CN105464791A - Top end air inflation smooth movement system - Google Patents
Top end air inflation smooth movement system Download PDFInfo
- Publication number
- CN105464791A CN105464791A CN201510969550.9A CN201510969550A CN105464791A CN 105464791 A CN105464791 A CN 105464791A CN 201510969550 A CN201510969550 A CN 201510969550A CN 105464791 A CN105464791 A CN 105464791A
- Authority
- CN
- China
- Prior art keywords
- extrusion
- turbine
- solid
- rotation
- control agent
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a top end air inflation smooth movement system and belongs to the technical field of machine design. The top end air inflation smooth movement system comprises an adjusting body, a rotary shaft, a rotary body, a drawing body, centrifugal bodies, balls, a pull rod, springs and an adjusting pipe. The rotary shaft and the rotary body are fixedly combined. The drawing body and the centrifugal bodies are all arranged in the rotary body. The balls are inlaid in the drawing body. One side walls of the centrifugal bodies make contact with the drawing body through the balls, and the other side walls of the centrifugal bodies are connected with the inner wall faces of the rotary body through the first springs. The top of the drawing body is connected with the inner wall face of the rotary body through the second spring. According to the top end air inflation smooth movement system, an adjusting plate moves upwards when the rotation speed of an engine is high, and the gas exhausting quantity of a turbine is large, and thus the loss of pump gas is small; when the rotation speed of the engine is low, the adjusting plate moves downwards, and the gas exhausting quantity of the turbine is small, and exhaust gas pulse energy can be fully used. The top end air inflation smooth movement system is reasonable in design, simple in structure and suitable for optimal design of a turbine gas exhausting system.
Description
Technical field
What the present invention relates to is that level and smooth movement system is inflated on a kind of top of technical field of mechanical design, and particularly level and smooth movement system is inflated on a kind of top being applicable to turbine blow-off system.
Background technique
Turbosupercharging is a kind of technology utilizing internal-combustion engine to operate the exhaust gas driven air compressor produced.Turbo charged Main Function improves air input of engine by air exactly, thus improves power and the moment of torsion of motor, allows car energeticallyer.After turbosupercharger loaded onto by a motor, its peak output can increase by 40% even higher compared with when being unkitted pressurized machine.So also just mean that the motor of same can export larger power after supercharging.With regard to by our modal 1.8T turbosupercharged engine, after supercharging, power can reach the level of 2.4L motor, but fuel consumption is but high unlike 1.8L motor how many, is exactly improve fuel economy and reduce exhaust emissions in another one aspect.But after have passed through supercharging, motor pressure and temperature operationally raises all greatly, therefore engine life can be shorter than the motor of same discharge capacity not through supercharging, and mechanical property, greasy property all can be affected, so also limit turbocharging technology application on the engine to a certain extent.The burning being intended for motor provides enough air, and make power character and the better economy of motor, turbocharging technology plays very important role.But existing turbo charge system all can not take into account the high and low rotating speed operating mode of motor preferably.
In existing technology, in order to take into account the high and low rotating speed operating mode of motor, turbosupercharger often has with exhaust gas by-pass valve, but exhaust gas by-pass valve is all close to turbine, cause valve body temperature higher, and must be regulated by engine charge pressure, self-control can not be carried out according to the rotating speed of motor.
Summary of the invention
The present invention is directed to above-mentioned the deficiencies in the prior art, provide a kind of top and inflate level and smooth movement system, turbine discharge quantity can be made to carry out self-control according to engine speed.
