CN109057988A - A kind of high-efficiency heating engine - Google Patents
A kind of high-efficiency heating engine Download PDFInfo
- Publication number
- CN109057988A CN109057988A CN201810880120.3A CN201810880120A CN109057988A CN 109057988 A CN109057988 A CN 109057988A CN 201810880120 A CN201810880120 A CN 201810880120A CN 109057988 A CN109057988 A CN 109057988A
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- China
- Prior art keywords
- cavity
- sliding
- end wall
- fixedly installed
- piston
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Classifications
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- 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
Abstract
The invention discloses a kind of high-efficiency heating 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 high-efficiency heating 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 high-efficiency heating engines, are able to solve above-mentioned present skill
The problems in art.
The present invention is achieved through the following technical solutions: a kind of high-efficiency heating engine of the invention, including fuselage,
The first cavity being arranged in the fuselage and the second cavity being arranged in the fuselage, first cavity and described the
It is provided with and communicated with third cavity between two cavitys, the 4th sky around the third cavity is provided in the third cavity end wall
Chamber, the piston cylinder that left distal end protrudes into first cavity is fixedly installed in the third cavity, and the outer surface of piston is solid
Dingan County is equipped with the radiating block protruded into the 4th cavity, and the first sliding cavity, first sliding are provided in the piston cylinder
It is intracavitary horizontally slip be provided with first piston, be provided with left and right perforation on the right side of first sliding cavity in end wall first is sliding
Dynamic hole, the first sliding bar being provided with that can be horizontally slipped in first sliding eye, the first sliding bar left distal end with
End wall is fixedly connected on the right side of the first piston, is provided with the 5th cavity of opening to the right on the left of second cavity in end wall,
First connecting rod is rotatably provided in second cavity, it is hinged between the first connecting rod and first sliding bar
It is connected with the second connecting rod, the first connecting rod bottom end is hingedly connected with the third connecting rod extended to the left, and described
It is provided with the second sliding cavity that Open Side Down in five cavity roofs, is connected between second sliding cavity and first sliding cavity
It is provided 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
It is hingedly connected with the 4th connecting rod extended downwardly on wall, is provided with the extended downwardly on rear side of second sliding cavity in end wall
Six cavitys are provided with third sliding cavity in end wall on rear side of the 6th cavity, can be rotated in end wall on rear side of the third sliding cavity
Be provided with the shaft through the fuselage, the shaft end in the third sliding cavity is fixedly installed with the first cone tooth
It takes turns, it is capable of sliding back and forth in the third sliding cavity to be provided with sliding rack, the 7th of left and right perforation is provided in the sliding rack
Cavity is rotatably provided with the spline housing that front and back extends, the rotation of spline housing front and rear sides end in the 7th cavity
It is set in the end wall of the 7th cavity front and back, the spline housing outer surface is fixedly installed with matches with first bevel gear disengaging
The second bevel gear of conjunction and the third hand tap gear on front side of the second bevel gear are provided with front and back in the spline housing and pass through
Logical splined hole, the splined hole internal spline are connected with the splined shaft that front and back extends, the splined shaft front and rear sides rotation
It is set in the end wall of the third sliding cavity front and back, the splined shaft front side end protrudes into the described 5th through the 6th cavity
In cavity, the splined shaft outer surface in the 6th cavity is fixedly installed with gear, the flower in the 5th cavity
Key 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
On front side of cam on end wall, the threaded hole through the sliding rack, the threaded hole screw-internal thread fit are provided in the sliding rack
It is connected with 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,
The threaded rod front side end protrudes into the 6th cavity through end wall on front side of the third sliding cavity, in the 6th cavity
The threaded rod front side end is connect with the motor power being fixedly installed in the end wall of the 6th cavity front side, and the described 6th is empty
The intracavitary screw thread rod outer surface, which is fixedly installed with, is detached from cooperation sector gear with the gear, is provided with too on the fuselage
Positive energy device, the solar energy equipment includes the battery and solar panels.
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.
