CN105545462B - A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure - Google Patents
A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure Download PDFInfo
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- CN105545462B CN105545462B CN201610079086.0A CN201610079086A CN105545462B CN 105545462 B CN105545462 B CN 105545462B CN 201610079086 A CN201610079086 A CN 201610079086A CN 105545462 B CN105545462 B CN 105545462B
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- bellows
- push rod
- hole
- rocking arm
- diaphragm
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- 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
- F02B37/183—Arrangements of bypass valves or actuators therefor
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- 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
- F02B37/183—Arrangements of bypass valves or actuators therefor
- F02B37/186—Arrangements of actuators or linkage for bypass valves
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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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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure belongs to technology of gasoline engine field, the turbine of the present invention, the housing of compressor two is docked, the outlet of intake shutter two is placed in before and after air throttle on air inlet pipeline, by-passing valve is put in turbine casing body, two bellows are placed in rocking arm both sides, two bellows are flexibly connected through two push rods with rocking arm, two bellows one end respectively with outlet before and after intake shutter, the two bellows other ends and atmosphere, air throttle is fixed in air inlet pipeline, the diaphragm of two push rod round ends and two bellows is affixed, the via clearance of the bar of two push rods and two bellows coordinates, the elongated hole of two push rods and two pin slides of rocking arm are connected, back-moving spring two ends are respectively and fixedly connected with turbine cylinder and rocking arm；Exhaust gas bypass of the achievable exhaust gas turbocharge gasoline engine of the present invention when Smaller load is not required to supercharging and big load crosses supercharging, improves the fuel economy of gasoline engine, the present invention is simple in construction, it is convenient to realize, can be obviously improved engine performance.
Description
Technical field
The invention belongs to technology of gasoline engine field, and in particular to a kind of pair of bellows-type gasoline exhaust turbine bypass valve control knot
Structure.
Background technology
To obtain bigger torque output, the mode of exhaust-driven turbo-charger exhaust-gas turbo charger of gasoline engine often taking improve admission pressure with
Increase air inflow.But because the operating condition of gasoline engine is transition, engine speed can directly change to highest from idling
Rotating speed, can also be from Smaller load mutation to big load, therefore fixed volute and the exhaust-driven turbo-charger exhaust-gas turbo charger of turbine size can not
All keep efficient in all condition ranges that gasoline engine is run, exhaust-driven turbo-charger exhaust-gas turbo charger matches the big load of high rotating speed and can caused
Moment of torsion is not enough during the slow-speed of revolution, and supercharging and larger exhaust can be produced in the big load of high rotating speed by matching slow-speed of revolution Smaller load
Resistance.For reply above mentioned problem, more universal solution is that exhaust-driven turbo-charger exhaust-gas turbo charger is matched into the slow-speed of revolution now, it is ensured that
The low speed torque output of gasoline engine, and the form deflated during load big to high rotating speed using by-passing valve is by excessive exhaust gas bypass
Fall, reduce the boost pressure of compressor.Exhaust-driven turbo-charger exhaust-gas turbo charger using it is more be capsule type exhaust gas by-pass valve deflation structure,
Bellows upper chamber directly communicates with blower outlet, when boost pressure exceedes the pressure limit of setting, in bellows upper chamber
Pressure can extrude diaphragm and overcome outside atmospheric pressure and spring force to promote push rod that exhaust gas by-pass valve is opened into realization deflation.
Exhaust-driven turbo-charger exhaust-gas turbo charger also increases the exhaust resistance of engine while admission pressure is lifted, also just because of its
The power output of engine is increased, this partial loss also tends to be ignored.The load control manner adjusted for gasoline engine amount
For, the non-standard-sized sheet of sub-load air throttle, pressure is often below local atmospheric pressure after air throttle, that is to say, that engine is not required to
Want plenum also to meet the air inflow demand of partial load condition, now continue to keep exhaust-driven turbo-charger exhaust-gas turbo charger pressurized state
The exhaust resistance of engine can be increased on the contrary, the economy of part load engine is reduced.In consideration of it, the present invention proposes one kind
Double capsule type gasoline exhaust turbine bypass valve control methods and structure, while Pressurized deflating was ensured, moreover it is possible to realize
Admission pressure, which is less than, equally opens exhaust gas by-pass valve when local atmospheric pressure does not need super charge, increase waste gas circulation interface, drop
Low exhaust resistance loss, improves the fuel economy of gasoline engine sub-load.
