CN109333871A - A kind of tire skinning machine rotates smoothly driving device with bottom - Google Patents
A kind of tire skinning machine rotates smoothly driving device with bottom Download PDFInfo
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- CN109333871A CN109333871A CN201811496228.9A CN201811496228A CN109333871A CN 109333871 A CN109333871 A CN 109333871A CN 201811496228 A CN201811496228 A CN 201811496228A CN 109333871 A CN109333871 A CN 109333871A
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- helical spring
- annular array
- elastic compression
- spring elastic
- effective control
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B17/00—Recovery of plastics or other constituents of waste material containing plastics
-
- 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
- Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
- Y02W30/00—Technologies for solid waste management
- Y02W30/50—Reuse, recycling or recovery technologies
- Y02W30/62—Plastics recycling; Rubber recycling
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- Engineering & Computer Science (AREA)
- Environmental & Geological Engineering (AREA)
- Mechanical Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention discloses a kind of tire skinning machines to rotate smoothly driving device, including bottom supporting substrate with bottom.The present invention utilizes driving motor, it is able to drive armature and carries out quick and stable state, and the device is the design principle of mechanical part, under the premise of with numerous control abilities, has the characteristics that long service life and at low cost, and, the device has the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity, spin intensity can be effectively prevent excessive and lead to the generation of component damaged phenomenon, furthermore, there is the device gas turbine air drive-type external environment to be pressurized acceleration mechanism, turbine principle can be utilized, realize the acceleration for rotary part, increase ability to work, in addition, the device has horizontality loop type rotation status stable supporting mechanism, it can be realized for horizontal rotation supporting role, to realize stable working condition.
Description
Technical field
The present invention relates to waste reclamation technical field, specially a kind of tire skinning machine rotates smoothly driving with bottom
Device.
Background technique
Currently, some special components are able to carry out recycling, then re-work recycling after surface property is impaired,
In for tire recovery value highest, but existing tire skinning machine with bottom rotate smoothly driving device work it is excessively numerous
Trivial and when rotated and unstable, limitation is bigger.
Summary of the invention
The purpose of the present invention is to provide a kind of tire skinning machines to rotate smoothly driving device with bottom, to solve above-mentioned back
The problem of being proposed in scape technology.
To achieve the above object, the invention provides the following technical scheme: a kind of tire skinning machine rotates smoothly drive with bottom
Multiple main support rods are installed in the upper surface of dynamic device, including bottom supporting substrate and main rod body sleeve, the bottom supporting substrate,
The upper surface center of the bottom supporting substrate installs a driving motor by bolt and installs shell, and the driving motor installation is outer
Shell is internally provided with driving motor installation space, and a driving motor is installed in the inside of the driving motor installation space, described
Main rod body sleeve is provided centrally with main set discharge hole, and a main rod body sleeve is respectively mounted on the body of rod of multiple main support rods, more
The side of a main rod body sleeve is mounted on transverse support bar, and a gas whirlpool is installed in the end of multiple transverse support bars
It takes turns air driven external environment and is pressurized acceleration mechanism, the gas turbine air drive-type external environment is pressurized acceleration mechanism bottom
End center is fixedly connected with the electric machine main shaft top of driving motor, and the gas turbine air drive-type external environment pressurization accelerates
A main rotating shaft is installed at mechanism top center, and an annular array helical spring elastic compression formula is installed on the top of the main rotating shaft
The maximum effective control mechanism of spin intensity, the annular array helical spring elastic compression formula maximum spin intensity effectively control machine
The secondary rotary shaft of top installation one of structure, the top of multiple main support rods is mounted on a top installation base plate by main connecting plate
Bottom, the top installation base plate is provided centrally with spindle hole, and a base bearing, the master are installed in the inside of the spindle hole
The inner ring of bearing is equipped with the axis body of the secondary rotary shaft, and the top of the pair rotary shaft passes through secondary connecting plate and installs a rotational circle
Plate body, top installation base plate upper surface and rotational circle plate body lower surface are respectively arranged with first annular groove structure and second
Circular groove structure installs horizontality loop type rotation between the first annular groove structure and second annular groove structure
Turn in stable condition supporting mechanism, the upper surface of the rotational circle plate body is provided with multiple bolts hole for installation.
