CN109057987A - A kind of heated engine - Google Patents
A kind of heated engine Download PDFInfo
- Publication number
- CN109057987A CN109057987A CN201810879414.4A CN201810879414A CN109057987A CN 109057987 A CN109057987 A CN 109057987A CN 201810879414 A CN201810879414 A CN 201810879414A CN 109057987 A CN109057987 A CN 109057987A
- Authority
- CN
- China
- Prior art keywords
- cavity
- sliding
- end wall
- piston
- fixedly installed
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
- F02G1/00—Hot gas positive-displacement engine plants
- F02G1/04—Hot gas positive-displacement engine plants of closed-cycle type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Transmission Devices (AREA)
Abstract
The invention discloses a kind of heated engines, including fuselage, the first cavity being arranged in the fuselage and the second cavity being arranged in the fuselage, third cavity is provided with and communicated between first cavity and second cavity, the 4th cavity around the third cavity is provided in the third cavity end wall, the piston cylinder that left distal end protrudes into first cavity is fixedly installed in the third cavity, the outer surface of piston is fixedly installed with the radiating block protruded into the 4th cavity, is provided with the first sliding cavity in the piston cylinder;Device structure of the invention is simple, it is easy to operate, equipment starting is driven to adjust with equipment output axle steer by using the same power source, progressive fueling device is set during equipment work again and improves equipment fuel economy, it cooperates and does not influence between each process, energy conversion efficiency and stability are not only increased, and improves device practical performance.
Description
Technical field
The present invention relates to engine art, specifically a kind of heated engine.
Background technique
With the development of science and technology, social progress, country promotes always high-tech development, in engine art, one
It is exactly that common engine transfer efficiency is lower directly there are a relatively difficult technical problem, it is suitable to can not find in existing equipment
Itself with adjust turn to external-combustion engine, general external-combustion engine using it is open heating cause the energy to be lost, not only conversion effect
Rate is low and energy consumption is serious general, therefore a kind of equipment of urgent need effectively solves problems.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of heated engines, are able to solve above-mentioned show in the art
The problem of.
The present invention is achieved through the following technical solutions: a kind of heated engine of the invention, including fuselage, setting
The first cavity in the fuselage and the second cavity being arranged in the fuselage, first cavity and described second empty
It is provided with and communicated with third cavity between chamber, the 4th cavity around the third cavity is provided in the third cavity end wall,
The piston cylinder that left distal end protrudes into first cavity, the fixed peace of the outer surface of piston are fixedly installed in the third cavity
Equipped with the radiating block protruded into the 4th cavity, it is provided with the first sliding cavity in the piston cylinder, in first sliding cavity
What can be horizontally slipped is provided with first piston, is provided with the first sliding of left and right perforation on the right side of first sliding cavity in end wall
Hole, the first sliding bar being provided with that can be horizontally slipped in first sliding eye, the first sliding bar left distal end and institute
It states end wall on the right side of first piston to be fixedly connected, is provided with the 5th cavity of opening to the right, institute on the left of second cavity in end wall
It states and is rotatably provided with first connecting rod in the second cavity, hingedly connect between the first connecting rod and first sliding bar
It is connected to the second connecting rod, the first connecting rod bottom end is hingedly connected with the third connecting rod extended to the left, and the described 5th
It is provided with the second sliding cavity that Open Side Down in cavity roof, is connected to and sets between second sliding cavity and first sliding cavity
It is equipped with the first intercommunicating pore, can slide up and down in second sliding cavity and be provided with second piston, the second piston lower end wall
On be hingedly connected with the 4th connecting rod extended downwardly, be provided with the 6th extended downwardly in end wall on rear side of second sliding cavity
Cavity is provided with third sliding cavity in end wall on rear side of the 6th cavity, rotatable in end wall on rear side of the third sliding cavity
It is provided with the shaft through the fuselage, the shaft end in the third sliding cavity is fixedly installed with first bevel gear,
Capable of sliding back and forth in the third sliding cavity to be provided with sliding rack, the 7th that left and right perforation is provided in the sliding rack is empty
Chamber, the spline housing that front and back extends rotatably is provided in the 7th cavity, and the rotation of spline housing front and rear sides end is set
It is placed in the end wall of the 7th cavity front and back, the spline housing outer surface is fixedly installed with and the first bevel gear is detached from and cooperates
Second bevel gear and the third hand tap gear on front side of the second bevel gear, front and back perforation is provided in the spline housing
Splined hole, the splined hole internal spline is connected with the splined shaft that front and back extends, and splined shaft front and rear sides rotation is set
It is placed in the end wall of the third sliding cavity front and back, the splined shaft front side end protrudes into the 5th sky through the 6th cavity
