CN102678284A - Mechanical regulating type turbine bleeding system - Google Patents
Mechanical regulating type turbine bleeding system Download PDFInfo
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- CN102678284A CN102678284A CN2012101362814A CN201210136281A CN102678284A CN 102678284 A CN102678284 A CN 102678284A CN 2012101362814 A CN2012101362814 A CN 2012101362814A CN 201210136281 A CN201210136281 A CN 201210136281A CN 102678284 A CN102678284 A CN 102678284A
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- 230000000740 bleeding effect Effects 0.000 title 1
- 230000001105 regulatory effect Effects 0.000 title 1
- 238000007789 sealing Methods 0.000 claims description 5
- 238000000034 method Methods 0.000 abstract description 6
- 238000002485 combustion reaction Methods 0.000 abstract description 4
- 238000004880 explosion Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 description 6
- 230000008878 coupling Effects 0.000 description 5
- 238000010168 coupling process Methods 0.000 description 5
- 238000005859 coupling reaction Methods 0.000 description 5
- 230000003750 conditioning effect Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000005474 detonation Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000007812 deficiency Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
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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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Abstract
一种内燃机技术领域的机械调节式涡轮放气系统，包括：压气机、涡轮、发动机、连接管、容积腔、移动体和弹性部件，第一连接管的两端分别与涡轮出气管、容积腔左壁面相连通，第二连接管的两端分别与发动机排气管、容积腔左壁面相连通，移动体安装在容积腔内，移动体通过弹性部件与容积腔下壁面相连接。在工作过程中，移动体可以在容积腔内上下移动。在发动机的低速工况，移动体向下移动，发动机的排气全部流经涡轮，发动机进气量相对增大，各缸燃烧较好；在发动机的高速工况，移动体向上移动，发动机的排气有一部分直接流入涡轮出气管，发动机进气量相对减小，各缸爆压降低。本发明设计合理，结构简单，适用于发动机的涡轮增压系统。
A mechanically adjustable turbine deflation system in the technical field of internal combustion engines, comprising: a compressor, a turbine, an engine, a connecting pipe, a volume chamber, a moving body and an elastic component, and the two ends of the first connecting pipe are connected to the turbine outlet pipe and the volume chamber respectively. The left wall is connected, and the two ends of the second connecting pipe are respectively connected with the engine exhaust pipe and the left wall of the volume chamber. The mobile body is installed in the volume chamber, and the mobile body is connected with the lower wall of the volume chamber through elastic components. During the working process, the mobile body can move up and down in the volume cavity. In the low-speed working condition of the engine, the moving body moves downward, and all the exhaust gas of the engine flows through the turbine, the intake air volume of the engine increases relatively, and the combustion of each cylinder is better; in the high-speed working condition of the engine, the moving body moves upward, and the engine Part of the exhaust gas flows directly into the turbine outlet pipe, the intake air volume of the engine is relatively reduced, and the explosion pressure of each cylinder is reduced. The invention has reasonable design and simple structure, and is suitable for the turbocharging system of the engine.
Description
Technical field
What the present invention relates to is the mechanical conditioning type turbine blow-off system of a kind of gas handling system of field of internal combustion engine, particularly turbosupercharged engine.
Background technique
Along with development of modern society, people require increasingly high to the power character and the Economy of motor.Under the certain situation of discharge capacity, want to improve the output power of motor, effective method just provides more fuel and burns.Provide more fuel to be easy to accomplish through oil nozzle to cylinder, yet the air quantity that is complementary with the fuel quantity that increases will be provided simultaneously, but do not accomplish so easily; Fuel burns under the prerequisite of air quantity deficiency, and firing effect is relatively poor.Certain when fuel injection quantity, when cylinder intake air quantity was big, then burning was better, and oil consumption is lower with discharging.The degree of vacuum that traditional naturally aspirated engine forms in cylinder when relying on piston to move downward fully sucks air, and the air that this traditional mode is difficult to q.s is provided is to support the perfect combustion of fuel.Therefore, the burning that is intended for motor provides enough air, makes the power character and the better economy of motor, and turbocharging technology is being played the part of very important role.But existing turbo charge system all can not be taken into account the high and low rotating speed operating mode of motor preferably.
Retrieval through to the existing technology document is found; Chinese patent ZL200410050996.3; Patent name: the variable modular pulse converter supercharging device of a kind of turbo-charged diesel; This patented technology provides the device of the shared volume continuous variable of exhaust in a kind of outlet pipe, can take into account the high and low rotating speed operating mode of motor preferably; But the variation of exhaust institute volume is to realize through moving up and down of movement rod in its outlet pipe; This just needs to increase the special control mechanism of a cover and controls moving of movement rod; Thereby the more complicated that the pressurization system structure is become, and the sealing of its exhaust piping is also relatively poor under high-temperature condition.