Further, the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity includes ring
The main hollow housing of the shape array helical spring elastic compression effective control mechanism of formula maximum spin intensity, annular array helical spring
The main hollow section of the effective control mechanism of elastic compression formula maximum spin intensity, annular array helical spring elastic compression formula are maximum
Spin intensity effective control mechanism column spinner, annular array helical spring elastic compression formula maximum spin intensity effectively control machine
The effective control mechanism of structure semi-circular recesses structure, annular array helical spring elastic compression formula maximum spin intensity is secondary hollow
Section, the effective control mechanism movable plate of annular array helical spring elastic compression formula maximum spin intensity, annular array spiral
The effective control mechanism helical spring of spring compression maximum spin intensity and annular array helical spring elastic compression formula
The maximum effective control mechanism push rod of spin intensity；The annular array helical spring elastic compression formula maximum spin intensity is effective
Control mechanism is fixedly connected with the center of main one end face of hollow housing with the end of a main rotating shaft, the annular array spiral bullet
Center of the spring elastic compression effective control mechanism of formula maximum spin intensity inside main hollow housing is the annular array spiral
The main hollow section of the effective control mechanism of spring compression maximum spin intensity, the annular array helical spring elasticity pressure
The contracting effective control mechanism of formula maximum spin intensity is being located at the annular array helical spring elastic compression formula with main hollow housing
The inside in the maximum main hollow section of the effective control mechanism of spin intensity is socketed an annular array helical spring elastic compression formula most
The effective control mechanism column spinner of big spin intensity, the annular array helical spring elastic compression formula maximum spin intensity are effective
Control mechanism is that annular array helical spring elastic compression formula maximum spin intensity effectively controls machine with the inside of main hollow housing
The secondary hollow section of structure, the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity are secondary hollow
The inside in section is in being located at the effective control mechanism master of the annular array helical spring elastic compression formula maximum spin intensity
Place the effective control mechanism activity of an annular array helical spring elastic compression formula maximum spin intensity in one end face of empty interval
Plate, the secondary hollow section of the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity is in place in institute
It states and fixes one between one end of annular array helical spring elastic compression formula maximum spin intensity effective control mechanism movable plate
The effective control mechanism helical spring of annular array helical spring elastic compression formula maximum spin intensity, the annular array spiral
One end face of spring compression maximum spin intensity effective control mechanism movable plate is provided with and its integral structure
The effective control mechanism push rod of annular array helical spring elastic compression formula maximum spin intensity, and the annular array spiral bullet
Spring elastic compression formula maximum spin intensity effective control mechanism push rod runs through the annular array helical spring elastic compression formula
The main hollow housing of the maximum effective control mechanism of spin intensity, and it is maximum to be located at the annular array helical spring elastic compression formula
The inside in the main hollow section of the effective control mechanism of spin intensity, the annular array helical spring elastic compression formula maximum rotation
The effective control mechanism of intensity is effectively controlled with push rod positioned at the annular array helical spring elastic compression formula maximum spin intensity
Mechanism processed is semicircular structure with the one end in main hollow section, and the annular array helical spring elastic compression formula maximum rotation is strong
The side for spending effective control mechanism column spinner is provided with for placing the annular array helical spring elastic compression formula maximum
The annular array helical spring elastic compression formula maximum spin intensity of spin intensity effective control mechanism push rod end is effectively controlled
Mechanism processed semi-circular recesses structure, the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
It is fixed with one end of column spinner and the end of secondary rotary shaft.
Further, the effective control mechanism spiral of the annular array helical spring elastic compression formula maximum spin intensity
It is secondary that the initial length of spring is greater than the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
The length in hollow section.
Further, the effective control mechanism push rod of the annular array helical spring elastic compression formula maximum spin intensity
The effective control mechanism of the construction profile and annular array helical spring elastic compression formula maximum spin intensity of end is semicircle recessed
The construction profile of slot structure is consistent.
Further, the gas turbine air drive-type external environment pressurization acceleration mechanism includes that gas turbine air drives
Dynamic formula external environment is pressurized acceleration mechanism and installs shell, gas turbine air drive-type external environment pressurization acceleration mechanism with turbine
Acceleration mechanism admission line, gas turbine air are pressurized with turbine installation space, gas turbine air drive-type external environment
Drive-type external environment is pressurized acceleration mechanism exhaust pipe, gas turbine air drive-type external environment pressurization acceleration mechanism is used
Admission line hole, gas turbine air drive-type external environment pressurization acceleration mechanism exhaust pipe hole, gas turbine air drive
Dynamic formula external environment is pressurized acceleration mechanism axis body mounting hole, gas turbine air drive-type external environment pressurization acceleration mechanism is used
Axis body installs shell and gas turbine air drive-type external environment is pressurized acceleration mechanism turbine；The gas turbine air drives
Dynamic formula external environment is pressurized acceleration mechanism and is provided centrally with gas turbine air drive-type external world ring with turbine installation interior of shell
Border is pressurized acceleration mechanism turbine installation space, and the gas turbine air drive-type external environment is pressurized acceleration mechanism turbine
Being respectively arranged in opposition two sides for installation shell is pressurized with the gas turbine air drive-type external environment of its integral structure
Acceleration mechanism admission line and gas turbine air drive-type external environment are pressurized acceleration mechanism exhaust pipe, the gas
Turbine air drive-type external environment is pressurized acceleration mechanism admission line and the pressurization of gas turbine air drive-type external environment
The inside of acceleration mechanism exhaust pipe is respectively arranged with connection gas turbine air drive-type external environment pressurization acceleration mechanism
Acceleration mechanism admission line hole and gas-turbine are pressurized with the gas turbine air drive-type external environment of turbine installation space
Air driven external environment is pressurized acceleration mechanism exhaust pipe hole, the gas turbine air drive-type external environment pressurization
Acceleration mechanism turbine installation housing center is run through by the axis body of electric machine main shaft, and the two is solid by bearing between position
Fixed, the electric machine main shaft is being located at gas turbine air drive-type external environment pressurization acceleration mechanism turbine installation space
Installation one is provided centrally with gas turbine air drive-type external environment pressurization acceleration mechanism and is installed with axis body on internal axis body
The gas turbine air drive-type external environment pressurization acceleration mechanism in hole installs shell, the gas turbine air driving with axis body
Formula external environment is pressurized acceleration mechanism and the side that axis body installs shell is provided with the gas turbine air with its integral structure
Drive-type external environment is pressurized acceleration mechanism turbine.
Further, the gas turbine air drive-type external environment pressurization acceleration mechanism installs the side of shell with turbine
Face is fixedly connected with the end of multiple main transverse connecting rods.
Further, the gas turbine air drive-type external environment pressurization acceleration mechanism installs outer casing end with turbine
Encapsulation process is being passed through through position by electric machine main shaft axis body in center.