Intracavitary, the splined shaft outer surface in the 6th cavity is fixedly installed with gear, the spline in the 5th cavity
Axis front side end is fixedly installed with cam, the 4th connecting rod and third connecting rod end be articulated and connected with it is described convex
On the end wall of wheel front side, the threaded hole through the sliding rack is provided in the sliding rack, the threaded hole screw-internal thread fit connects
It is connected to the threaded rod that front and back extends, the threaded rod front and rear sides are rotatably dispose in the end wall of the third sliding cavity front and back, institute
It states threaded rod front side end end wall on front side of the third sliding cavity and protrudes into the 6th cavity, the institute in the 6th cavity
It states threaded rod front side end and is connect with the motor power being fixedly installed in the end wall of the 6th cavity front side, the 6th cavity
The interior screw thread rod outer surface, which is fixedly installed with, is detached from cooperation sector gear with the gear.
Preferably technical solution is provided with fuel tank in end wall on the left of the fuselage, is provided on the fuel tank roof
Oil filler point outside connection, the oil filler point opening are fixedly installed with sealing cover.
Preferably technical solution is provided with the 8th cavity, the 8th cavity in end wall on the left of the 5th cavity
It is interior horizontally slip be provided with third piston, be provided with and communicated with the second intercommunicating pore between the 8th cavity and the fuel tank,
It is fixedly installed with check valve in second intercommunicating pore, is provided with and communicated with second between the 8th cavity and the 5th cavity
Sliding eye, what can be horizontally slipped in second sliding eye is provided with the second sliding bar, the second sliding bar left distal end with
End wall is fixedly connected on the right side of the third piston, is connected between the 8th cavity and first cavity and is provided with and communicated with third
Intercommunicating pore, the third connecting hole opening in first cavity are fixedly installed with atomizer.
Preferably technical solution has been fixedly installed with spark plug in end wall on the left of first cavity.
Preferably technical solution is provided with the external water inlet of connection in the 4th cavity roof and positioned at institute
State the water outlet on the right side of water inlet.
Preferably technical solution, the opposite limiting slot of the upper and lower end wall inner opening of second sliding eye, the limit
The limited block being fixedly connected with second sliding bar, the limited block and limiting slot right side are slidably provided in slot
Elasticity is provided with top pressure spring between end wall.
The beneficial effects of the present invention are: fuel is injected into the fuel tank first, so when being worked with equipment of the invention
After start the motor, while starting spark-discharge sparking, the motor rotation drives the sector rotation at this time
Dynamic to drive the gear rotation, the gear rotation drives the cam rotation, and second sliding bar is in the press at this time
It is moved to right under spring effect and twitches the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow is left
It moves that the third piston is driven to move to left, the third piston, which is moved to left, is pushed into first cavity, the combustion for the fuel
Material is atomized under atomizer effect, and atomized fuel is lighted under spark plug effect at this time, and the fuel starts pair
The first sliding intracavity gas heating, it is described to push the first piston, the first piston to the right after when gases are heated, they expand
The cam rotation is pushed by the connecting rod, the second piston moves up compressed air under cam effect at this time, this
Shi Suoshu first forms pressure difference between sliding intracavity gas, and the piston moves to left, so that the cam be driven to rotate, institute at the same time
It states motor rotation and drives the threaded rod rotation, the threaded rod rotation drives the sliding rack to move backward, the sliding rack
It moves backward and the first bevel gear is driven to engage with the third hand tap gear, at this point, cam rotation drives the spline
Axis rotation, the splined shaft rotation drive the spline housing rotation, and the spline housing rotation drives the third hand tap gear rotation,
The third hand tap gear drives the first bevel gear to rotate forward at this time, and the first bevel gear rotates forward described turn of drive
Axis rotates forward, and the splined shaft drives the cam rotation at the same time, and second sliding bar is in the press bullet at this time
It is moved to right under spring effect and twitches the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow is moved to left
To drive the third piston to move to left, the third piston, which is moved to left, is pushed into first cavity, the fuel for the fuel
It is atomized under atomizer effect, fuel is gradually added the efficiency of combustion for improving fuel, when the needs equipment is defeated
When shaft inverts, start the motor and rotate backward, the motor, which rotates backward, drives the threaded rod to rotate backward, the spiral shell
Rasp bar, which rotates backward, drives the sliding rack to move forward, the sliding rack move forward drive the first bevel gear with it is described
Second bevel gear engagement, at this point, cam rotation drives the splined shaft rotation, the splined shaft rotation drives the spline
Set rotation, the spline housing rotation drive the second bevel gear rotation, and the second bevel gear drives first cone at this time
Gear rotates backward, and the first bevel gear, which rotates backward, drives the shaft to rotate backward.
