CN102562270A - Turbine inlet area adaptive turbo charging system - Google Patents
Turbine inlet area adaptive turbo charging system Download PDFInfo
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- CN102562270A CN102562270A CN2011104485489A CN201110448548A CN102562270A CN 102562270 A CN102562270 A CN 102562270A CN 2011104485489 A CN2011104485489 A CN 2011104485489A CN 201110448548 A CN201110448548 A CN 201110448548A CN 102562270 A CN102562270 A CN 102562270A
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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
The invention discloses a turbine inlet area adaptive turbo charging system, which relates to the technical field of a combustion motor. The system comprises an air cylinder, an exhaust pipe, a connecting pipe, a turbine, two rotating plates, a rotating shaft and an elastic component. Two ends of the rotating shaft are arranged in the side wall of the connecting pipe; the rotating plates and the rotating shaft are fixedly connected into a whole; and front ends of the two rotating plates are connected with each other through the elastic component. When an engine is in a high-speed condition, the first rotating plate rotates clockwise, the second rotating plate rotates anticlockwise, the area of the opening between the two rotating plates becomes larger, the pumping loss is small, and the performance of the engine is good; and when the engine is in a low-speed condition, under the effect of the elastic component, the first rotating plate rotates anticlockwise, and the second rotating plate rotates clockwise, so that the area of the opening between the two rotating plates becomes smaller, available energy in front of the turbine is more, the admission pressure of the engine is higher, and the performance of the engine is good. The system has reasonable design and simple structure and is applicable to the turbo charging system with only one turbine inlet and a laterally arranged turbine.
Description
Technical field
What the present invention relates to is a kind of turbo charge system of field of internal combustion engine, particularly a kind of turbine inlet area self-adapting type turbo charge system.
Background technique
Along with the development of society and the raising of environmental requirement, the engine booster The Application of Technology more and more widely, in powerful motor mostly adopt turbocharging technology, to improve power and to reduce fuel consumption rate.Two kinds of basic patterns of turbo charge system are constant pressure charging system and impulse pressure charging system.Constant pressure charging system; The shared outlet pipe that volume is bigger of each cylinder, exhaust piping is relatively simple for structure, and it is constant that the outlet pipe internal pressure keeps basically; The pressure size is only relevant with the load and the rotating speed of motor, and the pressurization system that different cylinders are counted diesel engine can be designed for uniformity.Constant pressure charging system is when high-speed working condition, and pumping loss is less, and turbine efficiency is higher, and performance is more excellent; But when the low speed operating mode, can not make full use of the exhaust pulses energy.Impulse pressure charging system, according to each cylinder firing order, two cylinders or three cylinders that exhaust is not disturbed are connected with same outlet pipe, and the exhaust piping caliber is less, and the exhaust pulses energy can make full use of, low speed operating mode and instantaneous conditions better performances; But when high-speed working condition, pumping loss is bigger.This shows, if a waste pipe volume can change along with the conversion of operating mode, make exhaust pipe volume become big during high-speed working condition, during the low speed operating mode exhaust pipe volume is diminished, this is comparatively desirable.Under the constant prerequisite of exhaust pipe volume,, also can realize taking into account of motor high and low rotating speed operating mode through changing the area of turbine inlet.When the low speed operating mode, the turbine inlet area is diminished, available energy is more before the turbine; When high-speed working condition, make the turbine inlet area become big, the motor pumping loss is less, and this also is comparatively desirable.
Retrieval through to the existing technology document is found; Chinese patent ZL201020532937.0; Patent name: the turbo charging installation of exhaust outlet variable area; This patented technology provides a kind of device of turbine inlet area continuous variable, can take into account the high and low rotating speed operating mode of motor preferably; But the variation of its turbine inlet area is the rotation through rotating handles to be realized, this just needs to increase the special control mechanism of a cover control the rotation of rotating handles, thus the more complicated that the pressurization system structure is become.
Summary of the invention
The present invention is directed to the deficiency of above-mentioned existing technology; A kind of turbine inlet area self-adapting type turbo charge system is provided, has made its turbine inlet area can self-control, taken into account the high and low rotating speed operating mode of motor preferably; And simple in structure, do not need special control mechanism.