The present invention is achieved through the following technical solutions, the present invention includes suction tude, air filter, gas compressor, motor, outlet pipe, turbine, catalysis bag, bypass tube, control agent, running shaft, solid of rotation, extrusion, centrifugal body, ball, pull bar, regulator plate, first spring, second spring, adjutage, the intake and exhaust port of motor respectively with suction tude, outlet pipe is connected, air filter, gas compressor is connected in turn in suction tude, turbine, catalysis bag is connected in turn on outlet pipe, the two ends of bypass tube are connected with the outlet pipe before and after turbine respectively, and control agent is arranged on bypass tube, and regulator plate to be arranged in control agent and to seal with the internal face of control agent and contacts, running shaft and solid of rotation are consolidated, extrusion, centrifugal body is arranged in a rotating body, ball is embedded in extrusion, one sidewall of centrifugal body is contacted with extrusion by ball, another sidewall of centrifugal body is connected with the internal face of solid of rotation by the first spring, the internal face that the top of extrusion is connected with the internal face of solid of rotation by the second spring is connected, one end of pull bar is connected with the bottom surface of extrusion, other one end of pull bar is connected with the upper-end surface of regulator plate through after the upper wall surface of control agent, running shaft is connected with engine crankshaft by chain, the longitudinal section of extrusion is trapezoidal, one end of adjutage is connected with suction tude after gas compressor, and the other end of adjutage is connected with the control agent internal cavity of regulator plate upper end.
Further, centrifugal body, ball are array-type and arrange in the present invention, and the cross section of solid of rotation internal cavity is round, and the cross section of extrusion is round, and the cross section of centrifugal body, regulator plate is rectangular.
Compared with prior art, the present invention has following beneficial effect and is: the present invention is reasonable in design, and structure is simple; Turbine discharge quantity can carry out continuously adjustabe according to engine speed, thus takes into account the various operating conditionss of motor.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
The partial enlarged drawing of Fig. 2 Fig. 1;
Fig. 3 is the structural representation of A-A section in Fig. 1;
Fig. 4 is the structural representation of B-B section in Fig. 1;
Wherein: 1, suction tude, 2, air filter, 3, gas compressor, 4, motor, 5, outlet pipe, 6, turbine, 7, catalysis bag, 8, bypass tube, 9, control agent, 10, running shaft, 11, solid of rotation, 12, extrusion, 13, centrifugal body, 14, ball, 15, pull bar, 16, regulator plate, 17, the first spring, the 18, second spring, 19, adjutage.
Embodiment
Elaborate to embodiments of the invention below in conjunction with accompanying drawing, the present embodiment, premised on technical solution of the present invention, give detailed mode of execution and concrete operating process, but protection scope of the present invention is not limited to following embodiment.
embodiment
As shown in Figures 1 to 4, the present invention includes suction tude 1, air filter 2, gas compressor 3, motor 4, outlet pipe 5, turbine 6, catalysis bag 7, bypass tube 8, control agent 9, running shaft 10, solid of rotation 11, extrusion 12, centrifugal body 13, ball 14, pull bar 15, regulator plate 16, first spring 17, second spring 18, adjutage 19, the intake and exhaust port of motor 4 respectively with suction tude 1, outlet pipe 5 is connected, air filter 2, gas compressor 3 is connected in turn in suction tude 1, turbine 6, catalysis bag 7 is connected in turn on outlet pipe 5, the two ends of bypass tube 8 are connected with the outlet pipe 5 before and after turbine 6 respectively, control agent 9 is arranged on bypass tube 8, regulator plate 16 to be arranged in control agent 9 and to seal with the internal face of control agent 9 and contacts, running shaft 10 and solid of rotation 11 are consolidated, extrusion 12, centrifugal body 13 is arranged in solid of rotation 11, ball 14 is embedded in extrusion 12, one sidewall of centrifugal body 13 is contacted with extrusion 12 by ball 14, another sidewall of centrifugal body 13 is connected with the internal face of solid of rotation 11 by the first spring 17, the internal face that the top of extrusion 12 is connected with the internal face of solid of rotation 11 by the second spring 18 is connected, one end of pull bar 15 is connected with the bottom surface of extrusion 12, other one end of pull bar 15 is connected with the upper-end surface of regulator plate 16 through after the upper wall surface of control agent 9, running shaft 10 is connected with engine crankshaft by chain, the longitudinal section of extrusion 12 is trapezoidal, one end of adjutage 19 is connected with suction tude 1 after gas compressor 3, and the other end of adjutage 19 is connected with control agent 9 internal cavity of regulator plate 16 upper end, centrifugal body 13, ball 14 are array-type and arrange, the cross section of solid of rotation 11 internal cavity is round, and the cross section of extrusion 12 is round, and the cross section of centrifugal body 13, regulator plate 16 is rectangular.
