CN110685794B - Adjustable auxiliary device capable of prolonging service life of turbine - Google Patents
Adjustable auxiliary device capable of prolonging service life of turbine Download PDFInfo
- Publication number
- CN110685794B CN110685794B CN201911143814.XA CN201911143814A CN110685794B CN 110685794 B CN110685794 B CN 110685794B CN 201911143814 A CN201911143814 A CN 201911143814A CN 110685794 B CN110685794 B CN 110685794B
- Authority
- CN
- China
- Prior art keywords
- cavity
- communicated
- turbine
- cooling
- wall
- 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.)
- Active
Links
Images
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
-
- 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
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/005—Cooling of pump drives
-
- 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)
- Supercharger (AREA)
Abstract
The invention discloses an adjustable auxiliary device capable of prolonging the service life of a turbine, which comprises a machine body, wherein an engine is arranged on the left side of the machine body, a cavity with a rightward opening is arranged in the machine body, the turbine is fixedly arranged on the inner wall of the cavity, an exhaust cavity and an air suction cavity with a leftward opening are arranged in the machine body, the exhaust cavity and the air suction cavity are both communicated with the turbine, a power cavity is communicated between the exhaust cavity and the air suction cavity, and two sealing blocks which are symmetrical up and down are arranged on the right wall of the power cavity in a sliding manner.
Description
Technical Field
The invention relates to the technical field of turbines, in particular to an adjustable auxiliary device capable of prolonging the service life of a turbine.
Background
At present, with the continuous improvement of the technological level, the service efficiency of an automobile engine is continuously improved, the turbine is increased most commonly to realize turbocharging, after the supercharged gas is introduced into the engine again, the efficiency of the internal operation of the engine can be improved, but the automobile is suitable for long-distance or smooth road driving, on a common urban road, if the turbine is used, the turbine can be used for multiple times, the efficiency of the engine cannot be increased, carbon deposition can be increased, the service life of the turbine is shortened, and the like.
Disclosure of Invention
The object of the present invention is to provide an adjustable auxiliary device that increases the lifetime of the turbine, overcoming the above-mentioned drawbacks of the prior art.
The invention provides an adjustable auxiliary device capable of prolonging the service life of a turbine, which comprises a machine body, wherein an engine is arranged on the left side of the machine body, a cavity with a rightward opening is arranged in the machine body, the turbine is fixedly arranged on the inner wall of the cavity, an exhaust cavity and an air suction cavity with a leftward opening are arranged in the machine body, the exhaust cavity and the air suction cavity are both communicated with the turbine, a power cavity is communicated between the exhaust cavity and the air suction cavity, two vertically symmetrical sealing blocks are slidably arranged on the right wall of the power cavity, the sealing blocks can be used for sealing or communicating a channel between the turbine and the outside, a power mechanism capable of controlling the two sealing blocks to simultaneously move oppositely to achieve a sealing or communicating effect is arranged in the power cavity, a control cavity is arranged on the right side of the power cavity, the control cavity is communicated with the cavity, and an induction switch is fixedly arranged on the left side surface of the turbine, the control cavity is internally provided with a control mechanism which can be used for controlling the induction switch to be opened or closed in a linkage manner through the power mechanism, the lower side of the exhaust cavity is communicated with a through cavity, the lower side of the through cavity is communicated with a cooling cavity, the cooling cavity is communicated with the cavity, the lower side of the air suction cavity is communicated with an auxiliary cavity, the auxiliary cavity is communicated with the outside, the exhaust cavity and the air suction cavity are internally provided with a switching mechanism which can delay the operation of the turbine for a period of time after the engine stops operating, a coolable gas cooling pipe is arranged in the cooling cavity, and the cooling cavity is internally provided with a cooling mechanism which can cool gas and then supply air into the cavity in a reinforcing manner for cooling the turbine.
According to the technical scheme, an air suction pipe is communicated with the upper side of the engine and is communicated with the exhaust cavity, an exhaust pipe is communicated with the lower side of the engine and is communicated with the air suction cavity, an air suction port with an upward opening is communicated with the upper side of the exhaust cavity, and an air exhaust port with a downward opening is communicated with the lower side of the air suction cavity.