Summary of the invention
The present invention is directed to the deficiency of above-mentioned existing technology, a kind of mechanical conditioning type turbine blow-off system is provided, can take into account the high and low rotating speed operating mode of motor preferably.
The present invention realizes through following technological scheme; The present invention includes: compressor air inlet machine pipe, gas compressor, engine air inlet tube, motor, engine exhaust pipe, turbine, turbine steam outlet pipe, coupling shaft, first connecting tube, second connecting tube, cavity volume, cavity volume upper wall surface, cavity volume lower wall surface, cavity volume left side wall, the right wall of cavity volume, cavity volume front face, cavity volume rear surface, moving body and elastic member; Gas compressor links to each other through coupling shaft is coaxial with turbine; The air inlet/outlet of gas compressor is connected with the air outlet of compressor air inlet machine pipe, the suction port of engine air inlet tube respectively; The air inlet/outlet of motor is connected with the air outlet of engine air inlet tube, the suction port of engine exhaust pipe respectively; The air inlet/outlet of turbine is connected with the air outlet of engine exhaust pipe, the suction port of turbine steam outlet pipe respectively; The two ends of first connecting tube are connected with turbine steam outlet pipe, cavity volume left side wall respectively; The two ends of second connecting tube are connected with engine exhaust pipe, cavity volume left side wall respectively, and cavity volume upper wall surface, cavity volume lower wall surface, cavity volume left side wall, cavity volume right wall, cavity volume front face, the cavity volume rear surface is fixed is one, and moving body is installed in the cavity volume; Moving body contacts with the internal face sealing of cavity volume, and moving body is connected with the cavity volume lower wall surface through elastic member.The cross section of cavity volume is a rectangular, and elastic member is a spring.
In working procedure of the present invention, moving body can move up and down in cavity volume.When motor is in high-speed working condition; The engine exhaust pipe internal pressure is higher; Moving body moves up and tensile elasticity parts upwards, and a part of exhaust in the cavity volume flows in the turbine steam outlet pipe through first connecting tube, thereby makes the acting ability drop of turbine; The air inflow of motor reduces relatively, and each cylinder detonation pressure reduces; When motor is in the low speed operating mode; The engine exhaust pipe internal pressure is lower, and under the effect of elastic member, moving body moves down; Do not have in the cavity volume in exhaust flows in the turbine steam outlet pipe through first connecting tube; Thereby the acting ability of turbine is strengthened relatively, and the air inflow of motor increases relatively, and each cylinder burning better.
Compared with prior art, the present invention has following beneficial effect: the present invention can make that motor burns better, oil consumption is lower when the low speed operating mode, each cylinder detonation pressure is lower when high-speed working condition; And cavity volume is away from outlet pipe, and the volume cavity temperature is lower, and the sealing problem between moving body and the cavity volume also solves easily.
Description of drawings
Fig. 1 is the structural representation of mechanical conditioning type turbine blow-off system of the present invention;
Fig. 2 is the structural representation of A-A section among Fig. 1;
Fig. 3 is the structural representation of B-B section among Fig. 1;
Wherein: 1, compressor air inlet machine pipe, 2, gas compressor, 3, engine air inlet tube, 4, motor, 5, engine exhaust pipe; 6, turbine, 7, the turbine steam outlet pipe, 8, coupling shaft, 9, first connecting tube, 10, second connecting tube; 11, cavity volume, 12, the cavity volume upper wall surface, 13, the cavity volume lower wall surface, 14, cavity volume left side wall, 15, the right wall of cavity volume; 16, cavity volume front face, 17, the cavity volume rear surface, 18, moving body, 19, elastic member.
Embodiment
Below in conjunction with accompanying drawing embodiments of the invention are elaborated, present embodiment is a prerequisite with technological scheme of the present invention, provided detailed mode of execution and concrete operating process, but protection scope of the present invention is not limited to following embodiment.