The present invention realizes through following technological scheme; The present invention includes: first cylinder, second cylinder, the 3rd cylinder, first exhaust branch pipe, second exhaust branch pipe, the 3rd exhaust branch pipe, outlet pipe, connecting tube, turbine, connecting tube upper side wall, connecting tube lower wall, connecting tube front panel, connecting tube rear sidewall, first running shaft, second running shaft, first swivel plate, second swivel plate and elastic member; First cylinder, second cylinder, the 3rd cylinder are connected with outlet pipe through first exhaust branch pipe, second exhaust branch pipe, the 3rd exhaust branch pipe respectively; The outlet of outlet pipe is connected with the inlet of connecting tube; The outlet of connecting tube is connected with the inlet of turbine; Connecting tube upper side wall, connecting tube lower wall, connecting tube front panel, connecting tube rear sidewall fix as one; The cross section of connecting tube is a rectangular, and the two ends of first running shaft, second running shaft are installed in connecting tube front panel and the connecting tube rear sidewall respectively, and first swivel plate and first running shaft fix as one; Second swivel plate and second running shaft fix as one, and the front end of first swivel plate is connected through the front end of elastic member with second swivel plate.The elastic member parts are spring.
In working procedure of the present invention, first swivel plate can be in connecting tube is the axis rotation with first running shaft, and second swivel plate can be in connecting tube is the axis rotation with second running shaft.When motor was in high-speed working condition, exhaust pressure was higher in the outlet pipe, and first swivel plate turns clockwise, and second swivel plate is rotated counterclockwise, and the throat area between two swivel plates becomes big, and the motor pumping loss is less, and motor complete machine performance is more excellent; When motor was in the low speed operating mode, exhaust pressure was lower in the outlet pipe, under the effect of elastic member; First swivel plate is rotated counterclockwise; Second swivel plate turns clockwise, and the throat area between two swivel plates diminishes, and available energy is more before the turbine; Engine charge pressure is higher, and motor complete machine performance is more excellent.
Compared with prior art; The present invention has following beneficial effect: the present invention is reasonable in design; Simple in structure; Be applicable to that turbine inlet has the turbo charge system of and turbine side, can take into account the high and low rotating speed operating mode of motor, can make pressurization system not need special turbine inlet area control mechanism again.
Description of drawings
Fig. 1 is the structural representation of turbine inlet area self-adapting type turbo charge 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, first cylinder, 2, second cylinder, the 3, the 3rd cylinder, 4, first exhaust branch pipe, 5, second exhaust branch pipe; 6, the 3rd exhaust branch pipe, 7, outlet pipe, 8, connecting tube, 9, turbine, 10, the connecting tube upper side wall; 11, connecting tube lower wall, 12, the connecting tube front panel, 13, the connecting tube rear sidewall, 14, first running shaft; 15, second running shaft, 16, first swivel plate, 17, second swivel plate, 18, 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: first cylinder 1, second cylinder 2, the 3rd cylinder 3, first exhaust branch pipe 4, second exhaust branch pipe 5, the 3rd exhaust branch pipe 6, outlet pipe 7, connecting tube 8, turbine 9, connecting tube upper side wall 10, connecting tube lower wall 11, connecting tube front panel 12, connecting tube rear sidewall 13, first running shaft 14, second running shaft 15, first swivel plate 16, second swivel plate 17, first elastic member 18 and second elastic member 19; First cylinder 1, second cylinder 2, the 3rd cylinder 3 are connected with outlet pipe 7 through first exhaust branch pipe 4, second exhaust branch pipe 5, the 3rd exhaust branch pipe 6 respectively; The outlet of outlet pipe 7 is connected with the inlet of connecting tube 8; The outlet of connecting tube 8 is connected with the inlet of turbine 9; Connecting tube upper side wall 10, connecting tube lower wall 11, connecting tube front panel 12, connecting tube rear sidewall 13 fix as one; The cross section of connecting tube 8 is a rectangular; The two ends of first running shaft 14, second running shaft 15 are installed in connecting tube front panel 12 and the connecting tube rear sidewall 13 respectively, and first swivel plate 16 and first running shaft 14 fix as one, and second swivel plate 17 and second running shaft 15 fix as one; The front end of first swivel plate 16 is connected through the front end of elastic member 18 with second swivel plate 17, and elastic member 118 is a spring.
In working procedure of the present invention, first swivel plate 16 can be in connecting tube 8 is the axis rotation with first running shaft 14, and second swivel plate 17 can be connecting tube 8 in is that axis rotates with second running shaft 15.When motor was in high-speed working condition, exhaust pressure were higher in the outlet pipe 7, and first swivel plate 16 turns clockwise, and second swivel plate 17 is rotated counterclockwise, and the throat area between two swivel plates becomes big, and the motor pumping loss is less, and motor complete machine performance is more excellent; When motor was in the low speed operating mode, exhaust pressure was lower in the outlet pipe 7, under the effect of elastic member 118; First swivel plate 16 is rotated counterclockwise; Second swivel plate 17 turns clockwise, and the throat area between two swivel plates diminishes, and available energy is more before the turbine; Engine charge pressure is higher, and motor complete machine performance is more excellent.Therefore, the present invention can take into account the high and low rotating speed operating mode of motor preferably.