According to the technical scheme, the power mechanism comprises a motor fixedly arranged on the left wall of the power cavity, screw rods are arranged on the upper side and the lower side of the motor in a power connection mode, the screw rods are rotatably connected with the inner wall of the power cavity, sliders are connected to the periphery of the screw rods in a threaded fit mode, the sliders are connected with the left wall of the power cavity in a sliding mode, a fixed column is fixedly arranged on the right wall of the power cavity, a sliding ring is arranged on the periphery of the fixed column in a sliding mode, a first connecting rod is hinged to the front side face of each sliding ring and the corresponding slider, a second connecting rod is hinged to the front side face of the cooling cavity and the corresponding sealing block, a through hole is formed in the sealing block, and the threads.
Further technical scheme, control mechanism is including setting firmly draw runner on the sliding ring right flank, the right side intercommunication in power chamber is equipped with the slip chamber, the slip chamber with the control chamber intercommunication, the draw runner slides and establishes on the roof in slip chamber, the downside of draw runner has the tooth, it is equipped with from the driving away, pulley and rotation axis to rotate on the back wall in control chamber, first band pulley and gear have set firmly on the periphery of from the driving away, the gear can with the draw runner meshing, second band pulley and fan-shaped inductive wheel have set firmly on the periphery of rotation axis, fan-shaped inductive wheel can with inductive switch contact induction, the second band pulley with around being equipped with between the first band pulley and connecting the rope, connect the rope with pulley sliding connection.
According to the further technical scheme, a time delay device is fixedly arranged on the bottom surface of the turbine, and when the induction switch is not in contact with the fan-shaped induction wheel.
According to the technical scheme, the switch mechanism comprises a first rotating plate hinged to the right wall of the through cavity, a first spring is fixedly mounted between the first rotating plate and the right wall of the through cavity, a second rotating plate is hinged to the left wall of the auxiliary cavity, and a second spring is fixedly mounted between the second rotating plate and the right wall of the auxiliary cavity.
According to the technical scheme, the cooling mechanism comprises a fan shaft fixedly arranged between the left wall and the right wall of the cooling cavity, the right side face of the fan shaft is rotatably provided with the fan shaft, two symmetrical fan blades are fixedly arranged on the periphery of the fan shaft, a rectangular cavity is formed in the left side of the cooling cavity, a cooling device is fixedly arranged on the left wall of the rectangular cavity, and the left extending part of the cooling pipe extends into the rectangular cavity and is communicated with the cooling device.
According to the technical scheme, a first air chamber and a second air chamber are arranged in the turbine, the first air chamber is communicated with the exhaust cavity, the second air chamber is communicated with the air suction cavity, two bilaterally symmetrical connecting cavities are arranged between the first air chamber and the second air chamber in a communicated mode, a first turbine device is arranged on the top wall of the second air chamber in a rotating mode, and a second turbine device is arranged on the bottom wall of the first air chamber in a rotating mode.
Further technical scheme, the downside of gas vent with the equal fixed mounting in right side in supplementary chamber has first filter, induction port right side intercommunication is equipped with first filter chamber, the second filter has set firmly on the inner wall in first filter chamber, the second filter with the induction port intercommunication, the right side intercommunication in chamber of breathing in is equipped with the second filter chamber, fixed mounting has the third filter on the diapire in second filter chamber, the third filter with the chamber intercommunication of breathing in.
The invention has the beneficial effects that: the invention can be effectively combined with an engine, can improve the working efficiency of the engine by a turbocharging mode, can increase the using efficiency by controlling whether to use the turbine or not, can prolong the service life of the turbine, can delay the closing of the turbine when the device stops, and can blow the gas output by the turbine back to the cavity where the turbine is positioned by a cooling mode, thus being capable of quickly reducing the temperature of the turbine and prolonging the service life, wherein a power mechanism and a control mechanism can simultaneously run in a linkage way, a switching mechanism can separate two different air suction and exhaust modes, and the cooling mechanism can not only cool the gas, but also enhance the gas flow rate.
Drawings
FIG. 1 is a schematic view of the internal overall structure of the present invention;
FIG. 2 is an enlarged schematic view of the invention at A in FIG. 1;
FIG. 3 is an enlarged schematic view of the invention at B of FIG. 1;
FIG. 4 is an enlarged schematic view of the invention at C of FIG. 1;
fig. 5 is an enlarged schematic view of the invention at D in fig. 1.