Embodiment
Like Fig. 1, Fig. 2 and shown in Figure 3; The present invention includes: compressor air inlet machine pipe 1, gas compressor 2, engine air inlet tube 3, motor 4, engine exhaust pipe 5, turbine 6, turbine steam outlet pipe 7, coupling shaft 8, first connecting tube 9, second connecting tube 10, cavity volume 11, cavity volume upper wall surface 12, cavity volume lower wall surface 13, cavity volume left side wall 14, the right wall 15 of cavity volume, cavity volume front face 16, cavity volume rear surface 17, moving body 18 and elastic member 19; Gas compressor 2 and turbine 6 are through 8 coaxial linking to each other of coupling shaft; The air inlet/outlet of gas compressor 2 is connected with the air outlet of compressor air inlet machine pipe 1, the suction port of engine air inlet tube 3 respectively; The air inlet/outlet of motor 4 is connected with the air outlet of engine air inlet tube 3, the suction port of engine exhaust pipe 5 respectively; The air inlet/outlet of turbine 6 is connected with the air outlet of engine exhaust pipe 5, the suction port of turbine steam outlet pipe 7 respectively; The two ends of first connecting tube 9 are connected with turbine steam outlet pipe 7, cavity volume left side wall 14 respectively; The two ends of second connecting tube 10 are connected with engine exhaust pipe 5, cavity volume left side wall 14 respectively; Cavity volume upper wall surface 12, cavity volume lower wall surface 13, cavity volume left side wall 14, the right wall 15 of cavity volume, cavity volume front face 16, cavity volume rear surface 17 are fixed to be one; Moving body 18 is installed in the cavity volume 11, and moving body 18 contacts with the internal face sealing of cavity volume 11, and moving body 18 is connected with cavity volume lower wall surface 13 through elastic member 19; The cross section of cavity volume 11 is a rectangular, and elastic member 19 is a spring.
In working procedure of the present invention, moving body 18 can move up and down in cavity volume 11.When motor 4 is in high-speed working condition; Engine exhaust pipe 5 internal pressures are higher; Moving body 18 moves up and tensile elasticity parts 19 upwards, and a part of exhausts in the cavity volume 11 flow in the turbine steam outlet pipe 7 through first connecting tube 9, thereby make the acting ability drop of turbine 6; The air inflow of motor 4 reduces relatively, and each cylinder detonation pressure reduces; When motor 4 is in the low speed operating mode; Engine exhaust pipe 5 internal pressures are lower, and under the effect of elastic member 19, moving body 18 moves down; There is not exhaust to flow in the turbine steam outlet pipe 7 in the cavity volume 11 through first connecting tube 9; Thereby the acting ability of turbine 6 is strengthened relatively, and the air inflow of motor 4 increases relatively, and each cylinder burning better.Therefore, the present invention can take into account the high and low rotating speed operating mode of motor preferably.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101362814A CN102678284A (en) | 2012-05-03 | 2012-05-03 | Mechanical regulating type turbine bleeding system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101362814A CN102678284A (en) | 2012-05-03 | 2012-05-03 | Mechanical regulating type turbine bleeding system |
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| Publication Number | Publication Date |
|---|---|
| CN102678284A true CN102678284A (en) | 2012-09-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012101362814A Pending CN102678284A (en) | 2012-05-03 | 2012-05-03 | Mechanical regulating type turbine bleeding system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107725175A (en) * | 2017-10-18 | 2018-02-23 | 山东交通学院 | A kind of resonant pulse energy sustained release turbo charge system of spring oscillator |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0035691A1 (en) * | 1980-03-07 | 1981-09-16 | Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 | Charging pressure control device for internal-combustion engines |
| US6012289A (en) * | 1997-11-19 | 2000-01-11 | Caterpillar Inc. | Apparatus and method for utilizing a learned wastegate control signal for controlling turbocharger operation |
| JP2001193614A (en) * | 1999-12-07 | 2001-07-17 | Visteon Global Technologies Inc | Engine starter with turbocharger and starting method for it |
| CN201786446U (en) * | 2010-08-17 | 2011-04-06 | 芜湖杰锋汽车动力系统有限公司 | Gasoline engine turbocharger provided with pressure relief device |
| CN102191999A (en) * | 2010-03-17 | 2011-09-21 | 福特环球技术公司 | Turbocharger control |
-
2012
- 2012-05-03 CN CN2012101362814A patent/CN102678284A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0035691A1 (en) * | 1980-03-07 | 1981-09-16 | Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 | Charging pressure control device for internal-combustion engines |
| US6012289A (en) * | 1997-11-19 | 2000-01-11 | Caterpillar Inc. | Apparatus and method for utilizing a learned wastegate control signal for controlling turbocharger operation |
| JP2001193614A (en) * | 1999-12-07 | 2001-07-17 | Visteon Global Technologies Inc | Engine starter with turbocharger and starting method for it |
| CN102191999A (en) * | 2010-03-17 | 2011-09-21 | 福特环球技术公司 | Turbocharger control |
| CN201786446U (en) * | 2010-08-17 | 2011-04-06 | 芜湖杰锋汽车动力系统有限公司 | Gasoline engine turbocharger provided with pressure relief device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107725175A (en) * | 2017-10-18 | 2018-02-23 | 山东交通学院 | A kind of resonant pulse energy sustained release turbo charge system of spring oscillator |
| CN107725175B (en) * | 2017-10-18 | 2024-03-26 | 山东交通学院 | Spring vibrator resonance type pulse energy delayed release turbocharging system |
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Application publication date: 20120919 |