CN108942545A

CN108942545A - A kind of high efficiency Vortex wheel turbine

Info

Publication number: CN108942545A
Application number: CN201810924363.2A
Authority: CN
Inventors: 张振寰
Original assignee: Xuancheng Fei Cheng Environmental Protection Technology Co Ltd
Current assignee: Xuancheng Fei Cheng Environmental Protection Technology Co Ltd
Priority date: 2018-08-14
Filing date: 2018-08-14
Publication date: 2018-12-07

Abstract

The invention discloses a kind of high efficiency Vortex wheel turbines, including motivation body, the first cavity determining fuselage and being arranged in the motivation body, the second cavity is provided with below first cavity, the first rotation axis that left and right extends is provided in first cavity, the first rotation axis left distal end is connect with the motor power being fixed in the end wall of the first cavity left side, the first rotation axis right end is fixedly installed first bevel gear, rotation is provided with the second rotation axis extended up and down between first cavity and second cavity, the second rotation axis top end is fixedly installed the second bevel gear engaged with the first bevel gear；Device structure of the invention is simple, utilize electrical energy drive mechanical structure, the equipment is realized as needed automatically to polish to blade, and the polishing of homogeneous constant depth is carried out to blade, save blade processing, time and labour cost are saved simultaneously, guarantees the surface accuracy of blade, improves automation degree of equipment and practicability.

Description

A kind of high efficiency Vortex wheel turbine

Technical field

The present invention relates to machine finishing field, specifically a kind of high efficiency Vortex wheel turbine.

Background technique

With the development of the times, the demand of electric power is continuously increased, and the construction demand of generating set is consequently increased, and is sent out at present Motor group is to drive electrical power generators by the rotation of steam turbine, and the Vortex wheel turbine thermal efficiency is higher, and be vortexed The blade of wheeled steam turbine, which needs to polish after casting, to be finished, and the blade polishing of steam turbine is largely added using artificial at present Work, inefficiency, while easily there is excessively polishing or the excessively shallow problem of grinding depth, and existing equipment cost is excessively high, therefore need A kind of low-cost equipment solution problems.

Summary of the invention

Technical problem to be solved by the invention is to provide a kind of high efficiency Vortex wheel turbines, are able to solve above-mentioned The problems in present technology.

The present invention is achieved through the following technical solutions: a kind of high efficiency Vortex wheel turbine of the invention, packet The first cavity for including motivation body, determining fuselage and being arranged in the motivation body, the first cavity lower section are provided with the second sky Chamber is provided with the first rotation axis that left and right extends, the first rotation axis left distal end and fixed setting in first cavity Motor power connection on the left of first cavity in end wall, the first rotation axis right end are fixedly installed the first cone Gear rotates between first cavity and second cavity and is provided with the second rotation axis extended up and down, and described second turn Moving axis top end is fixedly installed the second bevel gear engaged with the first bevel gear, the second rotation axis bottom end It is provided with first gear, rotation is provided with the third rotation axis extended up and down, third rotation axis top in second cavity Portion end is provided with the first gear ring, has been engaged first planetary gear between first gear ring and the first gear, institute It states third rotation axis bottom end and is fixedly installed second gear, rotation is provided with the 4th extended up and down in second cavity Rotation axis, the 4th rotation axis top end are fixedly installed the third gear engaged with the second gear, and the described 4th The 4th gear is fixedly installed in rotation axis bottom end, and rotation is provided with the 5th rotation axis extended up and down in first cavity, The 5th rotation axis bottom end is fixedly installed the third hand tap gear engaged with the first bevel gear, the 5th rotation Axis outer surface is fixedly installed the first pulley above the third hand tap gear, and rotation is provided in first cavity 6th rotation axis of lower extension, the 6th rotation axis top end are fixedly installed the second belt wheel, second belt wheel and institute It states transmission between first pulley and is provided with the first belt, be provided with third cavity, the third cavity below first cavity Interior setting sliding block capable of sliding back and forth, is provided with the 4th cavity in the sliding block, outside the 6th rotation axis in the 4th cavity Surface is fixedly installed the 5th gear, and the 6th rotation axis outer surface rotation is provided with the 7th rotation axis extended up and down, institute It states the 7th rotation axis bottom end and is fixedly installed the second gear ring, be engaged between second gear ring and the 5th gear There is the second planetary gear, the 7th rotation axis top end is fixedly installed the 6th gear, and rotation is set in the 4th cavity It is equipped with the 7th rotation axis extended up and down, the 7th rotation axis top end is fixedly installed the 7th gear, and described 7th turn Moving axis bottom end is fixedly installed the 4th bevel gear, and it is dynamic to be provided with the eight revolution that left and right extends for rotation in the 4th cavity By spline engagement, the eight revolution moving axis outer surface is fixedly installed for axis, the eight revolution moving axis and its described rotation axis The 5th bevel gear engaged with the 4th bevel gear, described eight revolution moving axis or so end symmetrical is provided with the first traveling wheel, described Sliding block front side end be provided with the first traveling wheel symmetrical structure, it is recessed that the 6th rotation axis bottom end is provided with first Slot is slidably provided with eight revolution moving axis in first groove, and the eight revolution moving axis top end is fixedly installed One permanent magnetism iron slider, elasticity is provided with the first spring between the first permanent magnetism iron slider and first groove, and described first The first electromagnet is fixedly installed in groove top end wall, the eight revolution moving axis bottom end is fixedly installed link block, position It is provided with sanding block below the link block, elasticity is provided with second spring between the link block and the sanding block, should Equipment is provided with emergency stop device, and it includes scram button, the 5th spring and the 9th hard contact and the tenth hard contact.