Detailed Description
The invention will now be described in detail with reference to fig. 1-5, for convenience of description, the following orientations will now be defined: the up, down, left, right, and front-back directions described below correspond to the up, down, left, right, and front-back directions in the projection relationship of fig. 1 itself.
Referring to fig. 1 to 5, an adjustable auxiliary device capable of increasing the service life of a turbine according to an embodiment of the present invention includes a machine body 11, an engine 17 is disposed on a left side of the machine body 11, a cavity 41 with a rightward opening is disposed in the machine body 11, a turbine 35 is fixedly disposed on an inner wall of the cavity 41, an exhaust cavity 23 and an intake cavity 47 with a leftward opening are disposed in the machine body 11, the exhaust cavity 23 and the intake cavity 47 are both communicated with the turbine 35, a power cavity 67 is disposed between the exhaust cavity 23 and the intake cavity 47 in a communicating manner, two vertically symmetric closing blocks 27 are slidably disposed on a right wall of the power cavity 67, the closing blocks 27 can be used for closing or communicating a passage between the turbine 35 and the outside, a power mechanism 101 is disposed in the power cavity 67 and can control the two closing blocks 27 to simultaneously move in opposite directions to achieve a closing or communicating effect, a control cavity 49 is formed in the right side of the power cavity 67, the control cavity 49 is communicated with the cavity 41, an induction switch 60 is fixedly arranged on the left side surface of the turbine 35, a control mechanism 102 which can control the induction switch 60 to be opened or closed in a linkage manner through the power mechanism 101 is arranged in the control cavity 49, a through cavity 55 is communicated with the lower side of the exhaust cavity 23, a cooling cavity 29 is communicated with the lower side of the through cavity 55, the cooling cavity 29 is communicated with the cavity 41, an auxiliary cavity 48 is communicated with the lower side of the air suction cavity 47, the auxiliary cavity 48 is communicated with the outside, a switch mechanism 103 which can delay the operation of the turbine 35 for a period of time after the engine 17 stops operating is arranged in the exhaust cavity 23 and the air suction cavity 47, a coolable gas cooling pipe 31 is arranged in the cooling cavity 29, and air can be cooled and then be intensively blown into the cavity 41, a cooling mechanism 104 for cooling the turbine 35.
In addition, in one embodiment, an air intake pipe 12 is connected to the upper side of the engine 17, the air intake pipe 12 is connected to the air exhaust chamber 23, an air exhaust pipe 18 is connected to the lower side of the engine 17, the air exhaust pipe 18 is connected to the air intake chamber 47, an air intake port 24 with an upward opening is connected to the upper side of the air exhaust chamber 23, an air exhaust port 53 with a downward opening is connected to the lower side of the air intake chamber 47, and when the air exhaust chamber 23 and the air intake chamber 47 are closed by the closing block 27, the engine 17 can operate to intake and exhaust air through the air intake port 24 and the air exhaust port 53.
In addition, in one embodiment, the power mechanism 101 includes a motor 16 fixedly disposed on the left wall of the power cavity 67, both upper and lower sides of the motor 16 are respectively and dynamically connected with a screw 15, the screw 15 is rotatably connected with the inner wall of the power cavity 67, the outer periphery of the screw 15 is respectively and threadedly connected with a slider 13, the slider 13 is slidably connected with the left wall of the power cavity 67, the right wall of the power cavity 67 is fixedly provided with a fixed column 21, the outer periphery of the fixed column 21 is slidably provided with a sliding ring 19, the sliding ring 19 is hinged with the front side surface of the slider 13 to form a first connecting rod 14, the cooling cavity 29 is hinged with the front side surface of the closing block 27 to form a second connecting rod 20, the closing block 27 is provided with a through hole 28, the two screws 15 have opposite threads, and the two screws 15 can be rotated simultaneously by the operation of the motor 16, further, when the two sliders 13 are moved toward the motor 16 so that the slide ring 19 is slid rightward, the slide ring 19 moves the two closing blocks 27 away from each other, the exhaust chamber 23 communicates with the through hole 28, and the intake chamber 47 communicates with the through hole 28, the engine 17 communicates with the turbine 35, thereby achieving a turbo-charging effect.