Preferably technical solution, is equipped with solar panels on the fuselage upper surface, fixed in the fuselage roof
The battery of storage electricity is installed
The beneficial effects of the present invention are: fuel is injected into the fuel tank first, is then opened when being worked with equipment of the invention
The motor is moved, while starting the spark-discharge sparking, the motor rotation drives the sector gear to rotate band at this time
The gear rotation is moved, the gear rotation drives the cam rotation, and second sliding bar is in the top pressure spring at this time
Moved to right under effect and twitch the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow move to left from
And the third piston is driven to move to left, the third piston moves to left the fuel being pushed into first cavity, and the fuel exists
The lower atomization of atomizer effect, atomized fuel is lighted under spark plug effect at this time, and the fuel starts to described
First sliding intracavity gas heating, described to push the first piston to the right after when gases are heated, they expand, the first piston passes through
The connecting rod pushes the cam rotation, and the second piston moves up compressed air under cam effect at this time, at this time institute
It states and forms pressure difference between the first sliding intracavity gas, the piston moves to left, so that the cam be driven to rotate, the electricity at the same time
Machine rotation drives the threaded rod rotation, and the threaded rod rotation drives the sliding rack to move backward, and the sliding rack is backward
It is mobile that the first bevel gear is driven to engage with the third hand tap gear, at this point, cam rotation drives the splined shaft to turn
Dynamic, the splined shaft rotation drives the spline housing rotation, and the spline housing rotation drives the third hand tap gear rotation, at this time
The third hand tap gear drives the first bevel gear to rotate forward, and the first bevel gear, which rotates forward, is driving the shaft just
To rotation, the splined shaft drives the cam rotation at the same time, and second sliding bar is made in the top pressure spring at this time
Moved to right under and twitch the fuel, when the cam rotates one week, the second sliding bar described in the cam pushing tow move to left thus
The third piston is driven to move to left, the third piston, which is moved to left, is pushed into first cavity for the fuel, and the fuel is in institute
The lower atomization of atomizer effect is stated, fuel is gradually added the efficiency of combustion for improving fuel, when the needs equipment output shaft
When reversion, start the motor and rotate backward, the motor, which rotates backward, drives the threaded rod to rotate backward, the threaded rod
It rotates backward and the sliding rack is driven to move forward, the sliding rack, which moves forward, drives the first bevel gear and described second
Bevel gear engagement, at this point, cam rotation drives the splined shaft rotation, the splined shaft rotation drives the spline housing to turn
Dynamic, the spline housing rotation drives the second bevel gear rotation, and the second bevel gear drives the first bevel gear at this time
It rotates backward, 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 high-efficiency heating 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 high-efficiency heating engine of the invention, including fuselage 100, setting are in the fuselage
The first cavity 135 in 100 and the second cavity 121 being arranged in the fuselage 100, first cavity 135 with it is described
It is provided with and communicated with third cavity 125 between second cavity 121, is provided in 125 end wall of third cavity around the third
4th cavity 127 of cavity 125 is fixedly installed with left distal end in the third cavity 125 and protrudes into first cavity 135
Piston cylinder 133,133 outer surface of piston are fixedly installed with the radiating block 126 protruded into the 4th cavity 127, the work
The first sliding cavity 132 is provided in plug cylinder 133, what can be horizontally slipped in first sliding cavity 132 is provided with first piston
130, the first sliding eye 124 of left and right perforation, first sliding eye are provided in the 132 right side end wall of the first sliding cavity
The first sliding bar 123 being provided with that can be horizontally slipped in 124,123 left distal end of the first sliding bar and described first are lived
It fills in 130 right side end walls to be fixedly connected, the 5th cavity 118 of opening to the right, institute is provided in the 121 left side end wall of the second cavity
It states and is rotatably provided with first connecting rod 122 in the second cavity 121, the first connecting rod 122 and first sliding bar
The second connecting rod is hingedly connected between 123,122 bottom end of first connecting rod is hingedly connected with the third extended to the left
Connecting rod 120 is provided with the second sliding cavity 117 that Open Side Down, second sliding cavity in 118 roof of the 5th cavity
It is provided with and communicated with the first intercommunicating pore 131 between 117 and first sliding cavity 132, downslide can be gone up in second sliding cavity 117
Dynamic is provided with second piston 116, is hingedly connected with the 4th connecting rod extended downwardly on 116 lower end wall of second piston
115, the 6th cavity 140 extended downwardly is provided in the 117 rear side end wall of the second sliding cavity, after the 6th cavity 140
It is provided with third sliding cavity 141 in the wall of side, is rotatably provided in the 141 rear side end wall of third sliding cavity through described
The shaft 119 of fuselage 100,119 end of the shaft in the third sliding cavity 141 are fixedly installed with first bevel gear 147,
It is capable of sliding back and forth in the third sliding cavity 141 to be provided with sliding rack 142, left and right perforation is provided in the sliding rack 142
The 7th cavity 149, the spline housing 145 that front and back extends, the spline housing are rotatably provided in the 7th cavity 149
145 front and rear sides end are rotatably dispose in the 149 front and back end wall of the 7th cavity, the fixed peace in 145 outer surface of spline housing
Equipped with the second bevel gear 146 for being detached from cooperation with the first bevel gear 147 and positioned at 146 front side of second bevel gear
Third hand tap gear 148, the splined hole that front and back penetrates through is provided in the spline housing 145, and the splined hole internal spline is cooperatively connected
The splined shaft 114 for having front and back to extend, 114 front and rear sides of splined shaft are rotatably dispose in 141 front and back end of third sliding cavity
In wall, 114 front side end of splined shaft protrudes into the 5th cavity 118 through the 6th cavity 140, and the described 6th is empty
114 outer surface of the splined shaft in chamber 140 is fixedly installed with gear 138, the splined shaft in the 5th cavity 118
114 front side ends are fixedly installed with cam 113, and the 4th connecting rod 115 hingedly connects with 120 end of third connecting rod
It connects on the 113 front side end wall of cam, the threaded hole 144 through the sliding rack 142 is provided in the sliding rack 142,
144 screw-internal thread fit of threaded hole is connected with the threaded rod 143 that front and back extends, and 143 front and rear sides of the threaded rod rotation is set
It is placed in the 141 front and back end wall of third sliding cavity, before 143 front side end of threaded rod runs through the third sliding cavity 141
Side wall protrudes into the 6th cavity 140,143 front side end of the threaded rod in the 6th cavity 140 and fixed setting
It is connected by power in the motor 137 in the 140 front side end wall of the 6th cavity, the threaded rod 143 in the 6th cavity 140
Outer surface, which is fixedly installed with, is detached from cooperation sector gear 139 with the gear 138, and solar energy dress is provided on the fuselage 100
It sets, the solar energy equipment includes the battery 201 and solar panels 200.
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.
Valuably, solar panels 200 are installed on 100 upper surface of fuselage, are fixedly mounted in 100 roof of fuselage
There is the battery 201 of storage electricity, electricity is generated when the solar panels 200 receive illumination and is stored in the battery 201
It is interior to use for equipment
In the initial state, the motor 137 remains static equipment of the invention, and the sliding rack 142 is located at described the
Three sliding cavities, 141 middle position, the first bevel gear 147 and the second bevel gear 146 and the third hand tap gear 148
It 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 (7)
1. a kind of high-efficiency heating engine of the invention, including fuselage, the first cavity being arranged in the fuselage and setting
The second cavity in the fuselage is provided with and communicated with third cavity between first cavity and second cavity, described
It is provided with the 4th cavity around the third cavity in third cavity end wall, left side end is fixedly installed in the third cavity
The piston cylinder of first cavity is protruded at end, and the outer surface of piston is fixedly installed with the heat dissipation protruded into the 4th cavity
Block is provided with the first sliding cavity in the piston cylinder, and what can be horizontally slipped in first sliding cavity is provided with first piston, institute
The first sliding eye for being provided with left and right perforation on the right side of the first sliding cavity in end wall is stated, can be horizontally slipped in first sliding eye
The first sliding bar being provided with, the first sliding bar left distal end is fixedly connected with end wall on the right side of the first piston, described
The 5th cavity of opening to the right is provided on the left of second cavity in end wall, is rotatably provided with the first company in second cavity
Extension bar is hingedly connected with the second connecting rod, the first connecting rod bottom between the first connecting rod and first sliding bar
Portion end is hingedly connected with the third connecting rod extended to the left, and the second cunning that Open Side Down is provided in the 5th cavity roof
Dynamic chamber, is provided with and communicated with the first intercommunicating pore between second sliding cavity and first sliding cavity, in second sliding cavity
It can slide up and down and be provided with second piston, the 4th connection extended downwardly is hingedly connected on the second piston lower end wall
Bar is provided with the 6th cavity extended downwardly in end wall on rear side of second sliding cavity, sets in end wall on rear side of the 6th cavity
It is equipped with third sliding cavity, is rotatably provided with the shaft through the fuselage in end wall on rear side of the third sliding cavity, it is described