Device structure of the invention is simple, easy to operate, drives equipment starting defeated with equipment by using the same power source
Axle steer is adjusted out, and progressive fueling device is arranged during equipment work and improves equipment fuel economy, each
It cooperates and does not influence between process, not only increase energy conversion efficiency and stability, and it is practical to improve device
Performance.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.
Fig. 1 is a kind of heated engine overall structure diagram of the invention;
Fig. 2 is the structural schematic diagram of A-A in Fig. 1.
Specific embodiment
As Figure 1-Figure 2, a kind of heated engine of the invention, including fuselage 100, setting are in the fuselage 100
The first cavity 135 and the second cavity 121 for being arranged in the fuselage 100, first cavity 135 and described second empty
It is provided with and communicated with third cavity 125 between chamber 121, is provided in 125 end wall of third cavity around the third cavity 125
The 4th cavity 127, be fixedly installed with the piston cylinder that left distal end protrudes into first cavity 135 in the third cavity 125
133,133 outer surface of piston is fixedly installed with the radiating block 126 protruded into the 4th cavity 127, the piston cylinder 133
It is inside provided with the first sliding cavity 132, what can be horizontally slipped in first sliding cavity 132 is provided with first piston 130, and described
It is provided with the first sliding eye 124 of left and right perforation in one sliding cavity, 132 right side end wall, can be controlled in first sliding eye 124
The first sliding bar 123 of sliding being provided with, 123 left distal end of the first sliding bar and 130 right-hand end of first piston
Wall is fixedly connected, and the 5th cavity 118 of opening to the right, second cavity are provided in the 121 left side end wall of the second cavity
First connecting rod 122 is rotatably provided in 121, it is hinged between the first connecting rod 122 and first sliding bar 123
It is connected with the second connecting rod, 122 bottom end of first connecting rod is hingedly connected with the third connecting rod 120 extended to the left,
It is provided with the second sliding cavity 117 that Open Side Down in 5th cavity, 118 roof, second sliding cavity 117 and described the
It is provided with and communicated with the first intercommunicating pore 131 between one sliding cavity 132, can slide up and down and be provided in second sliding cavity 117
Second piston 116, is hingedly connected with the 4th connecting rod 115 extended downwardly on 116 lower end wall of second piston, and described second
The 6th cavity 140 extended downwardly, setting in the 140 rear side end wall of the 6th cavity are provided in 117 rear side end wall of sliding cavity
There is third sliding cavity 141, is rotatably provided in the 141 rear side end wall of third sliding cavity and turns through the fuselage 100
Axis 119,119 end of the shaft in the third sliding cavity 141 are fixedly installed with first bevel gear 147, and the third is sliding
It is capable of sliding back and forth in dynamic chamber 141 to be provided with sliding rack 142, the 7th cavity of left and right perforation is provided in the sliding rack 142
149, the spline housing 145 that front and back extends, 145 front and rear sides of spline housing are rotatably provided in the 7th cavity 149
End is rotatably dispose in the 149 front and back end wall of the 7th cavity, and 145 outer surface of spline housing is fixedly installed with and described
One bevel gear 147 is detached from the second bevel gear 146 of cooperation and the third hand tap gear positioned at 146 front side of second bevel gear