Preferably technical solution, second rotation axis outer surface are fixedly installed third belt wheel, and described 4th turn Moving axis outer surface is fixedly installed the eighth gear below the third gear, in second cavity above and below rotation setting What is extended has the 9th rotation axis, and the 9th rotation axis top end is fixedly installed the 4th belt wheel, the 4th belt wheel and institute It states transmission between third belt wheel and is provided with the second belt, the 9th rotation axis bottom end is fixedly installed and the octadentate Wheel is detached from the 9th gear of cooperation, is provided with the first sliding cavity below second cavity, is provided in first sliding cavity Elasticity setting third bullet between end wall on the right side of second permanent magnetism iron slider, the second permanent magnetism iron slider and first sliding cavity Spring is fixedly installed the second electromagnet in end wall on the right side of first sliding cavity, is conducive to control the motivation body quickly to the left Sliding, returns to initial position.

Preferably technical solution, described to determine to be provided with the second sliding groove in fuselage, end wall on rear side of second cavity Upper rotation is provided with the second traveling wheel with second sliding groove cooperation, described to determine to be provided with the first sliding groove in fuselage, institute It states and is fixedly installed first rack gear engaged with the 4th gear in end wall on rear side of the first sliding groove, be conducive to support simultaneously Mobile motivation body.

Preferably technical solution is provided with third sliding groove in end wall on the left of the third cavity, and the third is sliding Third sliding block is provided in dynamic slot, rotation is provided with the 5th belt wheel, the third sliding block and the third on the third sliding block Elasticity is provided with the 4th spring between sliding groove, is conducive to during second belt wheel slides back and forth, the first belt always with The first pulley and the cooperation of the second belt wheel transmission.

Preferably technical solution is provided with the 4th sliding groove in end wall on the left of the 4th cavity, and the described 4th is sliding The second permanent magnetism iron slider that left and right extends is provided in dynamic slot, the second permanent magnetism iron slider right end rotation is provided with and institute It states the 6th gear and the 7th gear is detached from the tenth gear of cooperation, the third permanent magnetism iron slider left pivot movement is provided with The gear set of cooperation, the third permanent magnetism iron slider left distal end and institute are detached from the 6th gear and the 7th gear It states elasticity between the end wall of the 4th sliding groove left side and is provided with the 4th spring, be fixedly installed in end wall on the left of the 4th sliding groove Third electromagnet, is conducive to control the sliding block and slides back and forth.

Preferably technical solution is fixedly installed the first hard contact on end wall on the left of second cavity, described Be fixedly installed the second hard contact on the right side of second cavity on end wall, it is described determine to be fixedly installed on the end wall of fuselage left side with it is described The third hard contact of first hard contact cooperation, it is described to determine to be fixedly installed on end wall on the right side of fuselage and second metal touching Point is detached from the 4th hard contact of cooperation, is fixedly installed fifth metal contact on rear side of the sliding block on end wall, before the sliding block It is fixedly installed the 6th hard contact on the wall of side, is fixedly installed and the fifth metal on end wall on rear side of the third cavity 7th hard contact of contact cooperation is fixedly installed on front side of the third cavity on end wall and the 6th hard contact is detached from 8th hard contact of cooperation is conducive to control first electromagnet, the second electromagnet and the energization of third electromagnet and break Electricity is conducive to control the electric machine operation state.