Further, the horizontality loop type rotation status stable supporting mechanism includes the rotation of horizontality loop type
In stable condition supporting mechanism base circle plate, horizontality loop type rotation status stable supporting mechanism top annular plate,
Horizontality loop type rotation status stable supporting mechanism bottom centre hole, horizontality loop type rotation status stablize support
Mechanism top center hole, horizontality loop type rotation status stable supporting mechanism bottom semicircular circular groove structure, water
Level state loop type rotation status stable supporting mechanism top semi-circular circular groove structure and horizontality loop type are contorted
State stable supporting mechanism ball；Horizontality loop type rotation status stable supporting mechanism base circle plate and the level
State loop type rotation status stable supporting mechanism is respectively arranged with the rotation of horizontality loop type with the center of top annular plate
In stable condition supporting mechanism bottom centre hole and horizontality loop type rotation status stable supporting mechanism top center hole,
At the top of horizontality loop type rotation status stable supporting mechanism base circle plate and horizontality loop type is contorted
State stable supporting mechanism is respectively arranged with horizontality loop type rotation status stable supporting mechanism with top annular board bottom portion and uses
Bottom semicircular circular groove structure and horizontality loop type rotation status stable supporting mechanism top semi-circular annular groove knot
Structure, horizontality loop type rotation status stable supporting mechanism bottom semicircular circular groove structure and horizontality annular
Formula rotation status stable supporting mechanism is rotated with multiple horizontality loop types are placed between top semi-circular circular groove structure
In stable condition supporting mechanism ball.
Further, the horizontality loop type rotation status stable supporting mechanism is mounted on first with base circle plate
The inside of circular groove structure.
Further, the horizontality loop type rotation status stable supporting mechanism is mounted on second with top annular plate
The inside of circular groove structure.
Compared with prior art, the beneficial effects of the present invention are: the present invention utilizes driving motor, it is able to drive armature
Quick and stable state is carried out, and the device is the design principle of mechanical part, in the premise with numerous control abilities
Under, have the characteristics that long service life and at low cost, moreover, the device has annular array helical spring elastic compression formula maximum
The effective control mechanism of spin intensity can effectively prevent spin intensity excessive and lead to the generation of component damaged phenomenon, in addition, should
There is device gas turbine air drive-type external environment to be pressurized acceleration mechanism, can utilize turbine principle, realize for rotation
The acceleration of component increases ability to work, in addition, there is the device horizontality loop type rotation status to stablize support machine
Structure can be realized for horizontal rotation supporting role, to realize stable working condition.
Detailed description of the invention
Fig. 1 is the complete section structural schematic diagram that a kind of tire skinning machine of the present invention rotates smoothly driving device with bottom；
Fig. 2 rotates smoothly annular array helical spring elasticity in driving device with bottom for a kind of tire skinning machine of the present invention
The structural schematic diagram of the effective control mechanism of compression maximum spin intensity；
Fig. 3 is that a kind of tire skinning machine of the present invention is rotated smoothly in driving device outside gas turbine air drive-type with bottom
The structural schematic diagram of boundary's Ambient charge acceleration mechanism；
It is contorted that Fig. 4 is that a kind of tire skinning machine of the present invention with bottom rotates smoothly horizontality loop type in driving device
The structural schematic diagram of state stable supporting mechanism；
In figure: 1, bottom supporting substrate, 2, main support rod, 3, main connecting plate, 4, top installation base plate, 5, spindle hole, 6,
Base bearing, 7, secondary rotary shaft, 8, secondary connecting plate, 9, rotational circle plate body, 10, the rotation of annular array helical spring elastic compression formula maximum
Turn the effective control mechanism of intensity, 101, the effective control mechanism master of annular array helical spring elastic compression formula maximum spin intensity
Hollow housing, 102, the main hollow section of the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity,
103, the effective control mechanism column spinner of annular array helical spring elastic compression formula maximum spin intensity, 104, annular array spiral shell
Rotation spring compression maximum spin intensity effective control mechanism semi-circular recesses structure, 105, annular array helical spring
The secondary hollow section of the effective control mechanism of elastic compression formula maximum spin intensity, 106, annular array helical spring elastic compression formula
The maximum effective control mechanism movable plate of spin intensity, 107, annular array helical spring elastic compression formula maximum spin intensity has
Effect control mechanism helical spring, 108, the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity is used
Push rod, 11, main rotating shaft, 12, driving motor install shell, 13, driving motor installation space, 14, driving motor, 15, motor
Main shaft, 16, gas turbine air drive-type external environment are pressurized acceleration mechanism, 161, gas turbine air drive-type external environment
Pressurization acceleration mechanism turbine installation shell, 162, gas turbine air drive-type external environment pressurization acceleration mechanism is pacified with turbine
Dress space, 163, gas turbine air drive-type external environment pressurization acceleration mechanism admission line, 164, gas turbine air
Drive-type external environment pressurization acceleration mechanism exhaust pipe, 165, gas turbine air drive-type external environment is pressurized acceleration machine
Structure admission line hole, 166, gas turbine air drive-type external environment pressurization acceleration mechanism exhaust pipe hole, 167, gas
Body turbine air drive-type external environment pressurization acceleration mechanism axis body mounting hole, 168, gas turbine air drive-type external world ring
Border pressurization acceleration mechanism axis body installation shell, 169, gas turbine air drive-type external environment is pressurized acceleration mechanism whirlpool
Wheel, 17, transverse support bar, 18, main rod body sleeve, 19, main set discharge hole, 20, second annular groove structure, 21, horizontality ring
Form rotation status stable supporting mechanism, 211, horizontality loop type rotation status stable supporting mechanism base circle plate,
212, horizontality loop type rotation status stable supporting mechanism top annular plate, 213, horizontality loop type rotation status
Stable supporting mechanism bottom centre hole, 214, horizontality loop type rotation status stable supporting mechanism top center hole,
215, horizontality loop type rotation status stable supporting mechanism bottom semicircular circular groove structure, 216, horizontality annular
Formula rotation status stable supporting mechanism top semi-circular circular groove structure, 217, horizontality loop type rotation status stablizes branch
Support mechanism ball, 22, bolt hole.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, a kind of embodiment provided by the invention: described including bottom supporting substrate 1 and main rod body sleeve 18
Multiple main support rods 2 are installed in the upper surface of bottom supporting substrate 1, and the upper surface center of the bottom supporting substrate 1 passes through bolt
One driving motor installation shell 12 is installed, the driving motor installation shell 12 is internally provided with driving motor installation space
13, a driving motor 14 is installed in the inside of the driving motor installation space 13, and the main rod body sleeve 18 is provided centrally with
Main set discharge hole 19 is respectively mounted a main rod body sleeve 18, multiple main rod body sleeves 18 on the body of rod of multiple main support rods 2
