SU1240933A2 - Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine - Google Patents
Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine Download PDFInfo
- Publication number
- SU1240933A2 SU1240933A2 SU833703427A SU3703427A SU1240933A2 SU 1240933 A2 SU1240933 A2 SU 1240933A2 SU 833703427 A SU833703427 A SU 833703427A SU 3703427 A SU3703427 A SU 3703427A SU 1240933 A2 SU1240933 A2 SU 1240933A2
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- internal combustion
- combustion engine
- exhaust system
- pressure pulse
- pulse converter
- Prior art date
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Classifications
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- 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
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- Supercharger (AREA)
Description
Изобретение относитс к машиностроению , а именно к двигателестроению, и может быть использовано в выпускных системах двигателей внутреннего сгорани с газотурбинным наддувом.The invention relates to mechanical engineering, in particular to engine-building, and can be used in exhaust systems of gas-turbine supercharged internal combustion engines.
Цель изобретени - повышение эффективности преобразовани импульсов давлени и мош,ности двигател внутреннего сгорани .The purpose of the invention is to increase the efficiency of the conversion of pressure and mosquito pulses to the internal combustion engine.
На фиг. 1 показан преобразователь импульсов , разрез; на фиг. 2 - сечение А-А на фиг. 1.FIG. 1 shows a pulse converter, a section; in fig. 2 is a section A-A in FIG. one.
Преобразователь содержит два выхлоп - ных коллектора 1 и 2 t одинаковым проходным сечением, смесительный патрубок 3 и подвижную разделительную перегородку 4. Выхлопные коллекторы 1 и 2 подключены к цилиндрам двигател (не показаны) с неперекрываюш,имис фазами выпуска и к смесительному патрубку 3, подключенному к турбокомпрессору (не показан). Разделительна перегородка 4 установлена в смесительном патрубке 3 в месте подсоединени к нему выхлопных коллекторов 1 и 2. Разделительна перегородка 4 установлена на оси 5, расположенной в месте подсоединени выхлопных коллекторов 1 и 2 к смесительному патрубку 3 с возможностью поворота вокруг нее. Преобразователь также снабжен ограничител ми 6 и 7 поворота разделительной перегородки 4 на угол, опре- дел юш,ий отношение минимальных проходфиг . 2The converter contains two exhaust manifolds 1 and 2 t with the same flow area, mixing nozzle 3 and movable partition wall 4. Exhaust headers 1 and 2 are connected to engine cylinders (not shown) with non-overlapping exhaust phases and to mixing nozzle 3 connected to the turbocharger (not shown). The dividing wall 4 is installed in the mixing pipe 3 at the point where the exhaust manifolds 1 and 2 are connected to it. The dividing wall 4 is installed on the axis 5 located at the point where the exhaust headers 1 and 2 are connected to the mixing pipe 3 can be turned around it. The converter is also provided with limiters 6 and 7 of the rotation of the dividing partition 4 by an angle, defined by us, the ratio of the minimum passages. 2
Составите.ль В. КозловCompile. V. Kozlov
Редактор М. ДылынТехред И. ВересКорректор Т. КолбEditor M. DylynTehred I. VeresKorrektor T. Kolb
Заказ 3468/29Тираж 523ПодписноеOrder 3468/29 Circulation 523 Subscription
ВНИИПИ Государственного комитета СССРVNIIPI USSR State Committee
по делам изобретений и открытийfor inventions and discoveries
113035, Москва, Ж-35, Раушска наб., д. 4/5113035, Moscow, Zh-35, Raushsk nab. 4/5
Филиал ППП «Патент, г. Ужгород, ул. Проектна , 4Branch PPP "Patent, Uzhgorod, st. Project, 4
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ных сечений 8 и 9 по обе стороны от нее между собой в пределах 0,3-1,0.8 and 9 on either side of it between 0.3-1.0.
Преобразователь работает следуюш.им образом.The converter works in the following way.
Выхлопные газы из цилиндров двигател поступают в выхлопные коллекторы 1 и 2, в смесительный патрубок 3, а из него в турбокомпрессор , который обеспечивает наддув двигател . При прохождении активного потока газов через один из коллекторов, например I, и через его минимальное проходное сечение 8 под действием разности сил давлени перегородка 4 поворачиваетс до ограничител 7 в сторону пассивного канала, которым вл етс коллектор 2, и тем самым 5 уменьшает плош.адь проходного сечени 9. В результате уменьшаетс заброс газов в пассивный канал и увеличиваетс скорость эжекции пассивного потока. В свою очередь увеличение площади проходного сечени 8 коллектора 1 приводит к уменьшению насосных потерь в цилиндрах, из которых в данный момент происходит выпуск газов.Exhaust gases from the engine cylinders flow into the exhaust manifolds 1 and 2, into the mixing tube 3, and from there into the turbocharger, which provides engine inflation. When the active gas flow passes through one of the collectors, for example I, and through its minimum flow area 8, under the action of the pressure difference, the partition 4 rotates up to the restrictor 7 towards the passive channel, which is the collector 2, and thereby reduces the area passage section 9. As a result, the gas is reduced into the passive channel and the ejection rate of the passive flow increases. In turn, an increase in the throughput area 8 of the collector 1 leads to a decrease in pumping losses in the cylinders, from which gases are currently released.
При выпуске газов из коллектора 2 активным становитс проходное сечение 9, перегородка 4 поворачиваетс в сторону коллектора до ограничител 6 с аналогичным эффектом. За счет выполнени отношени сечений 8 и 9 в пределах 0,3-1,0 обеспечиваетс регулирование преобразовател также и в период фиксированного режима работы.With the release of gases from the collector 2, the flow section 9 becomes active, the partition 4 turns in the direction of the collector to limiter 6 with the same effect. By making the ratios of sections 8 and 9 within the range of 0.3-1.0, the converter is also controlled during the fixed operating period.
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Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU833703427A SU1240933A2 (en) | 1983-12-15 | 1983-12-15 | Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU833703427A SU1240933A2 (en) | 1983-12-15 | 1983-12-15 | Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1191611A Addition SU527131A3 (en) | 1966-10-22 | 1967-10-22 | Lever winch |
Publications (1)
Publication Number | Publication Date |
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SU1240933A2 true SU1240933A2 (en) | 1986-06-30 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU833703427A SU1240933A2 (en) | 1983-12-15 | 1983-12-15 | Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine |
Country Status (1)
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SU (1) | SU1240933A2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102444469A (en) * | 2011-12-28 | 2012-05-09 | 上海交通大学 | Turbine inlet area adjustable turbocharging system |
CN102562270A (en) * | 2011-12-28 | 2012-07-11 | 上海交通大学 | Turbine inlet area adaptive turbo charging system |
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1983
- 1983-12-15 SU SU833703427A patent/SU1240933A2/en active
Non-Patent Citations (1)
Title |
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Авторское свидетельство СССР № 1191611, кл. F02 В 37/02, 13.12.83. * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102444469A (en) * | 2011-12-28 | 2012-05-09 | 上海交通大学 | Turbine inlet area adjustable turbocharging system |
CN102562270A (en) * | 2011-12-28 | 2012-07-11 | 上海交通大学 | Turbine inlet area adaptive turbo charging system |
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