CN102678277A - Air inlet bypass device in compressor rear air inlet pipe - Google Patents
Air inlet bypass device in compressor rear air inlet pipe Download PDFInfo
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- CN102678277A CN102678277A CN2012101362848A CN201210136284A CN102678277A CN 102678277 A CN102678277 A CN 102678277A CN 2012101362848 A CN2012101362848 A CN 2012101362848A CN 201210136284 A CN201210136284 A CN 201210136284A CN 102678277 A CN102678277 A CN 102678277A
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- air inlet
- cavity volume
- engine
- moving body
- pipe
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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
Abstract
The invention discloses an air inlet bypass device in a compressor rear air inlet pipe in the technical field of internal combustion engines. The system comprises a compressor, a turbine, an engine, connecting pipes, a volume cavity, a moving body and an elastic part, wherein two ends of a first connecting pipe are respectively communicated with an engine air inlet pipe and a volume cavity left wall surface; two ends of a second connecting pipe are respectively communicated with an engine exhaust pipe and the volume cavity left wall surface; the moving body is arranged in the volume cavity and connected with a volume cavity upper wall surface through the elastic part. In the operating process, the moving body can move up and down in the volume cavity; the moving body moves upwards under low-speed working conditions of the engine, air compressed by the compressor totally enters the engine, the air inlet quantity of the engine is relatively increased, and a relatively good combustion effect is achieved in each cylinder; and the moving body moves downwards under high-speed working conditions of the engine, part of air compressed by the compressor enters a turbine air outlet pipe, the air inlet quantity of the engine is relatively reduced, and the detonation pressure of each cylinder is reduced. The supercharged engine air inlet pipe deflating system is reasonable in design, simple in structure and suitable for a turbocharging system of the engine.
Description
Technical field
What the present invention relates to is air inlet by-pass collar in the suction tude behind the gas compressor 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, air inlet by-pass collar in the suction tude is provided behind a kind of gas compressor, 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 engine air inlet tube, 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 upper 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 air inlet tube internal pressure is higher; Moving body moves down and downward tensile elasticity parts, and first connecting tube and second connecting tube are connected through cavity volume, thereby a part of pressurized air behind the gas compressor is got in the turbine steam outlet pipe through second connecting tube; The air inflow of motor reduces relatively, and each cylinder detonation pressure reduces; When motor is in the low speed operating mode; The engine air inlet tube internal pressure is lower, and under the effect of elastic member, moving body moves up; And first connecting tube and second connecting tube can not be connected; Thereby make the pressurized air behind the gas compressor all get into motor, 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 air inlet by-pass collar in the suction tude behind the gas compressor 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 engine air inlet tube 3, 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 upper wall surface 12 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 air inlet tube 3 internal pressures are higher; Moving body 18 moves down and downward tensile elasticity parts 19, and first connecting tube 9 and second connecting tube 10 are connected through cavity volume 11, thereby a part of pressurized air behind the gas compressor 2 is got in the turbine steam outlet pipes 7 through second connecting tube 10; 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 air inlet tube 3 internal pressures are lower, and under the effect of elastic member 19, moving body 18 moves up; And first connecting tube 9 and second connecting tube 10 can not be connected; Thereby make the pressurized air behind the gas compressor 2 all get into motor 4, 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)
1. air inlet by-pass collar in the suction tude behind the gas compressor; Comprise 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) and coupling shaft (8); Gas compressor (2) and turbine (6) are through coaxial linking to each other of coupling shaft (8); 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; It is characterized in that also comprising 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); The two ends of first connecting tube (9) are connected with engine air inlet tube (3), 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), cavity volume right wall (15), cavity volume front face (16), cavity volume rear surface (17) is fixed is one; Moving body (18) is installed in the cavity volume (11); Moving body (18) contacts with the internal face sealing of cavity volume (11), and moving body (18) is connected with cavity volume upper wall surface (12) through elastic member (19).
2. air inlet by-pass collar in the suction tude behind the gas compressor according to claim 1, the cross section that it is characterized in that said cavity volume (11) is a rectangular, said elastic member (19) is a spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101362848A CN102678277A (en) | 2012-05-03 | 2012-05-03 | Air inlet bypass device in compressor rear air inlet pipe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101362848A CN102678277A (en) | 2012-05-03 | 2012-05-03 | Air inlet bypass device in compressor rear air inlet pipe |
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| Publication Number | Publication Date |
|---|---|
| CN102678277A true CN102678277A (en) | 2012-09-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012101362848A Pending CN102678277A (en) | 2012-05-03 | 2012-05-03 | Air inlet bypass device in compressor rear air inlet pipe |
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| CN (1) | CN102678277A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104595072A (en) * | 2014-11-30 | 2015-05-06 | 苏皓 | Charging efficiency improving system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2035829A1 (en) * | 1969-03-24 | 1970-12-24 | Sulzer Ag | |
| US4009574A (en) * | 1974-08-01 | 1977-03-01 | The French State | Compression-ignition internal combustion engines |
| US4528815A (en) * | 1981-11-05 | 1985-07-16 | Regie Nationale Des Usines Renault | Turbocharged internal combustion engine having means for controlling supercharging pressure |
| CN102400777A (en) * | 2011-11-03 | 2012-04-04 | 上海交通大学 | Single-vortex double-air compressor turbine pressurizing system with air escape valves |
-
2012
- 2012-05-03 CN CN2012101362848A patent/CN102678277A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2035829A1 (en) * | 1969-03-24 | 1970-12-24 | Sulzer Ag | |
| US4009574A (en) * | 1974-08-01 | 1977-03-01 | The French State | Compression-ignition internal combustion engines |
| US4528815A (en) * | 1981-11-05 | 1985-07-16 | Regie Nationale Des Usines Renault | Turbocharged internal combustion engine having means for controlling supercharging pressure |
| CN102400777A (en) * | 2011-11-03 | 2012-04-04 | 上海交通大学 | Single-vortex double-air compressor turbine pressurizing system with air escape valves |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104595072A (en) * | 2014-11-30 | 2015-05-06 | 苏皓 | Charging efficiency improving system |
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Application publication date: 20120919 |