gas operation mode
AR102627A1 (en) ELECTRICAL CABLE HARNESS FOR FUEL GAS SYSTEM AND METHOD TO PROVIDE ELECTRICAL POWER SUPPLY FOR THE FUEL GAS SYSTEM
GB201122397D0 (en) Eco 1 hydrogen gas engine
WO2018077451A8 (en) Valve train device
EP2987982A3 (en) Exhaust valve assembly for a two-stroke internal combustion engine
WO2013068639A3 (en) Device and method for reducing fuel material slip to the atmosphere in an|internal combustion piston engine, cylinder head for an internal combustion|piston engine
MX2019012474A (en) Crankcase ventilation systems.
ES2571627A1 (en) Composite motor (Machine-translation by Google Translate, not legally binding)
MX2016007824A (en) A cylinder head.
MX2016010138A (en) Piston with an open cooling chamber having a flow-effective oil guiding surface and method for cooling said piston.
Sturman NH3 engine overview
CN204126767U (en) The explosion-proof air inlet pressure stabilizing chamber of a kind of natural gas engine
WO2016104091A1 (en) Engine
WO2015189463A3 (en) Monitoring system for gas engine

Legal Events

Date Code Title Description
FG4A Patent for invention issued
KA4A Patent for invention lapsed due to non-payment of fees (with right of restoration)
MM4A Patent for invention definitely lapsed due to non-payment of fees