Side be mounted on transverse support bar 17, a gas turbine air drive-type is installed in the end of multiple transverse support bars 17
External environment is pressurized acceleration mechanism 16, gas turbine air drive-type external environment pressurization 16 bottom center of acceleration mechanism with
15 top of electric machine main shaft of driving motor 14 is fixedly connected, and the gas turbine air drive-type external environment is pressurized acceleration mechanism
A main rotating shaft 11 is installed on 16 tops center, and an annular array helical spring elastic compression is installed on the top of the main rotating shaft 11
The effective control mechanism 10 of formula maximum spin intensity, the annular array helical spring elastic compression formula maximum spin intensity are effectively controlled
The secondary rotary shaft 7 of top installation one of mechanism 10 processed, the top of multiple main support rods 2 is mounted on a top by main connecting plate 3
The bottom of portion's installation base plate 4, the top installation base plate 4 are provided centrally with spindle hole 5, the inside installation of the spindle hole 5
One base bearing 6, the inner ring of the base bearing 6 are equipped with the axis body of the secondary rotary shaft 7, and the top of the pair rotary shaft 7 passes through
Secondary connecting plate 8 installs a rotational circle plate body 9, and 4 upper surface of top installation base plate and 9 lower surface of rotational circle plate body are respectively set
There are first annular groove structure 19 and second annular groove structure 20, the first annular groove structure 19 and second annular groove
One horizontality loop type rotation status stable supporting mechanism 21, the upper surface of the rotational circle plate body 9 are installed between structure 20
It is provided with multiple bolts hole 22 for installation.
Referring to Fig. 2, the effective control mechanism 10 of annular array helical spring elastic compression formula maximum spin intensity wraps
Include annular array helical spring the elastic compression effective control mechanism of formula maximum spin intensity main hollow housing 101, annular array
The main hollow section 102 of the effective control mechanism of helical spring elastic compression formula maximum spin intensity, annular array helical spring bullet
Property compression maximum spin intensity effective control mechanism column spinner 103, the rotation of annular array helical spring elastic compression formula maximum
Turn the effective control mechanism semi-circular recesses structure 104 of intensity, annular array helical spring elastic compression formula maximum spin intensity
Effective control mechanism effectively controls machine with secondary hollow section 105, annular array helical spring elastic compression formula maximum spin intensity
Structure movable plate 106, annular array helical spring elastic compression formula maximum spin intensity effective control mechanism helical spring 107
With annular array helical spring elastic compression formula maximum spin intensity effective control mechanism push rod 108；The annular array spiral shell
Revolve center and the main rotation of main 101 1 end face of hollow housing of the effective control mechanism of spring compression maximum spin intensity
The end of axis 11 is fixedly connected, the effective control mechanism master of annular array helical spring elastic compression formula maximum spin intensity
Center inside hollow housing 101 is the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
With the hollow section 102 of master, during the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity is main
Empty capsid 101 is hollow positioned at the effective control mechanism master of the annular array helical spring elastic compression formula maximum spin intensity
The inside in section 102 is socketed an effective control mechanism column spinner of annular array helical spring elastic compression formula maximum spin intensity
103, the main hollow housing 101 of the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity it is interior
Portion is the secondary hollow section 105 of the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity, the ring
The inside in the secondary hollow section 105 of the effective control mechanism of shape array helical spring elastic compression formula maximum spin intensity is being located at institute
The annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity is stated to be put with an end face in main hollow section 102
Set an effective control mechanism movable plate 106 of annular array helical spring elastic compression formula maximum spin intensity, the circular array
The secondary hollow section 105 of the effective control mechanism of column helical spring elastic compression formula maximum spin intensity is being located at the annular array
The helical spring elastic compression effective control mechanism of formula maximum spin intensity is with fixing an annular array between one end of movable plate 106
Helical spring elastic compression formula maximum spin intensity effective control mechanism helical spring 107, the annular array helical spring
One end face of elastic compression formula maximum spin intensity effective control mechanism movable plate 106 is provided with the ring with its integral structure
Shape array helical spring elastic compression formula maximum spin intensity effective control mechanism push rod 108, and the annular array spiral
Spring compression maximum spin intensity effective control mechanism push rod 108 runs through the annular array helical spring elasticity pressure
The main hollow housing 101 of the contracting effective control mechanism of formula maximum spin intensity, and it is located at the annular array helical spring elasticity pressure
The inside in the main hollow section 102 of the effective control mechanism of contracting formula maximum spin intensity, the annular array helical spring elasticity pressure
The contracting effective control mechanism of formula maximum spin intensity is being located at the annular array helical spring elastic compression formula maximum with push rod 108
The effective control mechanism of spin intensity is semicircular structure with the one end in main hollow section 102, the annular array helical spring bullet
The property effective control mechanism of compression maximum spin intensity is provided with the side of column spinner 103 for placing the annular array spiral shell
Revolve the annular array helical spring elasticity pressure of spring compression maximum spin intensity effective control mechanism 108 end of push rod
Contracting formula maximum spin intensity effective control mechanism semi-circular recesses structure 104, the annular array helical spring elastic compression
The effective control mechanism of formula maximum spin intensity is fixed with one end of column spinner 103 and the end of secondary rotary shaft 7；The annular array
The initial length of helical spring elastic compression formula maximum spin intensity effective control mechanism helical spring 107 is greater than the annular
The length in the secondary hollow section 105 of the effective control mechanism of array helical spring elastic compression formula maximum spin intensity；The annular
The construction profile and circular array of array helical spring elastic compression formula maximum spin intensity effective control mechanism 108 end of push rod
The construction profile one of column helical spring elastic compression formula maximum spin intensity effective control mechanism semi-circular recesses structure 104
Cause, main function is: when driving resistance excessive, resistance is rotated greater than annular array helical spring elastic compression formula maximum
When the elasticity of intensity effective control mechanism helical spring 107, annular array helical spring elastic compression formula maximum can be made to revolve
Turn the effective control mechanism helical spring 107 of intensity to compress, under causation, so that realizing opposite rotation between two rotary shafts
Turn, so that the too fast rotation of secondary rotary shaft 7 will not be driven, plays a protective role, so annular array helical spring elastic compression formula
The elasticity of the maximum effective control mechanism helical spring 107 of spin intensity should be less than rotation of the driving motor 14 under maximum power
Turn dynamics.
Referring to Fig. 3, the gas turbine air drive-type external environment pressurization acceleration mechanism 16 includes that gas-turbine is empty
Gas drive dynamic formula external environment is pressurized acceleration mechanism and installs shell 161, the pressurization of gas turbine air drive-type external environment with turbine
Acceleration mechanism turbine installation space 162, gas turbine air drive-type external environment are pressurized acceleration mechanism admission line
163, gas turbine air drive-type external environment pressurization acceleration mechanism exhaust pipe 164, outside gas turbine air drive-type
Boundary Ambient charge acceleration mechanism admission line hole 165, gas turbine air drive-type external environment pressurization acceleration mechanism row
Feed channel hole 166, gas turbine air drive-type external environment pressurization acceleration mechanism axis body mounting hole 167, gas-turbine are empty
Gas drive dynamic formula external environment is pressurized acceleration mechanism and installs shell 168 and the pressurization of gas turbine air drive-type external environment with axis body
Acceleration mechanism turbine 169；The gas turbine air drive-type external environment pressurization acceleration mechanism installs shell 161 with turbine
Inside center is provided with gas turbine air drive-type external environment pressurization acceleration mechanism turbine installation space 162, the gas
Body turbine air drive-type external environment be pressurized acceleration mechanism with turbine install shell 161 opposition two sides be respectively arranged with
The gas turbine air drive-type external environment pressurization acceleration mechanism admission line 163 and gas-turbine of its integral structure are empty
Gas drive dynamic formula external environment is pressurized acceleration mechanism exhaust pipe 164, the gas turbine air drive-type external environment pressurization
Acceleration mechanism admission line 163 and gas turbine air drive-type external environment are pressurized acceleration mechanism exhaust pipe 164
Inside is respectively arranged with the gas of connection gas turbine air drive-type external environment pressurization acceleration mechanism turbine installation space 162
Body turbine air drive-type external environment is pressurized acceleration mechanism admission line hole 165 and gas turbine air drive-type external world ring
Border is pressurized acceleration mechanism exhaust pipe hole 166, and the gas turbine air drive-type external environment is pressurized acceleration mechanism whirlpool
Wheel installation 161 center of shell is run through by the axis body of electric machine main shaft 15, and the two is being fixed between position by bearing, described
Electric machine main shaft 15 is being located at gas turbine air drive-type external environment pressurization acceleration mechanism in turbine installation space 162
Installation one is provided centrally with gas turbine air drive-type external environment pressurization acceleration mechanism axis body mounting hole on the axis body in portion
167 gas turbine air drive-type external environment pressurization acceleration mechanism installs shell 168, the gas turbine air with axis body
Drive-type external environment is pressurized acceleration mechanism and the side that axis body installs shell 168 is provided with the gas whirlpool with its integral structure
It takes turns air driven external environment and is pressurized acceleration mechanism turbine 169；The gas turbine air drive-type external environment pressurization
Acceleration mechanism is fixedly connected with the side that turbine installs shell 161 with the end of multiple main transverse connecting rods 17；The gas whirlpool
Wheel air driven external environment pressurization acceleration mechanism is installed 161 end center of shell with turbine and is passed through by 15 axis body of electric machine main shaft
Position is worn by encapsulation process, main function is: when work, by the exhaust outlet of a turbine and gas turbine air drive-type
External environment is pressurized acceleration mechanism and is connected with admission line 163, and when wind energy enters, driving effect can be realized.
Referring to Fig. 4, the horizontality loop type rotation status stable supporting mechanism 21 includes horizontality loop type
At the top of rotation status stable supporting mechanism base circle plate 211, horizontality loop type rotation status stable supporting mechanism
Annular slab 212, horizontality loop type rotation status stable supporting mechanism bottom centre hole 213, the rotation of horizontality loop type
Turn in stable condition supporting mechanism top center hole 214, horizontality loop type rotation status stable supporting mechanism bottom half
Toroidal cavity structure 215, horizontality loop type rotation status stable supporting mechanism top semi-circular circular groove structure 216
With horizontality loop type rotation status stable supporting mechanism ball 217；The horizontality loop type rotation status is stablized
Supporting mechanism base circle plate 211 and horizontality loop type rotation status stable supporting mechanism top annular plate 212
Center is respectively arranged with horizontality loop type rotation status stable supporting mechanism bottom centre hole 213 and horizontality annular
Formula rotation status stable supporting mechanism top center hole 214, the horizontality loop type rotation status stable supporting mechanism
With 211 top of base circle plate and 212 bottom of horizontality loop type rotation status stable supporting mechanism top annular plate point
It is not provided with horizontality loop type rotation status stable supporting mechanism bottom semicircular circular groove structure 215 and horizontality
Loop type rotation status stable supporting mechanism top semi-circular circular groove structure 216, the horizontality loop type are contorted
State stable supporting mechanism bottom semicircular circular groove structure 215 and horizontality loop type rotation status stable supporting mechanism are used
Multiple horizontality loop type rotation status stable supporting mechanism balls are placed between top semi-circular circular groove structure 216
217；The horizontality loop type rotation status stable supporting mechanism base circle plate 211 is mounted on first annular groove knot
The inside of structure 19；The horizontality loop type rotation status stable supporting mechanism top annular plate 212 is mounted on the second ring
The inside of connected in star structure 20, main function are: can be realized the stable support function of horizontal rotation.
Specifically used mode: in present invention work, before work, the equipment for being used to position tire is mounted on rotational circle plate body
Then 9 upper surface makes driving motor 14 work, at this point, under power, rotational circle plate body 9 quickly rotates, formed
The exhaust outlet of turbine, using a turbine, is passed through pipeline and gas whirlpool when spin intensity deficiency by stable work premise
The air inlet port connection in air driven external environment pressurization acceleration mechanism 16 is taken turns, under wind energy, realize auxiliary
Help the effect of driving.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
Claims (10)
1. a kind of tire skinning machine rotates smoothly driving device, including bottom supporting substrate (1) and main rod body sleeve with bottom
(18), it is characterised in that: the upper surface of the bottom supporting substrate (1) is installed by multiple main support rods (2), the bottom branch support group
Driving motor installation shell (12) is installed by bolt in the upper surface center of plate (1), and the driving motor installs shell (12)
Be internally provided with driving motor installation space (13), a driving motor is installed in the inside of the driving motor installation space (13)
(14), the main rod body sleeve (18) is provided centrally with main set discharge hole (19), on the body of rod of multiple main support rods (2)
One main rod body sleeve (18) is installed, the side of multiple main rod body sleeves (18) is mounted on transverse support bar (17), multiple
Gas turbine air drive-type external environment pressurization acceleration mechanism (16) is installed in the end of the transverse support bar (17), described
The electric machine main shaft of gas turbine air drive-type external environment pressurization acceleration mechanism (16) bottom center and driving motor (14)
(15) top is fixedly connected, gas turbine air drive-type external environment pressurization acceleration mechanism (16) top center installation one
Main rotating shaft (11), it is strong that annular array helical spring elastic compression formula maximum rotation is installed on the top of the main rotating shaft (11)
It spends effective control mechanism (10), the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity (10)
The secondary rotary shaft (7) of top installation one, the top of multiple main support rods (2) is mounted on a top by main connecting plate (3)
The bottom of installation base plate (4), the top installation base plate (4) are provided centrally with spindle hole (5), the spindle hole (5) it is interior
A base bearing (6) are installed in portion, and the inner ring of the base bearing (6) is equipped with the axis body of the secondary rotary shaft (7), the pair rotary shaft
(7) top passes through secondary connecting plate (8) and installs a rotational circle plate body (9), top installation base plate (4) upper surface and rotational circle
Plate body (9) lower surface is respectively arranged with first annular groove structure (19) and second annular groove structure (20), first ring
One horizontality loop type rotation status is installed between connected in star structure (19) and second annular groove structure (20) and stablizes support
Mechanism (21), the upper surface of the rotational circle plate body (9) are provided with multiple bolts hole (22) for installation.
2. a kind of tire skinning machine according to claim 1 rotates smoothly driving device with bottom, it is characterised in that: described
The annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity (10) includes annular array helical spring bullet
The property effective control mechanism of compression maximum spin intensity main hollow housing (101), annular array helical spring elastic compression formula
The maximum effective control mechanism of spin intensity leads hollow section (102), the rotation of annular array helical spring elastic compression formula maximum
Intensity effective control mechanism column spinner (103), annular array helical spring elastic compression formula maximum spin intensity effectively control
Mechanism semi-circular recesses structure (104), the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity
With secondary hollow section (105), the effective control mechanism movable plate of annular array helical spring elastic compression formula maximum spin intensity
(106), annular array helical spring elastic compression formula maximum spin intensity effective control mechanism helical spring (107) and annular
The array helical spring elastic compression effective control mechanism of formula maximum spin intensity is with push rod (108)；The annular array spiral bullet
The center of main (101) one end face of hollow housing of the spring elastic compression effective control mechanism of formula maximum spin intensity and a main rotating shaft
(11) end is fixedly connected, the effective control mechanism master of annular array helical spring elastic compression formula maximum spin intensity
The internal center of hollow housing (101) is that the annular array helical spring elastic compression formula maximum spin intensity effectively controls machine
The main hollow section (102) of structure, the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity are used
Main hollow housing (101) is being located at the effective control mechanism use of the annular array helical spring elastic compression formula maximum spin intensity
The inside of main hollow section (102) is socketed an effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity
With column spinner (103), the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity is led hollow
The inside of shell (101) is the secondary hollow area of the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity
Between (105), the secondary hollow section of the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
(105) inside is in being located at the effective control mechanism master of the annular array helical spring elastic compression formula maximum spin intensity
It places the effective control mechanism of an annular array helical spring elastic compression formula maximum spin intensity and uses in one end face of empty interval (102)
Movable plate (106), the secondary hollow area of the effective control mechanism of annular array helical spring elastic compression formula maximum spin intensity
Between (105) be located at the effective control mechanism movable plate of the annular array helical spring elastic compression formula maximum spin intensity
(106) an effective control mechanism spiral of annular array helical spring elastic compression formula maximum spin intensity is fixed between one end
Spring (107), the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity is with movable plate (106)
An end face be provided with and effectively controlled with the annular array helical spring elastic compression formula maximum spin intensity of its integral structure
Mechanism is with push rod (108), and the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity is with pushing away
Bar (108) runs through the main hollow housing of the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity
(101), and it is located at the main hollow area of the annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity
Between (102) inside, the effective control mechanism push rod of the annular array helical spring elastic compression formula maximum spin intensity
(108) it is being located at the main hollow section of the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
(102) one end is semicircular structure, and the annular array helical spring elastic compression formula maximum spin intensity effectively controls machine
Structure is provided with the side of column spinner (103) for placing the annular array helical spring elastic compression formula maximum spin intensity
The annular array helical spring elastic compression formula maximum spin intensity of effective control mechanism push rod (108) end effectively controls machine
Structure effectively controls machine with semi-circular recesses structure (104), the annular array helical spring elastic compression formula maximum spin intensity
Structure is fixed with one end of column spinner (103) and the end of secondary rotary shaft (7).
3. a kind of tire skinning machine according to claim 2 rotates smoothly driving device with bottom, it is characterised in that: described
The annular array helical spring elastic compression effective control mechanism of formula maximum spin intensity is big with the initial length of helical spring (107)
In the length of the secondary hollow section (105) of the effective control mechanism of the annular array helical spring elastic compression formula maximum spin intensity
Degree.
4. a kind of tire skinning machine according to claim 2 rotates smoothly driving device with bottom, it is characterised in that: described
The construction profile of annular array helical spring elastic compression formula maximum spin intensity effective control mechanism push rod (108) end and
The structure of annular array helical spring elastic compression formula maximum spin intensity effective control mechanism semi-circular recesses structure (104)
Shape is consistent.
5. a kind of tire skinning machine according to claim 1 rotates smoothly driving device with bottom, it is characterised in that: described
Gas turbine air drive-type external environment pressurization acceleration mechanism (16) includes the pressurization of gas turbine air drive-type external environment
Acceleration mechanism is installed shell (161), gas turbine air drive-type external environment pressurization acceleration mechanism with turbine and is installed with turbine
Space (162), gas turbine air drive-type external environment are pressurized acceleration mechanism admission line (163), gas turbine air
Drive-type external environment is pressurized acceleration mechanism exhaust pipe (164), the pressurization of gas turbine air drive-type external environment accelerates
Mechanism is pressurized acceleration mechanism exhaust pipe hole with admission line hole (165), gas turbine air drive-type external environment
(166), gas turbine air drive-type external environment pressurization acceleration mechanism axis body mounting hole (167), gas turbine air drive
Dynamic formula external environment is pressurized acceleration mechanism axis body installation shell (168) and the pressurization of gas turbine air drive-type external environment adds
Fast mechanism is with turbine (169)；The gas turbine air drive-type external environment pressurization acceleration mechanism installs shell with turbine
(161) inside center is provided with gas turbine air drive-type external environment pressurization acceleration mechanism turbine installation space (162),
The gas turbine air drive-type external environment pressurization acceleration mechanism installs distinguishing in opposition two sides for shell (161) with turbine
Be provided with the gas turbine air drive-type external environment of its integral structure pressurization acceleration mechanism admission line (163) and
Gas turbine air drive-type external environment is pressurized acceleration mechanism exhaust pipe (164), the gas turbine air drive-type
External environment is pressurized acceleration mechanism admission line (163) and gas turbine air drive-type external environment pressurization acceleration mechanism is used
The inside of exhaust pipe (164) is respectively arranged with connection gas turbine air drive-type external environment pressurization acceleration mechanism turbine
The gas turbine air drive-type external environment of installation space (162) is pressurized acceleration mechanism admission line hole (165) and gas
Turbine air drive-type external environment is pressurized acceleration mechanism with exhaust pipe hole (166), outside the gas turbine air drive-type
Boundary's Ambient charge acceleration mechanism turbine installation shell (161) center is run through by the axis body of electric machine main shaft (15), and the two is being passed through
It wears and is fixed between position by bearing, the electric machine main shaft (15) is being located at gas turbine air drive-type external environment increasing
Installation one is provided centrally with outside gas turbine air drive-type on the internal axis body of pressure acceleration mechanism turbine installation space (162)
The gas turbine air drive-type external environment pressurization acceleration mechanism of boundary's Ambient charge acceleration mechanism axis body mounting hole (167) is used
Axis body installs shell (168), and the gas turbine air drive-type external environment pressurization acceleration mechanism installs shell with axis body
(168) side, which is provided with, is pressurized acceleration mechanism turbine with the gas turbine air drive-type external environment of its integral structure
(169)。
6. a kind of tire skinning machine according to claim 5 rotates smoothly driving device with bottom, it is characterised in that: described
The side of gas turbine air drive-type external environment pressurization acceleration mechanism turbine installation shell (161) connects with multiple main transverse directions
The end of extension bar (17) is fixedly connected.
7. a kind of tire skinning machine according to claim 5 rotates smoothly driving device with bottom, it is characterised in that: described
Gas turbine air drive-type external environment is pressurized acceleration mechanism and installs shell (161) end center by electric machine main shaft with turbine
(15) axis body passes through encapsulation process through position.