The shaft end in third sliding cavity is fixedly installed with first bevel gear, capable of sliding back and forth in the third sliding cavity to set
It is equipped with sliding rack, the 7th cavity of left and right perforation is provided in the sliding rack, is rotatably provided in the 7th cavity
The spline housing that front and back extends, spline housing front and rear sides end is rotatably dispose in the end wall of the 7th cavity front and back, described
Spline housing 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 second cone
Third hand tap gear on front side of gear is provided with the splined hole that front and back penetrates through, the splined hole internal spline cooperation in the spline housing
It is connected with the splined shaft that front and back extends, the splined shaft front and rear sides are rotatably dispose in the end wall of the third sliding cavity front and back,
The splined shaft front side end protrudes into the 5th cavity through the 6th cavity, the spline in the 6th cavity
Axis outer surface is fixedly installed with gear, and the splined shaft front side end in the 5th cavity is fixedly installed with cam, described
4th connecting rod and third connecting rod end are articulated and connected and on end wall, are arranged in the sliding rack on front side of the cam
There is the threaded hole through the sliding rack, the threaded hole screw-internal thread fit is connected with the threaded rod that front and back extends, the screw thread
Bar front and rear sides are rotatably dispose in the end wall of the third sliding cavity front and back, and the threaded rod front side end is sliding through the third
End wall protrudes into the 6th cavity on front side of dynamic chamber, the threaded rod front side end in the 6th cavity and is fixedly installed on institute
The motor power connection on front side of the 6th cavity in end wall is stated, the screw thread rod outer surface in the 6th cavity is fixedly installed with
It is detached from cooperation sector gear with the gear, solar energy equipment is provided on the fuselage, the solar energy equipment includes described
Battery and solar panels.
2. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: setting in end wall on the left of the fuselage
There is fuel tank, the oil filler point being provided with outside connection on the fuel tank roof, the oil filler point opening is fixedly installed with sealing cover.
3. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: on the left of the 5th cavity in end wall
It is provided with the 8th cavity, what can be horizontally slipped in the 8th cavity is provided with third piston, the 8th cavity and the oil
It is provided with and communicated with the second intercommunicating pore between case, check valve, the 8th cavity and institute are fixedly installed in second intercommunicating pore
It states and is provided with and communicated with the second sliding eye between the 5th cavity, what can be horizontally slipped in second sliding eye is provided with the second sliding
Bar, the second sliding bar left distal end are fixedly connected with end wall on the right side of the third piston, the 8th cavity and described the
Third connecting hole is provided with and communicated between one cavity, the fixed peace of the third connecting hole opening in first cavity
Equipped with atomizer.
4. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: on the left of first cavity in end wall
It has been fixedly installed with spark plug.
5. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: setting in the 4th cavity roof
There are the water inlet outside connection and the water outlet on the right side of the water inlet.
6. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: end wall above and below second sliding eye
Inner opening opposite limiting slot is slidably provided with the limit being fixedly connected with second sliding bar in the limiting slot
Elasticity is provided with top pressure spring between end wall on the right side of block, the limited block and the limiting slot.
7. a kind of high-efficiency heating engine according to claim 1, it is characterised in that: be equipped on the fuselage upper surface
Solar panels are fixedly installed with the battery of storage electricity in the fuselage roof.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810880120.3A CN109057988A (en) | 2018-08-03 | 2018-08-03 | A kind of high-efficiency heating engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810880120.3A CN109057988A (en) | 2018-08-03 | 2018-08-03 | A kind of high-efficiency heating engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109057988A true CN109057988A (en) | 2018-12-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810880120.3A Withdrawn CN109057988A (en) | 2018-08-03 | 2018-08-03 | A kind of high-efficiency heating engine |
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| CN (1) | CN109057988A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110808435A (en) * | 2019-11-20 | 2020-02-18 | 余姚心智新能源科技有限公司 | New energy automobile battery performance promotes protector |
-
2018
- 2018-08-03 CN CN201810880120.3A patent/CN109057988A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110808435A (en) * | 2019-11-20 | 2020-02-18 | 余姚心智新能源科技有限公司 | New energy automobile battery performance promotes protector |
| CN110808435B (en) * | 2019-11-20 | 2020-08-25 | 江苏华鹏智能仪表科技股份有限公司 | New energy automobile battery performance promotes protector |
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Application publication date: 20181221 |