In implementation process of the present invention, running shaft 10 is connected with engine crankshaft by chain.When motor 4 rotating speed is higher, the rotational speed of solid of rotation 11 is also higher, under the left and right of centrifugal force, centrifugal body 13 outwards moves and compresses the first spring 17, extrusion 12 moves up under the effect of the second spring 18, thus make pull bar 15 drive regulator plate 16 to move up, turbine 6 discharge quantity is comparatively large, and the pumping loss of motor 4 is less.In like manner, when the rotating speed of motor 4 is less, under about the elastic force of the first spring 17, centrifugal body 13 moves inward, thus makes pull bar 15 drive regulator plate 16 to move down, and turbine 6 discharge quantity is less, and turbine 7 can make full use of the pulse energy of exhaust.Under the effect of adjutage 19, the movement of regulator plate 16 is smoother.
Claims (2)
1. level and smooth movement system is inflated on a top, comprise suction tude (1), air filter (2), gas compressor (3), motor (4), outlet pipe (5), turbine (6), catalysis bag (7), the intake and exhaust port of motor (4) respectively with suction tude (1), outlet pipe (5) is connected, air filter (2), gas compressor (3) is connected in turn in suction tude (1), turbine (6), catalysis bag (7) is connected in turn on outlet pipe (5), it is characterized in that, also comprise bypass tube (8), control agent (9), running shaft (10), solid of rotation (11), extrusion (12), centrifugal body (13), ball (14), pull bar (15), regulator plate (16), first spring (17), second spring (18), adjutage (19), the two ends of bypass tube (8) are connected with the outlet pipe (5) before and after turbine (6) respectively, control agent (9) is arranged on bypass tube (8), regulator plate (16) to be arranged in control agent (9) and to seal with the internal face of control agent (9) and contacts, running shaft (10) and solid of rotation (11) are consolidated, extrusion (12), centrifugal body (13) is arranged in solid of rotation (11), ball (14) is embedded in extrusion (12), one sidewall of centrifugal body (13) is contacted with extrusion (12) by ball (14), another sidewall of centrifugal body (13) is connected by the internal face of the first spring (17) with solid of rotation (11), the internal face that the top of extrusion (12) is connected with the internal face of solid of rotation (11) by the second spring (18) is connected, one end of pull bar (15) is connected with the bottom surface of extrusion (12), other one end of pull bar (15) is connected with the upper-end surface of regulator plate (16) through after the upper wall surface of control agent (9), running shaft (10) is connected with engine crankshaft by chain, the longitudinal section of extrusion (12) is trapezoidal, one end of adjutage (19) and gas compressor (3) afterwards suction tude (1) are connected, the other end of adjutage (19) is connected with control agent (9) internal cavity of regulator plate (16) upper end.
2. level and smooth movement system is inflated on top according to claim 1, it is characterized in that centrifugal body (13), ball (14) be array-type arrange, the cross section of solid of rotation (11) internal cavity is round, the cross section of extrusion (12) is round, and the cross section of centrifugal body (13), regulator plate (16) is rectangular.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510969550.9A CN105464791A (en) | 2015-12-21 | 2015-12-21 | Top end air inflation smooth movement system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510969550.9A CN105464791A (en) | 2015-12-21 | 2015-12-21 | Top end air inflation smooth movement system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN105464791A true CN105464791A (en) | 2016-04-06 |
Family
ID=55602884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510969550.9A Pending CN105464791A (en) | 2015-12-21 | 2015-12-21 | Top end air inflation smooth movement system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN105464791A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105971685A (en) * | 2016-07-13 | 2016-09-28 | 孙志国 | Automatic following system of valve stroke |
CN106050398A (en) * | 2016-05-31 | 2016-10-26 | 上海交通大学 | Centrifugal rotating system driven by crankshaft |
CN106168145A (en) * | 2016-07-13 | 2016-11-30 | 孙志国 | Rotary stress balance height adjustment mechanism |
CN106194314A (en) * | 2016-07-13 | 2016-12-07 | 孙志国 | Intake and exhaust are with device cooperative control system |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104405499A (en) * | 2014-12-07 | 2015-03-11 | 魏江山 | Pumping loss controlling system |
CN104747279A (en) * | 2015-04-05 | 2015-07-01 | 上海凌翼动力科技有限公司 | Inlet air pressure controlled exhaust air bypass device |
CN104847436A (en) * | 2015-05-24 | 2015-08-19 | 赵梓涵 | Mechanical multidirectional movement mechanism |
CN104895668A (en) * | 2015-06-28 | 2015-09-09 | 钱蔚鑫 | Through hole flow type waste gas bypass system |
CN104989508A (en) * | 2015-08-15 | 2015-10-21 | 安徽工程大学 | Supercharged engine exhaust pipe volume control system and method |
-
2015
- 2015-12-21 CN CN201510969550.9A patent/CN105464791A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104405499A (en) * | 2014-12-07 | 2015-03-11 | 魏江山 | Pumping loss controlling system |
CN104747279A (en) * | 2015-04-05 | 2015-07-01 | 上海凌翼动力科技有限公司 | Inlet air pressure controlled exhaust air bypass device |
CN104847436A (en) * | 2015-05-24 | 2015-08-19 | 赵梓涵 | Mechanical multidirectional movement mechanism |
CN104895668A (en) * | 2015-06-28 | 2015-09-09 | 钱蔚鑫 | Through hole flow type waste gas bypass system |
CN104989508A (en) * | 2015-08-15 | 2015-10-21 | 安徽工程大学 | Supercharged engine exhaust pipe volume control system and method |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106050398A (en) * | 2016-05-31 | 2016-10-26 | 上海交通大学 | Centrifugal rotating system driven by crankshaft |
CN105971685A (en) * | 2016-07-13 | 2016-09-28 | 孙志国 | Automatic following system of valve stroke |
CN106168145A (en) * | 2016-07-13 | 2016-11-30 | 孙志国 | Rotary stress balance height adjustment mechanism |
CN106194314A (en) * | 2016-07-13 | 2016-12-07 | 孙志国 | Intake and exhaust are with device cooperative control system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105386864A (en) | Centre-fixed and periphery-rotating device | |
CN105386863A (en) | Device capable of rolling and sliding synchronously | |
CN104895668A (en) | Through hole flow type waste gas bypass system | |
CN104912654A (en) | External control system for gas bypass flow | |
CN105370389A (en) | Conical centrifugal tensile mechanism | |
CN105464791A (en) | Top end air inflation smooth movement system | |
CN102588076A (en) | Volume cavity regulating intake device | |
CN105422271A (en) | Slope-type pull rod up and down moving device | |
CN105422291A (en) | Plate type gas recirculation controlling device | |
CN105020060A (en) | Throttling maximum temperature adjusting device | |
CN105604688A (en) | Dynamic and static combined deflation system | |
CN105508028A (en) | Slope-inlaid type rolling device | |
CN105569827A (en) | Two-end-face linear contact system | |
CN105545537A (en) | Low-pressure gas recirculation regulating system | |
CN104747279A (en) | Inlet air pressure controlled exhaust air bypass device | |
CN204386747U (en) | A kind of plug-type engine charge control gear | |
CN105545538A (en) | Rotation driving type lifting control system | |
CN102787949A (en) | Pneumatic intake-exhaust circulation device | |
CN104912655A (en) | Elevating type gas reflux device | |
CN204961071U (en) | Tensile rotary mechanism of mechanical type | |
CN106837526A (en) | The driving rotation regulating system of magnetic field magnetic force | |
CN102767449A (en) | Cross gas intake and exhaust system | |
CN102678269A (en) | Supercharged engine air inlet pipe deflating system | |
CN102606278A (en) | Air inlet device with elastic component | |
CN105508036A (en) | Array type centrifugal body distribution system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160406 |
|
WD01 | Invention patent application deemed withdrawn after publication |