In addition, in one embodiment, the control mechanism 102 includes a slide bar 22 fixed on the right side surface of the slip ring 19, a slide cavity 52 is provided in communication with the right side of the power cavity 67, the slide cavity 52 is in communication with the control cavity 49, the slide bar 22 is slidably provided on the top wall of the slide cavity 52, the lower side surface of the slide bar 22 is provided with teeth, a driven walking wheel 64, a pulley 51 and a rotating shaft 62 are rotatably provided on the rear wall of the control cavity 49, a first pulley 65 and a gear 66 are fixed on the outer periphery of the driven walking wheel 64, the gear 66 is engageable with the slide bar 22, a second pulley 63 and a sector sensing wheel 61 are fixed on the outer periphery of the rotating shaft 62, the sector sensing wheel 61 is in contact sensing with the sensing switch 60, a connecting rope 50 is wound between the second pulley 63 and the first pulley 65, and the connecting rope 50 is slidably connected with the pulley 51, when the slide ring 19 moves rightwards, the slide bar 22 moves rightwards, so that the gear 66 drives the driven pulley 64 to rotate, the connecting rope 50 drives the second belt pulley 63 to drive the rotating shaft 62 to rotate, so that the sector-shaped induction wheel 61 rotates, and the induction switch 60 can start the turbine 35 when the sector-shaped induction wheel 61 rotates and contacts with the induction switch 60.
In addition, in one embodiment, a time delay 42 is fixedly arranged on the bottom surface of the turbine 35, and when the inductive switch 60 is not in contact with the sector-shaped inductive wheel 61, the turbine 35 can be turned off in a delayed manner through the time delay 42.
In addition, in one embodiment, said switch mechanism 103 comprises a first rotation plate 57 hinged on the right wall of said through cavity 55, a first spring 56 is fixedly mounted between the first rotation plate 57 and the right wall of the through cavity 55, a second rotating plate 58 is hinged on the left wall of the auxiliary cavity 48, a second spring 59 is fixedly arranged between the second rotating plate 58 and the right wall of the auxiliary cavity 48, when the exhaust chamber 23 and the intake chamber 47 communicate the engine 17 and the turbine 35, and the turbine 35 is operating, the gas exhausted from the engine 17 may cause the second rotating plate 58 to rotate downward and close the auxiliary chamber 48, therefore, the turbine 35 can absorb the gas exhausted by the engine 17, and the exhausted gas after the turbine 35 is pressurized can be directly introduced into the engine 17, so that the turbocharging effect is achieved.
In addition, in one embodiment, the cooling mechanism 104 includes a fan shaft 34 secured between the left and right walls of the cooling chamber 29, the right side surface of the fan shaft 34 is rotatably provided with the fan shaft 34, two symmetrical fan blades 36 are fixedly arranged on the periphery of the fan shaft 34, a rectangular cavity 30 is arranged at the left side of the cooling cavity 29, a cooling device 32 is fixedly arranged on the left wall of the rectangular cavity 30, the left extending part of the cooling pipe 31 extends into the rectangular cavity 30 and is communicated with the cooling device 32, when the closing block 27 closes the turbine 35 and the engine 17, the first rotating plate 57 is rotated downward by the gas discharged from the turbine 35, the temperature of the turbine 35 can be lowered by allowing the air to enter the cooling chamber 29, and blowing the air into the cavity 41 through the cooling of the cooling pipe 31 and the increased flow rate of the fan blades 36.
In addition, in one embodiment, a first air chamber 37 and a second air chamber 44 are arranged in the turbine 35, the first air chamber 37 is communicated with the exhaust cavity 23, the second air chamber 44 is communicated with the suction cavity 47, two bilaterally symmetrical connecting cavities 40 are arranged between the first air chamber 37 and the second air chamber 44 in a communication mode, a first turbine 43 is rotatably arranged on the top wall of the second air chamber 44, a second turbine 38 is rotatably arranged on the bottom wall of the first air chamber 37, and a turbocharging effect can be achieved through the turbine 35.