Claims (2)
1. turbine inlet area self-adapting type turbo charge system; Comprise: first cylinder (1), second cylinder (2), the 3rd cylinder (3), first exhaust branch pipe (4), second exhaust branch pipe (5), the 3rd exhaust branch pipe (6), outlet pipe (7), connecting tube (8), turbine (9), connecting tube upper side wall (10), connecting tube lower wall (11), connecting tube front panel (12), connecting tube rear sidewall (13); First cylinder (1), second cylinder (2), the 3rd cylinder (3) are connected with outlet pipe (7) through first exhaust branch pipe (4), second exhaust branch pipe (5), the 3rd exhaust branch pipe (6) respectively; The outlet of outlet pipe (7) is connected with the inlet of connecting tube (8); The outlet of connecting tube (8) is connected with the inlet of turbine (9); Connecting tube upper side wall (10), connecting tube lower wall (11), connecting tube front panel (12), connecting tube rear sidewall (13) fix as one; It is characterized in that also comprising: first running shaft (14), second running shaft (15), first swivel plate (16), second swivel plate (17) and elastic member (18); The cross section of connecting tube (8) is a rectangular; The two ends of first running shaft (14), second running shaft (15) are installed in connecting tube front panel (12) and the connecting tube rear sidewall (13) respectively; First swivel plate (16) fixes as one with first running shaft (14), and second swivel plate (17) fixes as one with second running shaft (15), and the front end of first swivel plate (16) is connected through the front end of elastic member (18) with second swivel plate (17).
2. turbine inlet area self-adapting type turbo charge system according to claim 1 is characterized in that said elastic member (18) is a spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011104485489A CN102562270A (en) | 2011-12-28 | 2011-12-28 | Turbine inlet area adaptive turbo charging system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011104485489A CN102562270A (en) | 2011-12-28 | 2011-12-28 | Turbine inlet area adaptive turbo charging system |
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| CN102562270A true CN102562270A (en) | 2012-07-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2011104485489A Pending CN102562270A (en) | 2011-12-28 | 2011-12-28 | Turbine inlet area adaptive turbo charging system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107795373A (en) * | 2017-08-31 | 2018-03-13 | 合肥雷光动力科技有限公司 | A kind of turbocharger for possessing air inlet adjustment function |
| CN109505696A (en) * | 2019-01-16 | 2019-03-22 | 王志伟 | A kind of automatic adjustable turbocharger |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2751987A1 (en) * | 1977-11-22 | 1979-05-23 | Motoren Turbinen Union | Engine with exhaust gas turbocharger - has variable cross-section injector to maintain efficiency under varying engine loads |
| SU1240933A2 (en) * | 1983-12-15 | 1986-06-30 | Харьковский Институт Инженеров Железнодорожного Транспорта Им.С.М.Кирова | Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine |
| WO2008125564A1 (en) * | 2007-04-16 | 2008-10-23 | Napier Turbochargers Limited | Exhaust gas turbocharger comprising a gas volume distributing device and method for operating such a turbocharger |
| CN101413429A (en) * | 2008-11-20 | 2009-04-22 | 上海交通大学 | Turbocharging system for adjusting exhausting pipe volume by rotating baffle |
| WO2010126169A1 (en) * | 2009-04-30 | 2010-11-04 | 協和発酵キリン株式会社 | Pharmaceutical composition for preventing vascular disorders which comprises alk1 inhibitor as active ingredient |
-
2011
- 2011-12-28 CN CN2011104485489A patent/CN102562270A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2751987A1 (en) * | 1977-11-22 | 1979-05-23 | Motoren Turbinen Union | Engine with exhaust gas turbocharger - has variable cross-section injector to maintain efficiency under varying engine loads |
| SU1240933A2 (en) * | 1983-12-15 | 1986-06-30 | Харьковский Институт Инженеров Железнодорожного Транспорта Им.С.М.Кирова | Pressure pulse converter for exhaust system of gas turbocharged internal combustion engine |
| WO2008125564A1 (en) * | 2007-04-16 | 2008-10-23 | Napier Turbochargers Limited | Exhaust gas turbocharger comprising a gas volume distributing device and method for operating such a turbocharger |
| CN101413429A (en) * | 2008-11-20 | 2009-04-22 | 上海交通大学 | Turbocharging system for adjusting exhausting pipe volume by rotating baffle |
| WO2010126169A1 (en) * | 2009-04-30 | 2010-11-04 | 協和発酵キリン株式会社 | Pharmaceutical composition for preventing vascular disorders which comprises alk1 inhibitor as active ingredient |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107795373A (en) * | 2017-08-31 | 2018-03-13 | 合肥雷光动力科技有限公司 | A kind of turbocharger for possessing air inlet adjustment function |
| CN109505696A (en) * | 2019-01-16 | 2019-03-22 | 王志伟 | A kind of automatic adjustable turbocharger |
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Application publication date: 20120711 |
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