Preferably technical solution, it is described to determine to be provided with the second groove on the left of fuselage in end wall, in second groove Sliding is provided with scram button, and elasticity is provided with the 5th spring between end wall on the right side of the scram button and second groove, It is fixedly installed the 9th hard contact on the scram button, is provided with and the 9th gold medal in end wall on the right side of second groove The tenth hard contact for belonging to contact cooperation, is conducive to the emergent stopping work of the equipment when an emergency happens, and prevents urgency Stop device accidentally touches, and improves the safety of the equipment.

The beneficial effects of the present invention are: the motivation body is determined on the left of fuselage positioned at described, first hard contact and institute The cooperation of third hard contact is stated, second electromagnet is not powered on, and the third gear is engaged with the second gear, the cunning Block is located on front side of the third cavity, and the 6th hard contact and the 8th hard contact cooperate, first electromagnet Be not powered on, the third electromagnet is not powered on, the tenth gear and the gear set with the 6th gear and institute It states the 7th gear and is detached from cooperation.

When using equipment polishing blade of the invention, the third electromagnet forward direction is powered, and the third electromagnet is sliding Block slides to the left drives the tenth gear to slide to the left, the tenth gear and the 6th gear and the 7th tooth Engagement is taken turns, the motor is started to work, and the motor drives first rotation axis to rotate, described in the first rotation axis drive First bevel gear rotation, the first bevel gear drive the second bevel gear rotation, and the second bevel gear drives the first tooth Wheel rotation, the first gear drive the first planetary gear rotation, and the first planetary gear drives first gear ring Rotation, first gear ring drive the second gear rotation, and the second gear drives the third gear rotation, and described the Three gears drive the 4th gear rotation, and Slideslip, the first bevel gear drive the third cone to the motivation body to the right Gear rotation, the third hand tap gear drive the first pulley rotation, and the first pulley drives the third belt wheel rotation, The third belt wheel drives the 6th rotation axis rotation, and the 6th rotation axis drives the 5th gear rotation, and described the Five gears drive, second planetary gear rotation, the second planetary gear drive second ring gear against rotation, described second Gear ring drives the rotation of the 6th gear, and the 6th gear drives the tenth gear rotation, and the tenth gear drives described the The engagement of seven gears, the 7th gear drive the 4th bevel gear rotation, and the 4th bevel gear drives the 5th cone tooth Wheel rotation, the 5th bevel gear drive the first walking rotation dynamic, and the sliding block moves backward, the 6th rotation axis band The eight revolution moving axis rotation is moved, the eight revolution moving axis drives the sanding block rotation, the polishing BOB(beginning of block) polishing steamer Machine blade, when the sliding block is moved on rear side of the third cavity, the fifth metal contact and the 7th hard contact Cooperation, third electromagnet introspection are powered, and the third permanent magnetism iron slider slides to the right, the tenth gear and described the Six gears and the 7th gear are detached from cooperation, and the gear set is engaged with the 6th gear and the 7th gear, The sliding block is mobile to end wall on front side of the third cavity, when the motivation body slide into it is described determine fuselage right side when, described the Two hard contacts and the 4th hard contact cooperate, and first electromagnet is powered, the first permanent magnetism iron slider upward sliding, institute It states the first permanent magnetism iron slider and drives the sanding block upward sliding, second electromagnet is powered, the second permanent magnetism iron slider Slideslip to the left, the third gear and the second gear, which are detached from, to be cooperated, and the eighth gear is engaged with the 9th gear, The second bevel gear drives the third belt wheel rotation, and the third belt wheel drives the 4th belt wheel to rotate, and the described 4th Belt wheel drives the 9th gear rotation, and the 9th gear drives the eighth gear rotation, and the eighth gear drives institute The 4th gear to be stated to rotate backward, the 4th gear drives the motivation body to determine end wall quick sliding on the left of fuselage to described, when When 6th hard contact and the 8th hard contact cooperate, the third electromagnet power-off, the sliding block stops movement, When first hard contact and the third hard contact cooperate, the motor stops working, and second electromagnet is disconnected Electricity, the first electromagnet power-off, the equipment return to original state.

Device structure of the invention is simple, and using electrical energy drive mechanical structure, it is automatic right as needed to realize the equipment Blade is polished, and to blade carry out the polishing of homogeneous constant depth, save blade processing, while save the time and labour at This, guarantees the surface accuracy of blade, improves automation degree of equipment and practicability.

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 Vortex wheel turbine overall structure overlook open schematic diagram of the invention；

Fig. 2 is the structural schematic diagram of A-A in Fig. 1；

Fig. 3 is the structural schematic diagram of B-B in Fig. 2；

Fig. 4 is the structural schematic diagram of C-C in Fig. 2;

Specific embodiment

As Figure 1-Figure 4, a kind of high efficiency Vortex wheel turbine of the invention, including motivation body 11, determine fuselage 12 And the first cavity 101 in the motivation body 11 is set, the second cavity 102, institute are provided with below first cavity 101 It states and is provided with the first rotation axis 18 that left and right extends in the first cavity 101,18 left distal end of the first rotation axis is set with fixation The motor 13 set in the 101 left side end wall of the first cavity is connected by power, and 18 right end of the first rotation axis fixation is set It is equipped with first bevel gear 17, rotation is provided with second extended up and down between first cavity 101 and second cavity 102 Rotation axis 20,20 top end of the second rotation axis are fixedly installed the second bevel gear engaged with the first bevel gear 17 19,20 bottom end of the second rotation axis is provided with first gear 23, and rotation is provided with downward in second cavity 102 The third rotation axis 26 stretched, 26 top end of third rotation axis are provided with the first gear ring 25, first gear ring 25 and institute It states and has been engaged first planetary gear 24 between first gear 23,26 bottom end of third rotation axis is fixedly installed Two gears 27, the interior rotation of second cavity 102 are provided with the 4th rotation axis 32 extended up and down, the 4th rotation axis 32 top Portion end is fixedly installed the third gear 30 engaged with the second gear 27, and 32 bottom end of the 4th rotation axis is fixed 4th gear 31 is set, and rotation is provided with the 5th rotation axis 14 extended up and down, the 5th rotation in first cavity 101 14 bottom end of axis is fixedly installed the third hand tap gear 16 engaged with the first bevel gear 17, outside the 5th rotation axis 14 Surface is fixedly installed the first pulley 15 above the third hand tap gear 16, rotation setting in first cavity 101 There is the 6th rotation axis 40 extended up and down, 40 top end of the 6th rotation axis is fixedly installed the second belt wheel 39, and described Transmission is provided with the first belt 41 between two belt wheels 39 and the first pulley 15, and the is provided with below first cavity 101 Three cavitys 103, setting sliding block 22 capable of sliding back and forth in the third cavity 103 are provided with the 4th cavity in the sliding block 22 105,40 outer surface of the 6th rotation axis in the 4th cavity 105 is fixedly installed the 5th gear 64, the 6th rotation axis The rotation of 40 outer surfaces is provided with the 7th rotation axis 67 extended up and down, and 67 bottom end of the 7th rotation axis is fixedly installed the Two gear rings 66, have been engaged the second planetary gear 65 between second gear ring 66 and the 5th gear 64, and the described 7th 67 top end of rotation axis is fixedly installed the 6th gear 55, and rotation is provided with the extended up and down in the 4th cavity 105 Seven rotation axis 42,42 top end of the 7th rotation axis are fixedly installed the 7th gear 43,42 bottom of the 7th rotation axis End is fixedly installed the 4th bevel gear 45, and rotation is provided with the eight revolution moving axis 47 that left and right extends in the 4th cavity 105, The eight revolution moving axis 47 passes through spline engagement, 47 outer surface of the eight revolution moving axis fixed setting with its described rotation axis 42 There is the 5th bevel gear 46 engaged with the 4th bevel gear 45,47 or so the end symmetrical of eight revolution moving axis is provided with the first walking Wheel 48,22 front side end of sliding block is provided with and 48 symmetrical structure of the first traveling wheel, 40 bottom of the 6th rotation axis End is provided with the first groove 106, and eight revolution moving axis 52, the eight revolution are slidably provided in first groove 106 52 top end of moving axis is fixedly installed the first permanent magnetism iron slider 73, the first permanent magnetism iron slider 73 and first groove Elasticity is provided with the first spring 53 between 106, is fixedly installed the first electromagnet 54 in 106 top end wall of the first groove, 52 bottom end of eight revolution moving axis is fixedly installed link block 49, is provided with sanding block below the link block 49 51, elasticity is provided with second spring 50 between the link block 49 and the sanding block 51, the equipment be provided with emergency stop device its Including scram button 203, the 5th spring 204 and the 9th hard contact 202 and the tenth hard contact 201.

Valuably, 20 outer surface of the second rotation axis is fixedly installed third belt wheel 21, outside the 4th rotation axis 32 Surface is fixedly installed the eighth gear 34 positioned at 30 lower section of third gear, in second cavity 102 in rotation setting Lower extension has the 9th rotation axis 36, and 36 top end of the 9th rotation axis is fixedly installed the 4th belt wheel 37, and the described 4th Transmission is provided with the second belt 38 between belt wheel 37 and the third belt wheel 21, and 36 bottom end of the 9th rotation axis fixation is set It is equipped with the 9th gear 35 for being detached from cooperation with the eighth gear 34, is provided with the first sliding cavity below second cavity 102 107, the second permanent magnetism iron slider 33, the second permanent magnetism iron slider 33 and described first are provided in first sliding cavity 107 Third spring 29 is arranged in elasticity between 107 right side end wall of sliding cavity, is fixedly installed in the 107 right side end wall of the first sliding cavity Second electromagnet 28 is conducive to control the motivation body 11 and quickly slide to the left, returns to initial position.

Valuably, described to determine to be provided with the second sliding groove 108 in fuselage 12, turn on the 102 rear side end wall of the second cavity Dynamic the second traveling wheel 56 being provided with second sliding groove 108 cooperation, it is described to determine to be provided with the first sliding groove in fuselage 12 104, first rack gear engaged with the 4th gear 31 is fixedly installed in the 104 rear side end wall of the first sliding groove 63, be conducive to support and mobile motivation body 11.

Valuably, third sliding groove 109, the third sliding groove 109 are provided in the 103 left side end wall of third cavity Inside be provided with third sliding block 57, rotation is provided with the 5th belt wheel 56 on the third sliding block 57, the third sliding block 57 with it is described Elasticity is provided with the 4th spring 74 between third sliding groove 109, is conducive to during second belt wheel 39 slides back and forth, first Belt 41 cooperates with the first pulley 15 and the transmission of the second belt wheel 39 always.

Valuably, the 4th sliding groove 110, the 4th sliding groove 110 are provided in the 105 left side end wall of the 4th cavity It is inside provided with the second permanent magnetism iron slider 60 that left and right extends, 60 right end of the second permanent magnetism iron slider rotation is provided with and institute It states the 6th gear 55 and the 7th gear 43 is detached from the tenth gear 59 of cooperation, turn on the left of the third permanent magnetism iron slider 60 Dynamic to be provided with the gear set 44 that cooperation is detached from the 6th gear 55 and the 7th gear 43, the third permanent magnet is sliding Elasticity is provided with the 4th spring 61, the 4th sliding between 110 left side end wall of 60 left distal end of block and the 4th sliding groove It is fixedly installed third electromagnet 62 in 110 left side end wall of slot, is conducive to control the sliding block 22 and slides back and forth.

Valuably, the first hard contact 75, second cavity are fixedly installed on the 102 left side end wall of the second cavity Be fixedly installed the second hard contact 77 on 102 right side end walls, it is described determine to be fixedly installed on 12 left side end wall of fuselage with it is described The third hard contact 76 of first hard contact 75 cooperation, it is described to determine to be fixedly installed and described second on 12 right side end wall of fuselage Hard contact 77 is detached from the 4th hard contact 78 of cooperation, is fixedly installed fifth metal contact on the 22 rear side end wall of sliding block 70, it is fixedly installed the 6th hard contact 72 on the 22 front side end wall of sliding block, it is fixed on the 103 rear side end wall of third cavity It is provided with the 7th hard contact 71 with the fifth metal contact 70 cooperation, is fixed on the 103 front side end wall of third cavity It is provided with the 8th hard contact 79 for being detached from cooperation with the 6th hard contact 72, is conducive to control first electromagnet 54, the second electromagnet 28 and third electromagnet 62 are powered and power off, and are conducive to control 13 working condition of motor.

Valuably, described to determine to be provided with the second groove 205 in 12 left side end wall of fuselage, sliding in second groove 205 It is provided with scram button 203, elasticity is provided with the 5th between 205 right side end wall of the scram button 203 and second groove Spring 204, is fixedly installed the 9th hard contact 202 on the scram button 203, in the 205 right side end wall of the second groove It is provided with the tenth hard contact 201 with the 9th hard contact 202 cooperation, is conducive to the equipment when an emergency happens Emergent stopping work, and prevent emergency stop device accidentally touch, improve the safety of the equipment.

In the initial state, the motivation body 11 determines 12 left side of fuselage, first gold medal positioned at described to equipment of the invention Belong to contact 75 and the third hard contact 76 to cooperate, second electromagnet 28 is not powered on, the third gear 30 with it is described Second gear 27 engages, and the sliding block 22 is located at 103 front side of third cavity, the 6th hard contact 72 and the described 8th Hard contact 79 cooperates, and first electromagnet 54 is not powered on, and the third electromagnet 62 is not powered on, the tenth gear 59 with And the gear set 44 is detached from the 6th gear 55 and the 7th gear 43 and cooperates.

When using equipment polishing blade of the invention, the third electromagnet 62 is positive to be powered, the third electromagnet Sliding block 60 slides to the left drives the tenth gear 59 to slide to the left, the tenth gear 59 and the 6th gear 55 and 7th gear 43 engagement, the motor 13 are started to work, and the motor 13 drives first rotation axis 18 to rotate, described First rotation axis 18 drives the first bevel gear 17 to rotate, and the first bevel gear 17 drives 19 turns of the second bevel gear Dynamic, the second bevel gear 19 drives first gear 23 to rotate, and the first gear 23 drives 24 turns of the first planetary gear Dynamic, the first planetary gear 24 drives first gear ring 25 to rotate, and first gear ring 25 drives the second gear 27 Rotation, the second gear 27 drive the third gear 30 to rotate, and the third gear 30 drives described 31 turns of 4th gear Dynamic, Slideslip, the first bevel gear 17 drive the third hand tap gear 16 to rotate to the motivation body 11 to the right, the third cone Gear 16 drives the first pulley 15 to rotate, and the first pulley 15 drives the third belt wheel 39 to rotate, the third band Wheel 39 drives the 6th rotation axis 40 rotation, and the 6th rotation axis 40 drives the 5th gear 64 to rotate, and the described 5th Gear 64 drives second planetary gear 65 to rotate, and second planetary gear 65 drives second gear ring 66 to rotate, institute It states the second gear ring 66 and drives the rotation of the 6th gear 55, the 6th gear drives the tenth gear 59 rotation, the tenth tooth Wheel 59 drives the 7th gear 43 engagement, and the 7th gear 43 drives the 4th bevel gear 45 to rotate, the 4th cone Gear 45 drives the 5th bevel gear 46 to rotate, and the 5th bevel gear 46 drives first traveling wheel 48 to rotate, described Sliding block 22 moves backward, and the 6th rotation axis 40 drives the eight revolution moving axis 52 to rotate, and the eight revolution moving axis 52 drives The sanding block 51 rotates, and the sanding block 51 starts turbine blade of polishing, when the sliding block 22 is moved to the third sky When 103 rear side of chamber, the fifth metal contact 70 cooperates with the 7th hard contact 71, and the introspection of third electromagnet 62 is logical Electricity, the third permanent magnetism iron slider 60 Slideslip to the right, the tenth gear 59 and the 6th gear 55 and the described 7th Gear 43 is detached from cooperation, and the gear set 44 is engaged with the 6th gear 55 and the 7th gear 43, the sliding block 22 It is mobile to the 103 front side end wall of third cavity, when the motivation body 11 slide into it is described determine 12 right side of fuselage when, described second Hard contact 77 and the 4th hard contact 78 cooperate, and first electromagnet 54 is powered, and the first permanent magnetism iron slider 73 is upwards Sliding, the first permanent magnetism iron slider 73 drive 51 upward sliding of sanding block, and second electromagnet 28 is powered, and described the Slideslip, the third gear 30 are detached from cooperation, the eighth gear with the second gear 27 to two permanent magnetism iron sliders 33 to the left 34 engage with the 9th gear 35, and the second bevel gear 19 drives the third belt wheel 21 to rotate, the third belt wheel 21 The 4th belt wheel 37 is driven to rotate, the 4th belt wheel 37 drives the 9th gear 35 to rotate, 35 band of the 9th gear It moves the eighth gear 34 to rotate, the eighth gear 34 drives the 4th gear 13 to rotate backward, the 4th gear 13 The motivation body 11 is driven to determine 12 left side end wall quick sliding of fuselage to described, when the 6th hard contact 72 and the described 8th When hard contact 79 cooperates, the third electromagnet 62 is powered off, and the sliding block 22 stops movement, when first hard contact 75 When cooperating with the third hard contact 76, the motor 13 stops working, and second electromagnet 28 powers off, first electricity Magnet 54 powers off, which returns to original state.