In addition, in one embodiment, a first filter 54 is fixedly mounted on the lower side of the exhaust port 53 and the right side of the auxiliary chamber 48, a first filter chamber 26 is communicated with the right side of the air suction port 24, a second filter 25 is fixedly mounted on the inner wall of the first filter chamber 26, the second filter 25 is communicated with the air suction port 24, a second filter chamber 45 is communicated with the right side of the air suction chamber 47, a third filter 46 is fixedly mounted on the bottom wall of the second filter chamber 45, the third filter 46 is communicated with the air suction chamber 47, and the first filter 54, the third filter 46 and the second filter 25 can play a role in purifying air.
In an initial state, the two sliding blocks 13 are respectively positioned at the upper side and the lower side, the sliding ring 19 drives the sliding strip 22 to be positioned at the leftmost side, the sealing block 27 seals the exhaust cavity 23 and the air suction cavity 47, the sector sensing wheel 61 is not in contact with the sensing switch 60, the first rotating plate 57 is positioned at the horizontal position, and the second rotating plate 58 seals the air suction cavity 47.
When the sealing block 27 seals the exhaust cavity 23 and the intake cavity 47, the engine 17 can intake and exhaust air through the intake port 24 and the exhaust port 53, the two screws 15 can rotate simultaneously by the operation of the motor 16, and then the two sliding blocks 13 can move towards the motor 16, so that the sliding ring 19 can slide towards the right, the sliding ring 19 can drive the two sealing blocks 27 to move towards the sides away from each other, so that the exhaust cavity 23 can be communicated with the through hole 28, the intake cavity 47 is communicated with the through hole 28, so that the engine 17 can be communicated with the turbine 35, so as to achieve the effect of turbocharging, the sliding ring 19 can move towards the right, so that the sliding bar 22 can move towards the right, so that the gear 66 can drive the driven pulley 64 to rotate, so that the connecting rope 50 can drive the second belt pulley 63 to drive the rotating shaft 62 to rotate, so that the fan-shaped induction wheel 61 can rotate, when the fan-shaped induction wheel 61 rotates and contacts, the sensing switch 60 can start the turbine 35, when the sensing switch 60 is not in contact with the sector sensing wheel 61, the turbine 35 can be closed in a delayed manner through the time delay device 42, when the exhaust cavity 23 and the air suction cavity 47 are communicated with the engine 17 and the turbine 35, and when the turbine 35 is operated, the gas exhausted by the engine 17 can enable the second rotating plate 58 to rotate downwards and close the auxiliary cavity 48, so that the gas exhausted by the engine 17 can be absorbed by the turbine 35, the exhausted gas after the turbine 35 is pressurized can be directly introduced into the engine 17, so as to achieve a turbine pressurization effect, when the turbine 35 and the engine 17 are closed by the closing block 27, the gas exhausted by the turbine 35 can enable the first rotating plate 57 to rotate downwards, so as to enable the gas to enter the cooling cavity 29, the gas is blown into the cavity 41 through the cooling of the cooling pipe 31 and the enhanced flow rate of the fan blades 36, so that the temperature of the turbine 35 can be reduced, the first filter 54, the third filter 46 and the second filter 25 can be used to clean gas.
The invention has the beneficial effects that: the invention can be effectively combined with an engine, can improve the working efficiency of the engine by a turbocharging mode, can increase the using efficiency by controlling whether to use the turbine or not, can prolong the service life of the turbine, can delay the closing of the turbine when the device stops, and can blow the gas output by the turbine back to the cavity where the turbine is positioned by a cooling mode, thus being capable of quickly reducing the temperature of the turbine and prolonging the service life, wherein a power mechanism and a control mechanism can simultaneously run in a linkage way, a switching mechanism can separate two different air suction and exhaust modes, and the cooling mechanism can not only cool the gas, but also enhance the gas flow rate.
It will be apparent to those skilled in the art that various modifications may be made to the above embodiments without departing from the general spirit and concept of the invention. All falling within the scope of protection of the present invention. The protection scheme of the invention is subject to the appended claims.
