RU2012129329A - DEVICE ENGINE DEVICE - Google Patents
DEVICE ENGINE DEVICE Download PDFInfo
- Publication number
- RU2012129329A RU2012129329A RU2012129329/06A RU2012129329A RU2012129329A RU 2012129329 A RU2012129329 A RU 2012129329A RU 2012129329/06 A RU2012129329/06 A RU 2012129329/06A RU 2012129329 A RU2012129329 A RU 2012129329A RU 2012129329 A RU2012129329 A RU 2012129329A
- Authority
- RU
- Russia
- Prior art keywords
- receiver
- combustion chamber
- gas
- air
- piston
- Prior art date
Links
Classifications
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
Устройство адиабатного двигателя работающего по термодинамическому циклу, где процессы реализуются по два такта в двух цилиндрах с поршнем, а сгорание и первичное расширение организовано в отдельной теплоизолированной камере сгорания, объединенной с ресивером генерируемого газа, отличающееся тем, что в одном цилиндре с поршнем воздух сжимается и подается в ресивер воздуха, затем он подается под углом к оси отдельной камеры сгорания оснащенной форсункой и свечой зажигания, кроме этого воздух нагнетается в пространство вокруг ребренных стенок камеры сгорания, к которой примыкает эжектор с раструбом, что обеспечивает выход нагретого сжатого воздуха вокруг камеры сгорания и рабочего тела в теплоизолированное устройство камеры сгорания с ресивером газа оборудованного предохранительным клапаном, в ресивере поддерживается газ с относительно постоянным пониженным давлением и температурой, для получения механической работы газ с ресивера подается с постоянным давлением в цилиндр с поршнем, где газ повторно расширяется, охлаждается и выбрасывается в атмосферу, т.е двойное расширение рабочего тела с много кратным понижением температуры и давления в теплоизолированном устройстве значительного объема обеспечивает работу двигателя без системы охлаждения, что повышает теплоиспользование (КПД двигателя).A device for an adiabatic engine operating in a thermodynamic cycle, where the processes are implemented in two cycles in two cylinders with a piston, and combustion and primary expansion are organized in a separate heat-insulated combustion chamber combined with a receiver of generated gas, characterized in that the air is compressed in one cylinder and the piston is supplied to the air receiver, then it is supplied at an angle to the axis of a separate combustion chamber equipped with a nozzle and spark plug, in addition, air is pumped into the space around the fins walls of the combustion chamber, to which an ejector with a bell is adjacent, which ensures the release of heated compressed air around the combustion chamber and the working fluid into a heat-insulated combustion chamber device with a gas receiver equipped with a safety valve, a gas with a relatively constant reduced pressure and temperature is maintained in the receiver to obtain a mechanical During operation, gas from the receiver is supplied with constant pressure to the cylinder with a piston, where the gas is re-expanded, cooled and released into the atmosphere, i.e., double expansion of the working fluid with many fold decrease in temperature and pressure in the heat insulated device provides a significant amount of the engine without a cooling system, which increases teploispolzovanie (motor efficiency).
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012129329/06A RU2541490C2 (en) | 2012-07-12 | 2012-07-12 | Adiabatic engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012129329/06A RU2541490C2 (en) | 2012-07-12 | 2012-07-12 | Adiabatic engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2012129329A true RU2012129329A (en) | 2014-01-20 |
RU2541490C2 RU2541490C2 (en) | 2015-02-20 |
Family
ID=49944894
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2012129329/06A RU2541490C2 (en) | 2012-07-12 | 2012-07-12 | Adiabatic engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2541490C2 (en) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4336686A (en) * | 1978-04-21 | 1982-06-29 | Combustion Research & Technology, Inc. | Constant volume, continuous external combustion rotary engine with piston compressor and expander |
SE422346B (en) * | 1980-07-02 | 1982-03-01 | Hedelin Lars G B | SET TO CONTROL THE PROCEDURE IN A COMBUSTION ENGINE AND COMBUSTION ENGINE FOR REALIZING THE SET |
US5964087A (en) * | 1994-08-08 | 1999-10-12 | Tort-Oropeza; Alejandro | External combustion engine |
DE59700306D1 (en) * | 1997-02-14 | 1999-09-09 | Amoco Corp | Cyclic combustion engine |
DE19746945A1 (en) * | 1997-10-23 | 1999-04-29 | Dietmar Dipl Ing Stope | Internal combustion engine with combustion chamber and heat exchanger |
RU2167315C2 (en) * | 1999-04-29 | 2001-05-20 | Фролов Михаил Петрович | Thermodynamic cycle for internal combustion engine and device for executing the cycle |
-
2012
- 2012-07-12 RU RU2012129329/06A patent/RU2541490C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2541490C2 (en) | 2015-02-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20150313 |