148, the splined hole that front and back penetrates through is provided in the spline housing 145, the splined hole internal spline is connected with front and back and extends
Splined shaft 114,114 front and rear sides of splined shaft are rotatably dispose in the 141 front and back end wall of third sliding cavity, the flower
114 front side end of key axis protrudes into the 5th cavity 118 through the 6th cavity 140, the institute in the 6th cavity 140
It states 114 outer surface of splined shaft and is fixedly installed with gear 138,114 front side end of the splined shaft in the 5th cavity 118 is solid
Dingan County is equipped with cam 113, and the 4th connecting rod 115 is articulated and connected and the cam with 120 end of third connecting rod
On 113 front side end walls, the threaded hole 144 through the sliding rack 142, the threaded hole 144 are provided in the sliding rack 142
Screw-internal thread fit is connected with the threaded rod 143 that front and back extends, and it is sliding that 143 front and rear sides of threaded rod are rotatably dispose in the third
In dynamic 141 front and back end wall of chamber, 143 front side end of threaded rod protrudes into described through the 141 front side end wall of third sliding cavity
6th cavity 140,143 front side end of the threaded rod in the 6th cavity 140 and is fixedly installed on the 6th cavity
Motor 137 in 140 front side end walls is connected by power, and 143 outer surface of the threaded rod in the 6th cavity 140 is fixedly mounted
Have and is detached from cooperation sector gear 139 with the gear 138.
Valuably, it is provided with fuel tank 103 in the 100 left side end wall of fuselage, is provided with connection on 103 roof of fuel tank
External oil filler point 101,101 opening of oil filler point are fixedly installed with sealing cover 102.
Valuably, it is provided with the 8th cavity 109 in the 118 left side end wall of the 5th cavity, it can in the 8th cavity 109
What is horizontally slipped is provided with third piston 105, is provided with and communicated with the second company between the 8th cavity 109 and the fuel tank 103
Through-hole 106 is fixedly installed with check valve 107, the 8th cavity 109 and the 5th cavity in second intercommunicating pore 106
The second sliding eye 150 is provided with and communicated between 118, what can be horizontally slipped in second sliding eye 150 is provided with the second sliding
Bar 108,108 left distal end of the second sliding bar are fixedly connected with the 105 right side end wall of third piston, the 8th cavity
It is connected between 109 and first cavity 135 and is provided with and communicated with third connecting hole 104, described in first cavity 135
104 opening of tee joint hole is fixedly installed with atomizer 134.
Valuably, it has been fixedly installed with spark plug 136 in the 135 left side end wall of the first cavity, for lighting described
One cavity, 135 fuel.
Valuably, the external water inlet 129 of connection is provided in 127 roof of the 4th cavity and positioned at the water inlet
Water outlet 128 on the right side of mouthful, convenient for coolant liquid circulation in the equipment.
Valuably, the opposite limiting slot 111 of about the 150 end wall inner opening of the second sliding eye, in the limiting slot 111
Slidably it is provided with the limited block 110 being fixedly connected with second sliding bar 108, the limited block 110 and the limit
Elasticity is provided with top pressure spring 112 between 111 right side end wall of slot.
In the initial state, the motor 137 remains static equipment of the invention, and the sliding rack 142 is located at institute
State 141 middle position of third sliding cavity, the first bevel gear 147 and the second bevel gear 146 and the triconodont
Wheel 148 is in disengaged position.
When being worked with equipment of the invention, fuel is injected into the fuel tank 103 first, then starts the motor
137, while starting the electric discharge of spark plug 136 sparking, the rotation of motor 137 drives the sector gear 139 to rotate at this time
The gear 138 is driven to rotate, the rotation of gear 138 drives the cam 113 to rotate, at this time second sliding bar 108
It is moved to right under the top pressure spring 112 effect and twitches the fuel, when the cam 113 rotates one week, the cam 113 is pushed up
It pushes away second sliding bar 108 to move to left that the third piston 105 is driven to move to left, the third piston 105 moves to left will be described
Fuel is pushed into first cavity 135, and the fuel is atomized under atomizer effect, and atomized fuel is in the fire at this time
It is lighted under 136 effect of flower plug, the fuel starts to heat gas in first sliding cavity 132, and described when gases are heated, they expand
Push the first piston 130 to the right afterwards, the first piston 130 pushes the cam 113 to rotate by the connecting rod, at this time
The second piston 116 moves up compressed air under the cam 113 effect, at this time in first sliding cavity 132 between gas
Pressure difference is formed, the piston 130 moves to left, so that the cam 113 be driven to rotate, the rotation of motor 137 is driven at the same time
The threaded rod 143 rotates, and the rotation of threaded rod 143 drives the sliding rack 142 to move backward, the sliding rack 142 to
It is mobile afterwards that the first bevel gear 147 is driven to engage with the third hand tap gear 148, at this point, the rotation of the cam 113 drives institute
The rotation of splined shaft 114 is stated, the rotation of splined shaft 114 drives the spline housing 145 to rotate, and the rotation of spline housing 145 drives
The third hand tap gear 148 rotates, and the third hand tap gear 148 drives the first bevel gear 147 to rotate forward at this time, described
First bevel gear 147, which rotates forward, drives the shaft 119 to rotate forward, and the splined shaft 114 drives described convex at the same time
113 rotation of wheel, second sliding bar 108 moves to right under the top pressure spring 112 effect and twitches the fuel at this time, when described
When cam 113 rotates one week, the second sliding bar 108 described in 113 pushing tow of cam moves to left to drive the third piston 105
It moves to left, the third piston 105, which is moved to left, is pushed into first cavity 135 for the fuel, and the fuel is in the atomizer
The lower atomization of effect, fuel is gradually added the efficiency of combustion for improving fuel, when needing equipment output shaft reversion, starting
The motor 137 rotates backward, and the motor 137, which rotates backward, drives the threaded rod 143 to rotate backward, the threaded rod
143, which rotate backward the drive sliding rack 142, moves forward, and the sliding rack 142, which moves forward, drives the first bevel gear
147 engage with the second bevel gear 146, at this point, the rotation of the cam 113 drives the splined shaft 114 to rotate, the spline
The rotation of axis 114 drives the spline housing 145 to rotate, and the rotation of spline housing 145 drives the second bevel gear 146 to rotate, this
Shi Suoshu second bevel gear 146 drives the first bevel gear 147 to rotate backward, 147 counter-rotating belts of first bevel gear
The shaft 119 is moved to rotate backward.
The beneficial effects of the present invention are: fuel is injected into the fuel tank first, so when being worked with equipment of the invention
After start the motor, while starting spark-discharge sparking, the motor rotation drives the sector rotation at this time
Dynamic to drive the gear rotation, the gear rotation drives the cam rotation, and second sliding bar is in the press at this time
It is moved to right under spring effect and twitches the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow is left
It moves that the third piston is driven to move to left, the third piston, which is moved to left, is pushed into first cavity, the combustion for the fuel
Material is atomized under atomizer effect, and atomized fuel is lighted under spark plug effect at this time, and the fuel starts pair
The first sliding intracavity gas heating, it is described to push the first piston, the first piston to the right after when gases are heated, they expand
The cam rotation is pushed by the connecting rod, the second piston moves up compressed air under cam effect at this time, this
Shi Suoshu first forms pressure difference between sliding intracavity gas, and the piston moves to left, so that the cam be driven to rotate, institute at the same time
It states motor rotation and drives the threaded rod rotation, the threaded rod rotation drives the sliding rack to move backward, the sliding rack
It moves backward and the first bevel gear is driven to engage with the third hand tap gear, at this point, cam rotation drives the spline
Axis rotation, the splined shaft rotation drive the spline housing rotation, and the spline housing rotation drives the third hand tap gear rotation,
The third hand tap gear drives the first bevel gear to rotate forward at this time, and the first bevel gear rotates forward described turn of drive
Axis rotates forward, and the splined shaft drives the cam rotation at the same time, and second sliding bar is in the press bullet at this time
It is moved to right under spring effect and twitches the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow is moved to left
To drive the third piston to move to left, the third piston, which is moved to left, is pushed into first cavity, the fuel for the fuel
It is atomized under atomizer effect, fuel is gradually added the efficiency of combustion for improving fuel, when the needs equipment is defeated
When shaft inverts, start the motor and rotate backward, the motor, which rotates backward, drives the threaded rod to rotate backward, the spiral shell
Rasp bar, which rotates backward, drives the sliding rack to move forward, the sliding rack move forward drive the first bevel gear with it is described
Second bevel gear engagement, at this point, cam rotation drives the splined shaft rotation, the splined shaft rotation drives the spline
Set rotation, the spline housing rotation drive the second bevel gear rotation, and the second bevel gear drives first cone at this time
Gear rotates backward, and the first bevel gear, which rotates backward, drives the shaft to rotate backward.
Device structure of the invention is simple, easy to operate, drives equipment starting defeated with equipment by using the same power source
Axle steer is adjusted out, and progressive fueling device is arranged during equipment work and improves equipment fuel economy, each
It cooperates and does not influence between process, not only increase energy conversion efficiency and stability, and it is practical to improve device
Performance.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection scope should be determined by the scope of protection defined in the claims.
Claims (6)
1. a kind of heated engine of the invention including fuselage, the first cavity being arranged in the fuselage and is arranged in institute
The second cavity in fuselage is stated, third cavity, the third are provided with and communicated between first cavity and second cavity
It is provided with the 4th cavity around the third cavity in cavity end wall, is fixedly installed with left distal end in the third cavity and stretches
Enter the piston cylinder of first cavity, the outer surface of piston is fixedly installed with the radiating block protruded into the 4th cavity, institute
It states and is provided with the first sliding cavity in piston cylinder, what can be horizontally slipped in first sliding cavity is provided with first piston, and described
The first sliding eye of left and right perforation, the setting that can be horizontally slipped in first sliding eye are provided on the right side of one sliding cavity in end wall
The first sliding bar having, the first sliding bar left distal end are fixedly connected with end wall on the right side of the first piston, and described second
The 5th cavity of opening to the right is provided on the left of cavity in end wall, is rotatably provided with the first connection in second cavity
Bar is hingedly connected with the second connecting rod, the first connecting rod bottom between the first connecting rod and first sliding bar
End is hingedly connected with the third connecting rod extended to the left, and the second sliding that Open Side Down is provided in the 5th cavity roof
Chamber is provided with and communicated with the first intercommunicating pore between second sliding cavity and first sliding cavity, can in second sliding cavity
What is slided up and down is provided with second piston, and the 4th connecting rod extended downwardly is hingedly connected on the second piston lower end wall,
The 6th cavity extended downwardly is provided on rear side of second sliding cavity in end wall, is provided in end wall on rear side of the 6th cavity
Third sliding cavity is rotatably provided with the shaft through the fuselage, the third in end wall on rear side of the third sliding cavity
The shaft end in sliding cavity is fixedly installed with first bevel gear, capable of sliding back and forth in the third sliding cavity to be provided with
Sliding rack is provided with the 7th cavity of left and right perforation in the sliding rack, front and back is rotatably provided in the 7th cavity
The spline housing of extension, spline housing front and rear sides end are rotatably dispose in the end wall of the 7th cavity front and back, the spline
Set outer surface, which is fixedly installed with, to be detached from the second bevel gear of cooperation with the first bevel gear and is located at the second bevel gear
The third hand tap gear of front side, the splined hole that front and back penetrates through is provided in the spline housing, and the splined hole internal spline is cooperatively connected
The splined shaft for having front and back to extend, the splined shaft front and rear sides are rotatably dispose in the end wall of the third sliding cavity front and back, described
Splined shaft front side end protrudes into the 5th cavity through the 6th cavity, outside the splined shaft in the 6th cavity
Surface is fixedly installed with gear, and the splined shaft front side end in the 5th cavity is fixedly installed with cam, and the described 4th
Connecting rod and third connecting rod end are articulated and connected and on end wall, are provided with and pass through in the sliding rack on front side of the cam
Wear the threaded hole of the sliding rack, the threaded hole screw-internal thread fit is connected with the threaded rod that front and back extends, before the threaded rod
Two sides are rotatably dispose in the end wall of the third sliding cavity front and back afterwards, and the threaded rod front side end runs through the third sliding cavity
Front side end wall protrudes into the 6th cavity, the threaded rod front side end in the 6th cavity and is fixedly installed on described the
Motor power on front side of six cavitys in end wall connects, and the screw thread rod outer surface in the 6th cavity is fixedly installed with and institute
It states gear and is detached from cooperation sector gear.