Claims (1)
1. An adjustable auxiliary device capable of prolonging the service life of a turbine comprises a machine body, and is characterized in that: the engine is arranged on the left side of the machine body, a cavity with a right opening is formed in the machine body, a turbine is fixedly arranged on the inner wall of the cavity, an exhaust cavity and an air suction cavity with a left opening are formed in the machine body, the exhaust cavity and the air suction cavity are both communicated with the turbine, a power cavity is communicated between the exhaust cavity and the air suction cavity, two sealing blocks which are symmetrical up and down are arranged on the right wall of the power cavity in a sliding mode, the sealing blocks can be used for sealing or communicating a passage between the turbine and the outside, and a power mechanism capable of controlling the two sealing blocks to move in opposite directions simultaneously to achieve a sealing or communicating effect is arranged in the power cavity; a control cavity is arranged on the right side of the power cavity and is communicated with the cavity, an inductive switch is fixedly arranged on the left side surface of the turbine, the control cavity is internally provided with a control mechanism which can control the induction switch to be turned on or off in a linkage way through the power mechanism, the lower side of the exhaust cavity is communicated with a through cavity, the lower side of the through cavity is communicated with a cooling cavity, the cooling cavity is communicated with the cavity, an auxiliary cavity is communicated with the lower side of the air suction cavity and communicated with the outside, an exhaust cavity and the air suction cavity are internally provided with a cavity which can be used for exhausting air, a switching mechanism for delaying the operation of the turbine for a period of time, a coolable gas cooling pipe arranged in the cooling cavity, the cooling cavity is internally provided with a cooling mechanism which can cool the gas and then intensively blow the gas into the cavity for cooling the turbine; an air suction pipe is communicated with the upper side of the engine and is communicated with the exhaust cavity, an exhaust pipe is communicated with the lower side of the engine and is communicated with the air suction cavity, an air suction port with an upward opening is communicated with the upper side of the exhaust cavity, and an exhaust port with a downward opening is communicated with the lower side of the air suction cavity; the power mechanism comprises a motor fixedly arranged on the left wall of the power cavity, the upper side and the lower side of the motor are both provided with screw rods in power connection, the screw rods are rotatably connected with the inner wall of the power cavity, the periphery of each screw rod is connected with a sliding block in a threaded fit manner, the sliding block is connected with the left wall of the power cavity in a sliding manner, the right wall of the power cavity is fixedly provided with a fixed column, the periphery of the fixed column is provided with a sliding ring in a sliding manner, the sliding ring is hinged with the front side surface of the sliding block to form a first connecting rod, the cooling cavity is hinged with the front side surface of the sealing block to form a second connecting rod, a through hole is formed in the sealing block; the control mechanism comprises a sliding strip fixedly arranged on the right side surface of the slip ring, the right side of the power cavity is communicated with a sliding cavity, the sliding cavity is communicated with the control cavity, the sliding strip is slidably arranged on the top wall of the sliding cavity, teeth are arranged on the lower side surface of the sliding strip, a driven walking wheel, a pulley and a rotating shaft are rotatably arranged on the rear wall of the control cavity, a first belt wheel and a gear are fixedly arranged on the periphery of the driven walking wheel, the gear can be meshed with the sliding strip, a second belt wheel and a fan-shaped induction wheel are fixedly arranged on the periphery of the rotating shaft, the fan-shaped induction wheel can be in contact induction with the induction switch, a connecting rope is wound between the second belt wheel and the first belt wheel, and the connecting rope is in sliding connection with the pulley; a time delay device is fixedly arranged on the bottom surface of the turbine, and when the induction switch is not in contact with the fan-shaped induction wheel; the switch