The content of the invention
It is an object of the invention to solve defect present in above-mentioned prior art there is provided it is a kind of cross supercharging big load and
Sub-load without supercharging opens turbocharger exhaust gas by-pass valve, reduces the skill of supercharging gasoline engine sub-load exhaust resistance
Art means.
To solve the above problems, the present invention adopts the following technical scheme that realization：
The present invention is by the A of bellows I, the B of bellows II, turbine cylinder 1, by-passing valve 2, bearing pin I 3, Rocker arm 4, pin shaft II 5, reset
10, air throttle 11, air inlet pipe are exported before spring 6, push rod I 7, push rod II 8, intake shutter after outlet 9, intake shutter
Road 12 and compressor housings 13 are constituted, and wherein turbine cylinder 1 is docked with compressor housings 13.
Outlet 9 is placed on the air inlet pipeline 12 before air throttle 11 before intake shutter, and 10 are exported after intake shutter
It is placed on the air inlet pipeline 12 after air throttle 11.
The A of bellows I and the B of bellows II are placed in the both sides of Rocker arm 4；The A of bellows I is connected by push rod I 7 with Rocker arm 4, the B of bellows II
It is connected by push rod II 8 with Rocker arm 4.
Push rod I 7 is arranged vertically with push rod II 8 and Rocker arm 4.
The A left ends of bellows I are connected with outlet 9 before intake shutter；The A right-hand members of bellows I pass through through hole I 22 and atmosphere.
The B right-hand members of bellows II are connected with outlet 10 after intake shutter；The B left ends of bellows II are by through hole through hole II 23 and greatly
Gas phase is led to.
Air throttle 11 is fixed in air inlet pipeline 12；Air inlet pipeline 12 and compressor housings 13 are affixed.
By-passing valve 2 is placed in turbine cylinder 1, and bearing pin I 3 is fixed in the left end of by-passing valve 2, the alignment supercharging of the right-hand member of by-passing valve 2
Device gas vent a；
Pin shaft II 5 is fixed in the Inner of turbine cylinder 1.
The hole I 14 of Rocker arm 4 is flexibly connected with bearing pin I 3, and the hole II 15 of Rocker arm 4 is flexibly connected with pin shaft II 5.
The diaphragm I 19 of the round end I 28 of push rod I 7 and the A of bellows I is affixed, between the bar I 29 of push rod I 7 and the A of bellows I through hole I 22
Gap coordinates,
The elongated hole I 30 of push rod I 7 is slidably connected with the bearing pin IV 17 of Rocker arm 4.
The diaphragm II 25 of the round end II 33 of push rod II 8 and the B of bellows II is affixed, and the bar II 32 and B's of bellows II of push rod II 8 is logical
The gap of hole II 23 coordinates,
The elongated hole II 31 of push rod II 8 is slidably connected with the pin shaft III 16 of Rocker arm 4.
The one end of back-moving spring 6 is fixed in turbine cylinder 1, and the other end of back-moving spring 6 is fixed in hole II 15 and the pin of Rocker arm 4
Between axle III 16.
The described A of bellows I is made up of left shell I 18, diaphragm I 19, right shell body I 20 and spring I 21, wherein left shell I 18
With the affixed formation can-like structure of right shell body I 20, the outer rim of diaphragm I 19 is fixed in the inner face of left shell I 18, and formed confined air
Chamber, spring I 21 is placed between diaphragm I 19 and the inner face of right shell body I 20, and through hole I 22 is located at the right-hand member of right shell body I 20.
The described B of bellows II is made up of left shell II 24, diaphragm II 25, spring II 26 and right shell body II 27, wherein left housing
Body II 24 and the affixed formation can-like structure of right shell body II 27, the outer rim of diaphragm II 25 are fixed in the inner face of left shell I 18, and formed
Closed cavity, spring II 26 is placed between diaphragm II 25 and the inner face of right shell body II 27, and through hole II 23 is located at the left end of left shell II 24.
Described Rocker arm 4 top is provided with hole I 14 and hole II 15, and Rocker arm 4 bottom is connected with pin shaft III 16 and bearing pin IV 17.
The push rod I 7 includes the elongated hole I 30 of I 28 bar of round end I 29, and wherein round end I 28 is located at the left end of bar I 29, and elongated hole I 30 is set
In the right-hand member of bar I 29, when by-passing valve 2 is closed, Rocker arm 4 bearing pin IV 17 is located at the A of nearly bellows I of the elongated hole I 30 of push rod I 7.
Described push rod II 8 includes elongated hole II 31, bar II 32 and round end II 33, and wherein elongated hole II 31 is left located at bar II 32
End, round end II 33 is located at the right-hand member of bar II 32, when by-passing valve 2 is closed, and Rocker arm 4 pin shaft III 16 is located at the nearly film of the elongated hole I 30 of push rod II 8
At the B of box II.
The course of work of the present invention is as follows：
(1) when engine, which is in admission pressure after air throttle 11, is less than the Smaller load of local atmospheric pressure：Due to air inlet pipe
Outlet 10 is connected with the B of bellows II after air throttle, therefore is in negative pressure state in the cavity between diaphragm II 25 and right shell body II 27,
The compression spring II 26 of diaphragm II 25 is moved to the direction of right shell body II 27 under the pressure of external pressure, and diaphragm II 25 can drive
Push rod II 8 is simultaneously mobile, and push rod II 8 pulls rocking arm 3 to open by-passing valve 2, while back-moving spring (4) is elongated, realizes gasoline engine
The exhaust gas bypass of Smaller load, reduces exhaust back pressure.Meanwhile, the right side of push rod I 7 is elongated hole I (30), and push rod I 7 will not be with push rod II 8
It is mobile.
(2) admission pressure is more than local atmospheric pressure after engine is in air throttle 11, but pressure is not up to before air throttle
During the moderate duty of boost pressure limit value：Back-moving spring 4, which tenses rocking arm 3, closes by-passing valve 2, the A interior diaphragms I 19 of bellows I and film
The B interior diaphragms II 25 of box II are in initial stretched condition, and push rod I 7 and push rod II 8 are not moved, and give full play to exhaust gas turbocharge
The pressurization of device.
(3) when pressure is higher than boost pressure limit value to engine before big load, air throttle 11：Due to air inlet pipe solar term
Outlet 9 is connected with the A of bellows I in front of the door, and the confined air cavity pressure between diaphragm I 19 and left shell I 18 is limited also above boost pressure
Value, diaphragm I 19 overcomes compression spring I 21 after the pretightning force of spring I 21 to be moved to the A left shells I 18 of bellows I, while driving push rod I 7
Equidirectional movement, push rod II 8 is not moved, and push rod I 7 promotes rocking arm 3 to open exhaust gas by-pass valve 2, while back-moving spring 4 is elongated,
The exhaust gas bypass of the big load of gasoline engine is realized, supercharging was prevented.
Compared with prior art the beneficial effects of the invention are as follows：
1. the bellows that bellows and a negative pressure that the present invention is moved by a malleation are moved, it is possible to achieve exhaust gas turbine increases
Exhaust gas bypass of the pressure gasoline engine when Smaller load is not required to supercharging and big load crosses supercharging, reduces the exhaust resistance of gasoline engine, improves
The fuel economy of gasoline engine.
2. the used herein structure of two bellows push rods and a rocking arm, the elongated hole in push rod Yu rocking arm hinged place
Under design, the action of independent push rod does not interfere with another push rod.
3. the present invention is simple in construction, it is convenient to realize, less input, which can obtain obvious engine performance, to be improved.
Brief description of the drawings
Fig. 1 is double schematic diagrames of the bellows-type gasoline exhaust turbine by-pass valve control structure when exhaust gas by-pass valve is closed
Fig. 2 is the structural representation of rocking arm
Fig. 3 is the structural representation of bellows I
Fig. 4 is the structural representation of bellows II
Fig. 5 is the structural representation of push rod I
Fig. 6 is the structural representation of push rod II
Fig. 7 is that double bellows-type gasoline exhaust turbine by-pass valve control structures exhaust gas by-pass valve under the pulling of push rod I is opened
Schematic diagram
Fig. 8 is that double bellows-type gasoline exhaust turbine by-pass valve control structures exhaust gas by-pass valve under the promotion of push rod II is opened
Schematic diagram
Wherein：A. Rocker arm 5 pin shaft IIs of I B. bellows of bellows, II 1. turbine cylinder, 2. by-passing valve, 3. bearing pin I 4.
6. outlet 11. after 10. intake shutters is exported before the intake shutter of 7. push rod of back-moving spring, I 8. push rod II 9. to save
The left shell I of I 15. hole of valve 12. air inlet pipeline, 13. compressor housings, 14. hole, II 16. pin shaft III, 17. bearing pin IV 18.
19. the spring of II 25. diaphragm of diaphragm I 20. right shell body, I 21. spring, I 22. through hole, I 23. through hole, II 24. left shell II 26.
The a. gas vents of II 27. II 33. round end of right II body of shell 28. round end, I 29. bar, I 30. elongated hole, I 31. elongated hole, II 32. bar II
Embodiment
Below against accompanying drawing, by describe the shape to each mechanism involved by the embodiment of the present invention, construction,
Mutual alignment and annexation, the effect of each several part and operation principle between each several part etc. are described in further detail：
A kind of double capsule type gasoline exhaust turbine by-pass valve control structures it is main by：The A of bellows I, the B of bellows II,
Turbine cylinder 1, by-passing valve 2, bearing pin I 3, Rocker arm 4, pin shaft II 5, back-moving spring 6, push rod I 7, push rod II 8, air inlet pipe solar term
In front of the door outlet 9, outlet 10 after intake shutter, air throttle 11, air inlet pipeline 12, compressor housings 13, hole I 14, hole II 15,
Pin shaft III 16, bearing pin IV 17, left shell I 18, diaphragm I 19, right shell body I 20, spring I 21, through hole I 22, through hole II 23, left shell
II 24, diaphragm II 25, spring II 26, right shell body II 27, round end I 28, bar I 29, elongated hole I 30, elongated hole II 31, bar II 32, round end
II 33 compositions.
As depicted in figs. 1 and 2, described turbine volute 1 is cast iron materials, mainly plays waste gas drainage, turbine
The exhaust gas entrance end of volute 1 has bypass passageways to connect with the port of export；By-passing valve 2 be placed in turbine volute 1 exhaust gas entrance end and
The port of export has in bypass passageways, and bearing pin I 3 is fixed in the left end of by-passing valve 2, and the right-hand member of by-passing valve 2 alignment gas vent a, control bypass is logical
The break-make in road.
Described Rocker arm 4 top is provided with hole I 14 and hole II 15, and Rocker arm 4 bottom is connected with pin shaft III 16 and bearing pin IV 17；Shake
The hole I 14 of arm 4 is flexibly connected with bearing pin I 3, and the hole II 15 of Rocker arm 4 is flexibly connected with pin shaft II 5, and is supported on turbine volute 1
It is interior.
The push rod I 7 is arranged vertically with push rod II 8 and Rocker arm 4, is placed in Rocker arm 4 both sides.
Described one end of back-moving spring 6 is fixed in turbine cylinder 1, and the other end of back-moving spring 6 is fixed in the hole II 15 of Rocker arm 4
Between pin shaft III 16, it is ensured that when Rocker arm 4 is not promoted, by-passing valve 2, which is in, makes the exhaust gas entrance end and outlet of turbine volute 1
The position of the complete disconnection of bypass passageways between end.
Described compressor housings 13 are relative with turbine volute 1 to be connect, for compressing air inlet；Compressor housings 13 export with
Air inlet pipeline 12 is affixed.
The air throttle 11 is fixed in air inlet pipeline 12；Outlet 9 is placed in entering before air throttle 11 before intake shutter
10 are exported on air pipe 12, after intake shutter to be placed on the air inlet pipeline 12 after air throttle 11.
The A of bellows I and the B of bellows II are placed in the both sides of Rocker arm 4；The A of bellows I is connected by push rod I 7 with Rocker arm 4, bellows
II B is connected by push rod II 8 with Rocker arm 4.
The A left ends of bellows I 9 are connected with outlet before intake shutter, and by pressure transmission before air throttle 11 to bellows I
Left side in A.
The B right-hand members of bellows II 10 are connected with outlet after intake shutter, and by pressure transmission after air throttle 11 to film
Right side in the B of box II.
As shown in figure 3, the described A of bellows I is made up of left shell I 18, diaphragm I 19, right shell body I 20 and spring I 21, wherein
Left shell I 18 and the affixed formation can-like structure of right shell body I 20, the outer rim of diaphragm I 19 are fixed in the inner face of left shell I 18, and with its shape
Into closed cavity, spring I 21 is placed between diaphragm I 19 and the inner face of right shell body I 20, and through hole I 22 is located at the right-hand member of right shell body I 20；Institute
State diaphragm I 19 and connected with the cavity that left shell I 18 is formed with outlet 9 before intake shutter；Diaphragm I 19 and the shape of right shell body I 20
Into cavity pass through through hole I 22 and atmosphere；Diaphragm I 19 can be deformed upon in the presence of the pressure difference of both sides.
As shown in figure 4, the described B of bellows II is by II 27 groups of left shell II 24, diaphragm II 25, spring II 26 and right shell body
Into wherein left shell II 24 and the affixed formation can-like structure of right shell body II 27, the outer rim of diaphragm II 25 are fixed in left shell I 18
Face, and formed closed cavity, spring II 26 are placed between diaphragm II 25 and the inner face of right shell body II 27, and through hole II 23 is located at a left side
The left end of housing II 24.Cavity between the diaphragm II 25 and left shell II 24 is connected by through hole II 23 with air；Diaphragm II
Cavity between 25 and right shell body II 27 is connected with outlet 10 after intake shutter；Diaphragm II 25 is in the presence of the pressure difference of both sides
It can deform upon.
As shown in figure 5, the push rod I 7 includes the elongated hole I 30 of I 28 bar of round end I 29, wherein round end I 28 is located at the left end of bar I 29,
Elongated hole I 30 is located at the right-hand member of bar I 29.The diaphragm I 19 of the round end I 28 of push rod I 7 and the A of bellows I is affixed, the bar I 29 and bellows of push rod I 7
The I A gap of through hole I 22 coordinates, it is allowed to which push rod I 7 can have certain oscillating quantity；The elongated hole I 30 of push rod I 7 and the bearing pin of Rocker arm 4
IV 17 are slidably connected, it is allowed to which the bearing pin IV 17 of rocking arm 3 is slided in elongated hole I 30；When the diaphragm I 19 in the A of bellows I is in both sides pressure difference
In the presence of when can deform upon, push rod I 7 is moved, and then pulls Rocker arm 4 to be rotated around pin shaft II 5, and by-passing valve 2 is opened；It is other
When port valve 2 is closed, Rocker arm 4 bearing pin IV 17 is located at the A of nearly bellows I of the elongated hole I 30 of push rod I 7.
As shown in fig. 6, described push rod II 8 includes elongated hole II 31, bar II 32 and round end II 33, wherein elongated hole II 31 is located at
The left end of bar II 32, round end II 33 is located at the right-hand member of bar II 32.The diaphragm II 25 of the round end II 33 of push rod II 8 and the B of bellows II is affixed, pushes away
The bar II 32 of bar II 8 coordinates with the B of bellows II gap of through hole II 23, it is allowed to which push rod II 8 can have certain oscillating quantity；Push rod II
8 elongated hole II 31 is slidably connected with the pin shaft III 16 of Rocker arm 4, it is allowed to which the pin shaft III 16 of rocking arm 3 is slided in elongated hole II 31；Work as film
Diaphragm II 25 in the B of box II in the presence of the pressure difference of both sides when that can be deformed upon, and push rod II 8 is moved, and then promote Rocker arm 4
Rotated around pin shaft II 5, by-passing valve 2 is opened；When by-passing valve 2 is closed, Rocker arm 4 pin shaft III 16 is located at the near of the elongated hole II 31 of push rod II 8
At the B of bellows II.
As shown in fig. 7, being less than local atmospheric pressure for pressure after air throttle 11, the B interior diaphragms II 25 of bellows II are in suction function
Under overcome and pull push rod II 8 to be moved to the B directions of bellows II after the pressure of spring II 26, the band motion rocker arm 3 of push rod II 8 is rotated by-passing valve
2 open, and the long pore structure of the right-hand member of push rod I 7 makes push rod I 7 during the rotation of rocking arm 3 not move.Now, engine discharge waste gas
It can jointly be discharged through exhaust gas turbine and bypass line, increase waste gas circulation area, and then reduce the exhaust resistance of engine
Loss, part load engine economy is improved.
As shown in figure 8, being acted on for pressure before air throttle 11 higher than limit value, the A interior diaphragms I 19 of bellows I is pressurized in boost pressure
Under overcome and promote push rod I 7 to be moved to the B of bellows II opposite direction after the pressure of spring I 21, band motion rocker arm 3 rotation of push rod I 7 will bypass
Valve 2 is opened, and push rod II 8 is due to being long pore structure, and it promotes the rotary course of rocking arm 3 also not move in push rod I 7.Now, it is more
Engine exhaust can flow out from bypass line, reduce the exhaust gas flow for flowing through exhaust gas turbine, so as to reduce the increasing of big load
Pressure degree, plays dual parts of reducing supercharging level and reduces exhaust resistance.
Claims (6)
1. a kind of double capsule type gasoline exhaust turbine by-pass valve arrangements, it is characterised in that by bellows I (A), bellows II (B),
Turbine cylinder (1), by-passing valve (2), bearing pin I (3), rocking arm (4), pin shaft II (5), back-moving spring (6), push rod I (7), push rod
Exported before II (8), intake shutter (9), outlet (10) after intake shutter, air throttle (11), air inlet pipeline (12) and
Compressor housings (13) are constituted, and wherein turbine cylinder (1) is docked with compressor housings (13)；Exported before intake shutter
(9) it is placed on the air inlet pipeline (12) before air throttle (11), (10) is exported after intake shutter and are placed in after air throttle (11)
On air inlet pipeline (12)；Bellows I (A) and bellows II (B) are placed in the both sides of rocking arm (4)；Bellows I (A) by push rod I (7) with
Rocking arm (4) is connected, and bellows II (B) is connected by push rod II (8) with rocking arm (4)；Push rod I (7) and push rod II (8) and rocking arm (4)
It is arranged vertically；(A) left end of bellows I is connected with exporting (9) before intake shutter；(A) right-hand member of bellows I by through hole I (22) with
Atmosphere；(B) right-hand member of bellows II is connected with exporting (10) after intake shutter；(B) left end of bellows II passes through through hole through hole
II (23) are communicated with air；Air throttle (11) is fixed in air inlet pipeline (12)；Air inlet pipeline (12) and compressor housings (13)
It is affixed；By-passing valve (2) is placed in turbine cylinder (1), and bearing pin I (3) is fixed in by-passing valve (2) left end, by-passing valve (2) right-hand member pair
Quasi- booster gas vent (a)；Pin shaft II (5) is fixed in turbine cylinder (1) bottom；The hole I (14) of rocking arm (4) and bearing pin I (3)
It is flexibly connected, the hole II (15) of rocking arm (4) is flexibly connected with pin shaft II (5)；The round end I (28) of push rod I (7) and bellows I (A)
Diaphragm I (19) is affixed, and the bar I (29) of push rod I (7) coordinates with through hole I (22) gap of bellows I (A), the elongated hole I of push rod I (7)
(30) bearing pin IV (17) with rocking arm (4) is slidably connected；The round end II (33) of push rod II (8) and the diaphragm II of bellows II (B)
(25) affixed, the bar II (32) of push rod II (8) coordinates with through hole II (23) gap of bellows II (B), the elongated hole II of push rod II (8)
(31) pin shaft III (16) with rocking arm (4) is slidably connected；Back-moving spring (6) one end is fixed in turbine cylinder (1), back-moving spring
(6) other end is fixed between the hole II (15) of rocking arm (4) and pin shaft III (16).
2. double capsule type gasoline exhaust turbine by-pass valve arrangements as described in claim 1, it is characterised in that described film
Box I (A) is made up of left shell I (18), diaphragm I (19), right shell body I (20) and spring I (21), wherein left shell I (18) and the right side
The affixed formation can-like structure of housing I (20), diaphragm I (19) outer rim is fixed in left shell I (18) inner face, and formed confined air
Chamber, spring I (21) is placed between diaphragm I (19) and right shell body I (20) inner face, and through hole I (22) is located at right shell body I (20) right-hand member.
