SU1460372A1 - Method of operation of four-stroke two-chamber supercharged internal combustion engine - Google Patents

Method of operation of four-stroke two-chamber supercharged internal combustion engine Download PDF

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Publication number
SU1460372A1
SU1460372A1 SU874259510A SU4259510A SU1460372A1 SU 1460372 A1 SU1460372 A1 SU 1460372A1 SU 874259510 A SU874259510 A SU 874259510A SU 4259510 A SU4259510 A SU 4259510A SU 1460372 A1 SU1460372 A1 SU 1460372A1
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SU
USSR - Soviet Union
Prior art keywords
additional
air
cylinder
chamber
fuel
Prior art date
Application number
SU874259510A
Other languages
Russian (ru)
Inventor
Аркадий Иосифович Хуциев
Original Assignee
Коломенский Филиал Всесоюзного Заочного Политехнического Института
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Priority to SU874259510A priority Critical patent/SU1460372A1/en
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Publication of SU1460372A1 publication Critical patent/SU1460372A1/en

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    • 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

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Abstract

Изобретение позвол ет снизить механическую напр женность двигател  путем уменьшени  динамики цикла, а также теплонапр женность дополнительной камеры сгорани  (КС). В цилиндр через КС 4 при помощи впускного клапана 10 с фазами работы, совпадающими с фазами работы впускного клапапроизвод т подачу дополнительна 1 1 него воздуха, сжатого до давлени , превьшающего давление сжатого воздуха , подаваемого в цилиндр через клапан 11, При поступлении воздуха в КС 4, а затем в цилиндр через канал 7 клапана 10 при открытых клапанах 6 и 10 через форсунку 5 впрыскивают первую порцию топлива в количестве 5-15% от общей цикловой подачи топлива в двигатель после завершени  процесса продувки на такте впуска и в цилиндр направл ют из КС 4 топливо- воздушную смесь, а затем дополнитель- ный воздух, который предварительно нагревают или охлаждают. 2 з.п. ф-лы, 2 ил. о (ЛThe invention allows to reduce the mechanical stress of the engine by reducing the dynamics of the cycle, as well as the thermal stress of the additional combustion chamber (CS). Into the cylinder through CS 4 with the help of the inlet valve 10 with the work phases coinciding with the work phases of the inlet valve, an additional 1 1 him of air is supplied, compressed to a pressure that exceeds the pressure of the compressed air supplied to the cylinder through valve 11, When air enters the COP 4 and then in the cylinder through the channel 7 of the valve 10 with the valves 6 and 10 open, through the nozzle 5, the first portion of fuel is injected in an amount of 5-15% of the total fuel supply cycle to the engine after the purging process is completed during the intake stroke and into the cylinder of COP dissolved Aulus 4 fuel-air mixture, and then The additional air which is heated or cooled. 2 hp f-ly, 2 ill. o (l

Description

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Claims (3)

Формула изобрет е.нияClaim 1. Способ работы четырехтактного .двухкамерного двигателя внутреннего сгорания с наддувом путем предвари- ' ’ тельного сжатия воздуха в компрессоре, подачи его в цилиндр через впускной клапанподачи в цилиндр топливово.здушной смеси, сжатия ее с одновременным перепуском в дополнительную камеру в количестве, пропорциональном нагрузке двигателя, подачи топлива в основную и дополнительную камеры сгорания с образованием в них топливовоздушной смеси с одинаковым коэффициентом избытка воздуха, воспламенения смеси в основной и дополнительной камерах, расширения газов в цилиндре и выпуска отработавших газов с последующим расширением их На турбине, отличающийся тем, что,с целью снижения механической напряженности двигателя путем уменьшения, динамики цикла, в цилиндр через дополнительную камеру при помощи дополнительного клапана с фазами работы, совпадающими с фазами работы впускного . клапана, производят подачу дополнительного, воздуха, сжатого до давления, превышающего давление сжатого /1. The method of operation of a four-stroke. Two-chamber internal combustion engine with pressurization by preliminary compression of the air in the compressor, supplying it to the cylinder through the inlet valve, supplying the air-fuel mixture to the cylinder, compressing it while transferring it to the additional chamber in an amount proportional to the load engine, supplying fuel to the primary and secondary combustion chambers with the formation of an air-fuel mixture in them with the same coefficient of excess air, igniting the mixture in the main and additional chambers, expanding the gases in the cylinder and exhaust exhaust with their subsequent expansion On the turbine, characterized in that, in order to reduce the mechanical tension of the engine by reducing the dynamics of the cycle, into the cylinder through the additional chamber using an additional valve with the phases of operation coinciding with the phases inlet work. valves, supply additional air compressed to a pressure exceeding the compressed pressure / воздуха, подаваемого в цилиндр через впускной клапан, причем во время подачи дополнительного воздуха производят в дополнительную камеру дополнительную подачу топлива в количестве 5-15% от суммарной цикловой подачи, обеспечивая последовательную подачу в цилиндр из дополнительной камеры топливовоздушной смеси, а затем дополнительного воздуха.air supplied to the cylinder through the inlet valve, and during the supply of additional air, additional fuel is supplied to the additional chamber in an amount of 5-15% of the total cyclic supply, providing a sequential supply of air-fuel mixture to the cylinder from the additional chamber, and then additional air. 2. Способ поп.!·, отличающийся тем, что дополнительный воздух перед подачей в дополнитель- 5 ную камеру нагревают.2. The method of pop.! ·, Characterized in that the additional air is heated before being fed into the additional 5th chamber. 3. Способ поп.1, о тлич а ющ и й с я тем, что, с целью снижения теплонапряженности дополнительной камеры сгорания, дополнительный3. The method of pop. 1, different from the fact that, in order to reduce the heat stress of the additional combustion chamber, an additional 10 воздух перед подачей в дополнительную камеру охлаждают.10, the air is cooled before being fed into the additional chamber. оabout Составитель Л.Павлович Compiled by L. Pavlovich
SU874259510A 1987-04-13 1987-04-13 Method of operation of four-stroke two-chamber supercharged internal combustion engine SU1460372A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU874259510A SU1460372A1 (en) 1987-04-13 1987-04-13 Method of operation of four-stroke two-chamber supercharged internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU874259510A SU1460372A1 (en) 1987-04-13 1987-04-13 Method of operation of four-stroke two-chamber supercharged internal combustion engine

Publications (1)

Publication Number Publication Date
SU1460372A1 true SU1460372A1 (en) 1989-02-23

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SU874259510A SU1460372A1 (en) 1987-04-13 1987-04-13 Method of operation of four-stroke two-chamber supercharged internal combustion engine

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4135135A1 (en) * 1991-10-24 1993-04-29 Theo Goepel SELF-IGNITIONING PISTON COMBUSTION ENGINE
WO2009091282A3 (en) * 2007-12-29 2009-09-24 Sergeev Alexandr Nikolaevich Internal combustion engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Авторское свидетельство СССР № 1355734, кл. F 02 В 37/00, 1986. *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4135135A1 (en) * 1991-10-24 1993-04-29 Theo Goepel SELF-IGNITIONING PISTON COMBUSTION ENGINE
WO2009091282A3 (en) * 2007-12-29 2009-09-24 Sergeev Alexandr Nikolaevich Internal combustion engine
US8235023B2 (en) 2007-12-29 2012-08-07 Alexandr Nikolaevich Sergeev Internal combustion engine

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