The beneficial effects of the present invention are: equipment of the invention is in the initial state, the motivation body determines fuselage positioned at described Left side, first hard contact and the third hard contact cooperate, and second electromagnet is not powered on, the third gear It is engaged with the second gear, the sliding block is located on front side of the third cavity, the 6th hard contact and the 8th gold medal Belong to contact cooperation, first electromagnet is not powered on, and the third electromagnet is not powered on, the tenth gear and the gear Group, which is detached from the 6th gear and the 7th gear, to be cooperated.

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

1. a kind of high efficiency Vortex wheel turbine of the invention, including motivation body, determines fuselage and be arranged in the motivation body The first interior cavity, it is characterised in that: be provided with the second cavity below first cavity, be provided with a left side in first cavity First rotation axis of right extension, the first rotation axis left distal end and is fixed on the left of first cavity in end wall Motor power connection, the first rotation axis right end are fixedly installed first bevel gear, first cavity and described the Rotation is provided with the second rotation axis extended up and down between two cavitys, and the second rotation axis top end is fixedly installed and institute The second bevel gear of first bevel gear engagement is stated, the second rotation axis bottom end is provided with first gear, and described second is empty Intracavitary rotation is provided with the third rotation axis extended up and down, and the third rotation axis top end is provided with the first gear ring, described First planetary gear is engaged between first gear ring and the first gear, the third rotation axis bottom end fixation is set It is equipped with second gear, rotation is provided with the 4th rotation axis extended up and down, the 4th rotation axis top in second cavity End is fixedly installed the third gear engaged with the second gear, the 4th rotation axis bottom end fixed setting the 4th Gear, the interior rotation of first cavity are provided with the 5th rotation axis extended up and down, and the 5th rotation axis bottom end is fixed It is provided with the third hand tap gear engaged with the first bevel gear, the 5th rotation axis outer surface is fixedly installed positioned at described First pulley above third hand tap gear, rotation is provided with the 6th rotation axis extended up and down in first cavity, and described the Six rotation axis top ends are fixedly installed the second belt wheel, and transmission is provided with the between second belt wheel and the first pulley One belt, the first cavity lower section are provided with third cavity, and setting sliding block capable of sliding back and forth in the third cavity is described The 4th cavity is provided in sliding block, the 6th rotation axis outer surface in the 4th cavity is fixedly installed the 5th gear, described The rotation of 6th rotation axis outer surface is provided with the 7th rotation axis extended up and down, the 7th rotation axis bottom end fixed setting There is the second gear ring, the second planetary gear, the 7th rotation have been engaged between second gear ring and the 5th gear Axis top end is fixedly installed the 6th gear, and rotation is provided with the 7th rotation axis extended up and down, institute in the 4th cavity It states the 7th rotation axis top end and is fixedly installed the 7th gear, the 7th rotation axis bottom end is fixedly installed the 4th cone Gear, the interior rotation of the 4th cavity are provided with the eight revolution moving axis that left and right extends, the eight revolution moving axis and its described turn Moving axis is fixedly installed the 5th bevel gear engaged with the 4th bevel gear by spline engagement, the eight revolution moving axis outer surface, The eight revolution moving axis or so end symmetrical is provided with the first traveling wheel, and the sliding block front side end is provided with and the first row It walks and takes turns symmetrical structure, the 6th rotation axis bottom end is provided with the first groove, is slidably arranged in first groove There is eight revolution moving axis, the eight revolution moving axis top end is fixedly installed the first permanent magnetism iron slider, and first permanent magnet is sliding Elasticity is provided with the first spring between block and first groove, and the first electricity is fixedly installed in the first groove top end wall Magnet, the eight revolution moving axis bottom end are fixedly installed link block, are provided with sanding block below the link block, institute State elasticity between link block and the sanding block and be provided with second spring, the equipment be provided with emergency stop device it include emergency stop by Button, the 5th spring and the 9th hard contact and the tenth hard contact.

2. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: outside second rotation axis Surface is fixedly installed third belt wheel, and the 4th rotation axis outer surface is fixedly installed below the third gear Octadentate wheel, what the interior rotation setting of second cavity extended up and down has the 9th rotation axis, and the 9th rotation axis top end is consolidated Surely it is provided with the 4th belt wheel, is driven between the 4th belt wheel and the third belt wheel and is provided with the second belt, described 9th turn Moving axis bottom end is fixedly installed the 9th gear that cooperation is detached from the eighth gear, is provided with below second cavity First sliding cavity is provided with the second permanent magnetism iron slider, the second permanent magnetism iron slider and described first in first sliding cavity Third spring is arranged in elasticity between end wall on the right side of sliding cavity, is fixedly installed the second electromagnetism in end wall on the right side of first sliding cavity Iron is conducive to control the motivation body and quickly slide to the left, returns to initial position.

3. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: described to determine setting in fuselage There is the second sliding groove, rotation is provided with the second walking with second sliding groove cooperation on end wall on rear side of second cavity Wheel, it is described to determine to be provided with the first sliding groove in fuselage, it is fixedly installed and the described 4th in end wall on rear side of first sliding groove First rack gear of gear engagement is conducive to support and mobile motivation body.

4. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: on the left of the third cavity It is provided with third sliding groove in end wall, third sliding block is provided in the third sliding groove, rotates setting on the third sliding block There is the 5th belt wheel, elasticity is provided with the 4th spring between the third sliding block and the third sliding groove, is conducive to described second During belt wheel slides back and forth, the first belt cooperates with the first pulley and the second belt wheel transmission always.

5. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: on the left of the 4th cavity It is provided with the 4th sliding groove in end wall, is provided with the second permanent magnetism iron slider that left and right extends in the 4th sliding groove, described the The rotation of two permanent magnetism iron slider right ends is provided with the tenth tooth that cooperation is detached from the 6th gear and the 7th gear Wheel, the third permanent magnetism iron slider left pivot movement are provided with the tooth that cooperation is detached from the 6th gear and the 7th gear Elasticity is provided with the 4th bullet between end wall on the left of wheel group, the third permanent magnetism iron slider left distal end and the 4th sliding groove Spring is fixedly installed third electromagnet in end wall on the left of the 4th sliding groove, is conducive to control the sliding block and slides back and forth.

6. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: on the left of second cavity It is fixedly installed the first hard contact on end wall, is fixedly installed the second hard contact, institute on end wall on the right side of second cavity It states and determines to be fixedly installed the third hard contact with first hard contact cooperation on end wall on the left of fuselage, it is described to determine the fuselage right side The 4th hard contact that cooperation is detached from second hard contact is fixedly installed on the wall of side, on rear side of the sliding block on end wall It is fixedly installed fifth metal contact, is fixedly installed the 6th hard contact, the third cavity on end wall on front side of the sliding block The 7th hard contact with fifth metal contact cooperation, end wall on front side of the third cavity are fixedly installed on rear side end wall On be fixedly installed with the 6th hard contact be detached from cooperation the 8th hard contact, be conducive to control first electromagnetism Iron, the second electromagnet and third electromagnet are powered and power-off, is conducive to control the electric machine operation state.

7. a kind of high efficiency Vortex wheel turbine according to claim 1, it is characterised in that: described to determine fuselage left-hand end It is provided with the second groove in wall, sliding is provided with scram button in second groove, the scram button and described second recessed Elasticity is provided with the 5th spring between end wall on the right side of slot, is fixedly installed the 9th hard contact on the scram button, and described the The tenth hard contact with the 9th hard contact cooperation is provided on the right side of two grooves in end wall, is had when an emergency happens It works conducive to the emergent stopping of the equipment, and prevents emergency stop device and accidentally touch, improve the safety of the equipment.