2. a kind of heated engine according to claim 1, it is characterised in that: be provided with oil in end wall on the left of the fuselage
Case, the oil filler point being provided on the fuel tank roof outside connection, the oil filler point opening are fixedly installed with sealing cover.
3. a kind of heated engine according to claim 1, it is characterised in that: setting in end wall on the left of the 5th cavity
Have the 8th cavity, what can be horizontally slipped in the 8th cavity is provided with third piston, the 8th cavity and the fuel tank it
Between be provided with and communicated with the second intercommunicating pore, be fixedly installed with check valve in second intercommunicating pore, the 8th cavity and described the
The second sliding eye is provided with and communicated between five cavitys, what can be horizontally slipped in second sliding eye is provided with the second sliding bar,
The second sliding bar left distal end is fixedly connected with end wall on the right side of the third piston, the 8th cavity and first sky
Third connecting hole is provided with and communicated between chamber, the third connecting hole opening in first cavity is fixedly installed with
Atomizer.
4. a kind of heated engine according to claim 1, it is characterised in that: fixed in end wall on the left of first cavity
Spark plug has been installed.
5. a kind of heated engine according to claim 1, it is characterised in that: the company of being provided in the 4th cavity roof
Lead to external water inlet and the water outlet on the right side of the water inlet.
6. a kind of heated engine according to claim 1, it is characterised in that: opened in end wall above and below second sliding eye
Mouthful opposite limiting slot is slidably provided with the limited block being fixedly connected with second sliding bar, institute in the limiting slot
It states elasticity between limited block and limiting slot right side end wall and is provided with top pressure spring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810879414.4A CN109057987A (en) | 2018-08-03 | 2018-08-03 | A kind of heated engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810879414.4A CN109057987A (en) | 2018-08-03 | 2018-08-03 | A kind of heated engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN109057987A true CN109057987A (en) | 2018-12-21 |
Family
ID=64833129
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810879414.4A Withdrawn CN109057987A (en) | 2018-08-03 | 2018-08-03 | A kind of heated engine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN109057987A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110001216A (en) * | 2019-04-22 | 2019-07-12 | 杭州致爱包装制品有限公司 | A kind of label machine |
-
2018
- 2018-08-03 CN CN201810879414.4A patent/CN109057987A/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110001216A (en) * | 2019-04-22 | 2019-07-12 | 杭州致爱包装制品有限公司 | A kind of label machine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109057987A (en) | A kind of heated engine | |
CN109057988A (en) | A kind of high-efficiency heating engine | |
CN109057989A (en) | A kind of Novel heating engine | |
CN109296450A (en) | A kind of application method of new energy engine | |
CN207526581U (en) | gear rotor engine | |
CN110013681B (en) | Waste heat recovery's distillation stove | |
CN203584652U (en) | Low-temperature starting system of loader-digger | |
CN203570420U (en) | Spray chamber type turbocharged internal combustion engine | |
CN101581246A (en) | Engine system being capable of strengthening the power | |
CN109098854A (en) | A kind of gas turbine | |
CN107117057B (en) | A kind of new-energy automobile charging unit | |
CN204554804U (en) | A kind of seawater decomposition combustion device | |
CN110030107A (en) | A kind of engine piston | |
CN103628977A (en) | Dual-prism rotor engine | |
CN108954385A (en) | A kind of burner and its application method of gas turbine | |
CN108177517A (en) | A kind of novel hybrid driving equipment | |
CN201461048U (en) | Generator system capable of reinforcing power | |
CN108826260A (en) | A kind of biomass solid fuel high efficient combustion device | |
CN204627741U (en) | External combustion rotary engine | |
CN208124352U (en) | A kind of integration heat accumulating burner | |
CN109098941A (en) | A kind of novel hot machine and its application method | |
CN208900246U (en) | A kind of energy-saving environmental protection device of engine | |
CN109339939A (en) | A kind of new energy engine | |
CN207073432U (en) | Novel straight-shaft engine | |
CN205895378U (en) | Internal combustion tail gas processing device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181221 |
|
WW01 | Invention patent application withdrawn after publication |