mechanism comprises a first rotating plate hinged to the right wall of the through cavity, a first spring is fixedly installed between the first rotating plate and the right wall of the through cavity, a second rotating plate is hinged to the left wall of the auxiliary cavity, and a second spring is fixedly installed between the second rotating plate and the right wall of the auxiliary cavity; the cooling mechanism comprises a fan shaft fixedly arranged between the left wall and the right wall of the cooling cavity, the right side surface of the fan shaft is rotatably provided with the fan shaft, two symmetrical fan blades are fixedly arranged on the periphery of the fan shaft, the left side of the cooling cavity is provided with a rectangular cavity, the left wall of the rectangular cavity is fixedly provided with a cooling device, and the leftwards extending part of the cooling pipe extends into the rectangular cavity and is communicated with the cooling device; a first air chamber and a second air chamber are arranged in the turbine, the first air chamber is communicated with the exhaust cavity, the second air chamber is communicated with the air suction cavity, two bilaterally symmetrical connecting cavities are communicated between the first air chamber and the second air chamber, a first turbine device is rotatably arranged on the top wall of the second air chamber, and a second turbine device is rotatably arranged on the bottom wall of the first air chamber; the downside of gas vent with the equal fixed mounting in right side in supplementary chamber has first filter, induction port right side intercommunication is equipped with first filter chamber, the second filter has set firmly on the inner wall in first filter chamber, the second filter with the induction port intercommunication, the right side intercommunication in chamber of breathing in is equipped with the second filter chamber, fixed mounting has the third filter on the diapire in second filter chamber, the third filter with the chamber intercommunication of breathing in.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911143814.XA CN110685794B (en) | 2019-11-20 | 2019-11-20 | Adjustable auxiliary device capable of prolonging service life of turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911143814.XA CN110685794B (en) | 2019-11-20 | 2019-11-20 | Adjustable auxiliary device capable of prolonging service life of turbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110685794A CN110685794A (en) | 2020-01-14 |
| CN110685794B true CN110685794B (en) | 2021-03-12 |
Family
ID=69117120
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911143814.XA Active CN110685794B (en) | 2019-11-20 | 2019-11-20 | Adjustable auxiliary device capable of prolonging service life of turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110685794B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201284121Y (en) * | 2008-08-30 | 2009-08-05 | 江苏天奇物流系统工程股份有限公司 | Equipment with safety maintenance apparatus |
| CN102089509A (en) * | 2008-07-16 | 2011-06-08 | 博格华纳公司 | Diagnosing a cooling subsystem of an engine system in response to dynamic pressure sensed in the subsystem |
| CN104334240A (en) * | 2013-08-22 | 2015-02-04 | Ykk株式会社 | Slide Fastener Manufacturing Device And Slide Fastener Manufacturing Method |
| CN104712419A (en) * | 2013-12-17 | 2015-06-17 | 现代自动车株式会社 | Engine system |
| CN105637192A (en) * | 2013-10-16 | 2016-06-01 | 瓦锡兰芬兰有限公司 | Method for operating an internal combustion engine |
| CN107969379A (en) * | 2017-12-01 | 2018-05-01 | 泉州速创时代工业设计有限公司 | A kind of circular movable aerator |
| CN108211634A (en) * | 2018-02-13 | 2018-06-29 | 卢素珠 | A kind of Petroleum refining purifying apparatus of smoke and fume |
| CN109083740A (en) * | 2018-08-13 | 2018-12-25 | 金华市亨宝物资有限公司 | A kind of method and apparatus of durable adjusting turbine |
| CN110076036A (en) * | 2019-06-04 | 2019-08-02 | 台州市椒江预提自动化设备有限公司 | A kind of trees antifreezeization spraying method and spraying equipment |
| CN110330097A (en) * | 2019-08-01 | 2019-10-15 | 仙居卡贝环保科技有限公司 | A kind of multi-stage aeration device for sewage treatment |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58206823A (en) * | 1982-05-28 | 1983-12-02 | Aisin Seiki Co Ltd | Exhaust air regeneration control system of diesel engine with supercharger |
| US6205784B1 (en) * | 1999-07-27 | 2001-03-27 | Alliedsignal Inc. | Integrally mounted pneumatic solenoid valve for wastegate control |
| DE10156704A1 (en) * | 2001-11-13 | 2003-05-22 | Iav Gmbh | Method and appliance for operating exhaust gas turbocharger for IC engines with electrically assisted drive based on comparison of actual operating conditions and family of operating characteristics |