3. double capsule type gasoline exhaust turbine by-pass valve arrangements as described in claim 1, it is characterised in that described film
Box II (B) is made up of left shell II (24), diaphragm II (25), spring II (26) and right shell body II (27), wherein left shell II
(24) with the affixed formation can-like structure of right shell body II (27), diaphragm II (25) outer rim is fixed in left shell I (18) inner face, and and its
Closed cavity is formed, spring II (26) is placed between diaphragm II (25) and right shell body II (27) inner face, through hole II (23) is located at a left side
Housing II (24) left end.
4. double capsule type gasoline exhaust turbine by-pass valve arrangements as described in claim 1, it is characterised in that described shakes
Arm (4) top is provided with hole I (14) and hole II (15), and rocking arm (4) bottom is connected with pin shaft III (16) and bearing pin IV (17).
5. double capsule type gasoline exhaust turbine by-pass valve arrangements as described in claim 1, it is characterised in that the push rod I
(7) (29) elongated hole I (30) of round end I (28) bar I is included, wherein round end I (28) is located at bar I (29) left end, and elongated hole I (30) is located at bar
I (29) right-hand member.
6. double capsule type gasoline exhaust turbine by-pass valve arrangements as described in claim 1, it is characterised in that described pushes away
Bar II (8) includes elongated hole II (31), bar II (32) and round end II (33), and wherein elongated hole II (31) is located at bar II (32) left end, circle
First II (33) are located at bar II (32) right-hand member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610079086.0A CN105545462B (en) | 2016-02-04 | 2016-02-04 | A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610079086.0A CN105545462B (en) | 2016-02-04 | 2016-02-04 | A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105545462A CN105545462A (en) | 2016-05-04 |
| CN105545462B true CN105545462B (en) | 2017-10-10 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201610079086.0A Active CN105545462B (en) | 2016-02-04 | 2016-02-04 | A kind of pair of bellows-type gasoline exhaust turbine by-pass valve control structure |
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| CN107605589A (en) * | 2017-11-02 | 2018-01-19 | 福州大学 | A kind of double vacuum tank gasoline exhaust turbocharger and control method based on by-passing valve control |
| CN113123858B (en) * | 2019-12-31 | 2022-09-09 | 比亚迪股份有限公司 | Bypass valve assembly, turbocharger and vehicle |
| CN112682166A (en) * | 2020-12-18 | 2021-04-20 | 合肥工业大学 | Multistage control device of turbocharger |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US3941035A (en) * | 1969-11-06 | 1976-03-02 | Trw Inc. | Control unit and method |
| JPS5569725A (en) * | 1978-11-18 | 1980-05-26 | Nissan Motor Co Ltd | Exhaust gas by-passing valve mechanism for use with exhaust turbo-supercharger |
| FR2508974B1 (en) * | 1981-07-03 | 1986-04-04 | Renault | METHOD AND DEVICE FOR CONTROLLING THE EXHAUST DISCHARGE VALVE OF A TURBOCHARGED INTERNAL COMBUSTION ENGINE |
| JPS59180031A (en) * | 1983-03-29 | 1984-10-12 | Aisin Seiki Co Ltd | Apparatus for controlling exhaust by-pass valve of turbocharger |
| SE501488C2 (en) * | 1993-07-08 | 1995-02-27 | Mecel Ab | Arrangement and procedure for idle control and charge pressure control in a supercharged internal combustion engine |
| DE102006054044A1 (en) * | 2006-11-16 | 2008-05-21 | Volkswagen Ag | Internal combustion engine i.e. otto engine, has actuator with membrane working on mechanism, and chamber connected with air system over line and clock valve, and another chamber connected with air system over line and non-return valve |
| JP6237140B2 (en) * | 2013-11-13 | 2017-11-29 | 株式会社Ihi | Diaphragm actuator and turbocharger |
| CN203742769U (en) * | 2014-01-24 | 2014-07-30 | 长城汽车股份有限公司 | Waste gas bypass valve control mechanism for engine turbocharging system |
| CN205382988U (en) * | 2016-02-04 | 2016-07-13 | 吉林大学 | Two membrane box -shaped gasoline engine exhaust turbine bypass valve control structures |
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