8. a kind of tire skinning machine according to claim 1 rotates smoothly driving device with bottom, it is characterised in that: described
Horizontality loop type rotation status stable supporting mechanism (21) includes horizontality loop type rotation status stable supporting mechanism
With base circle plate (211), horizontality loop type rotation status stable supporting mechanism top annular plate (212), horizontal
State loop type rotation status stable supporting mechanism stablizes support with bottom centre hole (213), horizontality loop type rotation status
Mechanism top center hole (214), horizontality loop type rotation status stable supporting mechanism bottom semicircular annular groove knot
Structure (215), horizontality loop type rotation status stable supporting mechanism top semi-circular circular groove structure (216) and horizontal
State loop type rotation status stable supporting mechanism is with ball (217)；The horizontality loop type rotation status stablizes support machine
Structure is in base circle plate (211) and horizontality loop type rotation status stable supporting mechanism top annular plate (212)
The heart is respectively arranged with horizontality loop type rotation status stable supporting mechanism bottom centre hole (213) and horizontality annular
Formula rotation status stable supporting mechanism stablizes support machine with top center hole (214), the horizontality loop type rotation status
Structure base circle plate (211) top and horizontality loop type rotation status stable supporting mechanism top annular plate (212)
Bottom be respectively arranged with horizontality loop type rotation status stable supporting mechanism bottom semicircular circular groove structure (215) and
Horizontality loop type rotation status stable supporting mechanism top semi-circular circular groove structure (216), the horizontality ring
Form rotation status stable supporting mechanism is steady with bottom semicircular circular groove structure (215) and horizontality loop type rotation status
Determine supporting mechanism and is stablized with multiple horizontality loop type rotation status are placed between top semi-circular circular groove structure (216)
Supporting mechanism is with ball (217).
9. a kind of tire skinning machine according to claim 8 rotates smoothly driving device with bottom, it is characterised in that: described
Horizontality loop type rotation status stable supporting mechanism is mounted on first annular groove structure (19) with base circle plate (211)
Inside.
10. a kind of tire skinning machine according to claim 8 rotates smoothly driving device with bottom, it is characterised in that: institute
It states horizontality loop type rotation status stable supporting mechanism and is mounted on second annular groove structure with top annular plate (212)
(20) inside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811496228.9A CN109333871A (en) | 2018-12-07 | 2018-12-07 | A kind of tire skinning machine rotates smoothly driving device with bottom |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811496228.9A CN109333871A (en) | 2018-12-07 | 2018-12-07 | A kind of tire skinning machine rotates smoothly driving device with bottom |
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| Publication Number | Publication Date |
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| CN109333871A true CN109333871A (en) | 2019-02-15 |
Family
ID=65303238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811496228.9A Pending CN109333871A (en) | 2018-12-07 | 2018-12-07 | A kind of tire skinning machine rotates smoothly driving device with bottom |
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| Country | Link |
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| CN (1) | CN109333871A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110579302A (en) * | 2019-08-26 | 2019-12-17 | 米兰 | Centrifugal force type object maximum tension detection device |
| CN110635397A (en) * | 2019-08-31 | 2019-12-31 | 徐承玉 | End fixing device for power transmission line wire |
| CN110771518A (en) * | 2019-10-23 | 2020-02-11 | 华琳琳 | Ground cleaning device for animal husbandry |
| CN110917662A (en) * | 2019-12-09 | 2020-03-27 | 唐振三 | Micro-vibration type bubble removing device for liquid raw materials |
| CN111042989A (en) * | 2019-12-30 | 2020-04-21 | 张建兴 | Wind-driven stable rotating device |
| CN111404107A (en) * | 2020-03-26 | 2020-07-10 | 宋庆点 | Underground wire embedding device for power installation |
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| CN204782113U (en) * | 2015-07-10 | 2015-11-18 | 四川工程职业技术学院 | Revolving stage |
| CN107639709A (en) * | 2017-10-20 | 2018-01-30 | 单梦霞 | A kind of mechanical Firewood cutter |
| CN108099495A (en) * | 2017-12-22 | 2018-06-01 | 中信戴卡股份有限公司 | A kind of wheel assembly equipment |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN204782113U (en) * | 2015-07-10 | 2015-11-18 | 四川工程职业技术学院 | Revolving stage |
| CN107639709A (en) * | 2017-10-20 | 2018-01-30 | 单梦霞 | A kind of mechanical Firewood cutter |
| CN108099495A (en) * | 2017-12-22 | 2018-06-01 | 中信戴卡股份有限公司 | A kind of wheel assembly equipment |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110579302A (en) * | 2019-08-26 | 2019-12-17 | 米兰 | Centrifugal force type object maximum tension detection device |
| CN110579302B (en) * | 2019-08-26 | 2021-08-03 | 泰州亚泰金属有限公司 | Centrifugal force type object maximum tension detection device |
| CN110635397A (en) * | 2019-08-31 | 2019-12-31 | 徐承玉 | End fixing device for power transmission line wire |
| CN110771518A (en) * | 2019-10-23 | 2020-02-11 | 华琳琳 | Ground cleaning device for animal husbandry |
| CN110917662A (en) * | 2019-12-09 | 2020-03-27 | 唐振三 | Micro-vibration type bubble removing device for liquid raw materials |
| CN111042989A (en) * | 2019-12-30 | 2020-04-21 | 张建兴 | Wind-driven stable rotating device |
| CN111404107A (en) * | 2020-03-26 | 2020-07-10 | 宋庆点 | Underground wire embedding device for power installation |
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