| FR2836700A1 (en) * | 2002-03-01 | 2003-09-05 | Renault | LOW PRESSURE EXHAUST GAS RECIRCULATION SYSTEM |
| US6931842B2 (en) * | 2002-11-29 | 2005-08-23 | Nissan Motor Co., Ltd. | Regeneration of diesel particulate filter |
| DE602006007463D1 (en) * | 2005-05-11 | 2009-08-06 | Borgwarner Inc | ENGINE AIR MANAGEMENT SYSTEM |
| CN101054921B (en) * | 2007-05-21 | 2010-07-07 | 哈尔滨工程大学 | Turbo supercharger surging forecast control device for ship-mounted diesel engine and its control method |
-
2019
- 2019-11-20 CN CN201911143814.XA patent/CN110685794B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102089509A (en) * | 2008-07-16 | 2011-06-08 | 博格华纳公司 | Diagnosing a cooling subsystem of an engine system in response to dynamic pressure sensed in the subsystem |
| CN201284121Y (en) * | 2008-08-30 | 2009-08-05 | 江苏天奇物流系统工程股份有限公司 | Equipment with safety maintenance apparatus |
| CN104334240A (en) * | 2013-08-22 | 2015-02-04 | Ykk株式会社 | Slide Fastener Manufacturing Device And Slide Fastener Manufacturing Method |
| CN105637192A (en) * | 2013-10-16 | 2016-06-01 | 瓦锡兰芬兰有限公司 | Method for operating an internal combustion engine |
| CN104712419A (en) * | 2013-12-17 | 2015-06-17 | 现代自动车株式会社 | Engine system |
| CN107969379A (en) * | 2017-12-01 | 2018-05-01 | 泉州速创时代工业设计有限公司 | A kind of circular movable aerator |
| CN108211634A (en) * | 2018-02-13 | 2018-06-29 | 卢素珠 | A kind of Petroleum refining purifying apparatus of smoke and fume |
| CN109083740A (en) * | 2018-08-13 | 2018-12-25 | 金华市亨宝物资有限公司 | A kind of method and apparatus of durable adjusting turbine |
| CN110076036A (en) * | 2019-06-04 | 2019-08-02 | 台州市椒江预提自动化设备有限公司 | A kind of trees antifreezeization spraying method and spraying equipment |
| CN110330097A (en) * | 2019-08-01 | 2019-10-15 | 仙居卡贝环保科技有限公司 | A kind of multi-stage aeration device for sewage treatment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110685794A (en) | 2020-01-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1775392A3 (en) | Construction machine | |
| CN110685794B (en) | Adjustable auxiliary device capable of prolonging service life of turbine | |
| CN111678348A (en) | Device for rapidly cooling box-type furnace | |
| CN101272073B (en) | Ventilated cooling rainproof high-speed motor of electric bicycle | |
| CN209256099U (en) | It is a kind of for the radium-shine equipment carved characters of touch tablet | |
| CN218063507U (en) | High-frequency three-way reversing valve convenient for removing impurities in valve | |
| CN110925827A (en) | Side-draft range hood with underlying reverse fan system | |
| CN102562185B (en) | Two-channel variable-section volute device with flow-guiding blades | |
| CN111058903B (en) | Turbine engine with protection function | |
| CN209897445U (en) | Novel electronic device | |
| CN107377178B (en) | A kind of breaker of agricultural production industry solid block fertilizer | |
| CN206159117U (en) | Adjustable electricelectric of impeller moves electronic pump | |
| CN211162455U (en) | Dust collection pipeline structure capable of controlling opening and closing of multiple air outlets | |
| CN211852809U (en) | Intercooler side seal structure | |
| CN214501537U (en) | Pollution prevention and control device for improving air quality of underground building | |
| CN217164505U (en) | Hydraulic breaking hammer capable of automatically adjusting stroke | |
| CN215172373U (en) | But valve of catalytic combustion furnace of high temperature regulation | |
| CN213072505U (en) | Banbury mixer frequency conversion device | |
| CN214662192U (en) | Small-gap low-leakage high-throughput rotary valve | |
| CN213063641U (en) | Novel mining adjustable wind window | |
| CN215217171U (en) | Curing oven convenient to slide cooling | |
| CN211529016U (en) | Cooling control device for automobile engine exhaust pipe bench test | |
| CN213383783U (en) | Energy-saving automobile temperature adjusting device | |
| CN220437150U (en) | Cooling device for white corundum smelting | |
| CN215902418U (en) | Organic waste gas administers movable high-efficient collection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210218 Address after: 215000 Ruyuan Road, science and Technology Park, Xiangcheng Economic Development Zone, Suzhou City, Jiangsu Province Applicant after: Suzhou Ketai Technology Co.,Ltd. Address before: Room 703, 7 / F, building 7, Bosi Mingzuo, Xicheng, Xihu District, Hangzhou City, Zhejiang Province, 310013 Applicant before: Hangzhou nanzhixin Technology Co.,Ltd. |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |