CN103107681B - Cam type straight wing suspended magnetic eddy-current coupling - Google Patents
Cam type straight wing suspended magnetic eddy-current coupling Download PDFInfo
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- CN103107681B CN103107681B CN201310013056.6A CN201310013056A CN103107681B CN 103107681 B CN103107681 B CN 103107681B CN 201310013056 A CN201310013056 A CN 201310013056A CN 103107681 B CN103107681 B CN 103107681B
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Abstract
The invention relates to a cam type straight wing suspended magnetic eddy-current coupling. The cam type straight wing suspended magnetic eddy-current coupling comprises a left conductor plate, a left magnetic plate, a middle plate, a right magnetic plate and a right conductor plate, wherein the left conductor plate, the left magnetic plate, the middle plate, the right magnetic plate and the right conductor plate are parallelly arranged. Vanes are arranged between the left conductor plate and the right conductor plate, wherein the vanes are arranged along the circumference. Vane shafts are connected with the left conductor plate and the right conductor plate in a rotatable mode and are fixedly connected with a rotary rod after being stretched from the left conductor plate, wherein the rotary rod is perpendicular to the vanes. The upper end of the rotary rod is connected with a third sliding block which slides inside a cam groove of a cam plate. The cam plate is sleeved on an input shaft in a rotatable mode. The center of the cam groove deviates from the input shaft. The vanes simulate work of vanes of a straight wing thruster under the limit of the cam groove. The invention provides the cam type straight wing suspended magnetic eddy-current coupling which can use self-rotation to produce vane lifting force of certain size and direction to balance the gravity of the coupling. All control mechanisms of the coupling are mechanical structures, and the cam type straight wing suspended magnetic eddy-current coupling is simple and reliable in control and is suitable for a large-scale or super large-scale magnetic eddy-current coupling.
Description
Technical field
The present invention relates to a kind of magnetic eddy-current coupling.
Background technology
In actual life, use the transmission shaft driven system application of shaft coupling connection widely, almost relate to the field of motor power transmission in industrial occasions and life, all can use the transmission shaft driven technology of shaft coupling.The shaft coupling used in current mechanical field mostly is mechanical coupling and hydraulic type shaft coupling.Mechanical coupling is rigid connection, mechanical force transmitting torque, in installation process, owing to there is axial dipole field error, the load supporting original paper can be increased, and radial offset error causes the dither of equipment by producing sudden change load, in addition, rigid connection also can produce impact load instantaneously in startup.Fluid coupling speed governing belongs to poor efficiency mode of speed regulation, speed adjustable range is limited, and throw switch at a high speed about 5%-10%, and low speed slip loss is large, reach as high as more than 30% of rated power, precision is low, poor linearity, low-response, and starting current is large, and device is large, be not suitable for transformation, and easy leakage, maintenance complexity, expense greatly, can not meet the needs improving device integrated automation level.
Magnetic couple shaft coupling using magnetic force coupled drive technology, also claim magnetic eddy-current coupling, the shaft coupling of transmission of comparing, has following advantage: 1. energy-saving effect: 25% ~ 66%; 2. maintenance workload is little, and be almost non-maintaining product, maintenance cost is extremely low; 3. allow the larger installation error of centralization (maximum can be 5mm), enormously simplify Installation and Debugging process; 4. there is overload protection function, thus improve the reliability of whole system, the damage that the system that completely eliminates causes because of overload; 5. improve the startup ability of motor, reduce shock and vibration, coordinate the sharing of load that multimachine drives; 6. speed-regulating type can realize the stepless of output speed when motor speed is substantially constant; 7. long service life, designed life is 30 years, and can useful life of parts in prolongation system; 8. be easy to realize remote control and automatically control, process control is accurately high; 9. structure is simple, and adapt to various adverse circumstances, environmentally friendly, do not produce pollutant, do not produce harmonic wave, volume is little, easy for installation.
But the large-scale and ultra-large type magnetic couple coupling product of technology maturation in the market, due to the limitation by this body structure of product and technical scheme, still there is some technical disadvantages and deficiency in the technical performance of product own, mainly contain: 1. depth of parallelism problem, in order to transmit large torque, gap between conductor disc and disk many times only has several millimeter, the torque of transmitting is larger, gap needs less, for large-scale and ultra-large type magnetic eddy-current coupling, due to conductor disc and disk diameter very large, now slightly not parallel, will collide between them, thus cause damage, 2. heat dissipation problem, Nd-Fe-Bo permanent magnet material is the preferred material of permanent magnet, but the ability to work of NdFeB material is very high to the requirement of temperature, temperature is one of main factor affecting NdFeB material operating efficiency, even can completely lose ability to work when temperature is more than 85 degree.
Summary of the invention
In order to solve the problems referred to above that existing magnetic eddy-current coupling exists, the invention provides a kind ofly carry air-gap separation governor motion, structure simple, stable and reliable for performance, that conveniently can realize output shaft in operating mode process speed change require, adjusting speed accuracy is high, Action of Gravity Field can be solved under the cam type straight wing suspension magnetic eddy-current coupling of depth of parallelism shortcoming problem.
The present invention adopts following technical scheme:
Cam type straight wing suspension magnetic eddy-current coupling, comprise the power shaft be connected with the first motor, the output shaft be connected with load, on described power shaft, fixed cover is equipped with left conductor disc, described cam type straight wing suspension magnetic eddy-current coupling also comprises the right conductor disc with left conductor disc synchronous axial system, left disk and right disk is provided with between described left conductor disc and right conductor disc, the telophragma be fixedly connected with output shaft is furnished with between left disk and right disk, left conductor disc, left disk, telophragma, right disk, right conductor disc is arranged in parallel, described left disk, telophragma, right disk synchronous axial system, blade circumferentially is also connected with between described left conductor disc and right conductor disc, the sharf of described blade is rotating to be connected in left conductor disc and right conductor disc, sharf is fixedly connected with the dwang of perpendicular layout after stretching out in left conductor disc, the upper end of described dwang connects the 3rd slide block, 3rd slide block slides in the cam path of a cam disc, this cam disc is contained on power shaft by the 3rd bearing holder (housing, cover), cam disc is fixed by fixed mechanism, the misalignment power shaft of cam path, blade is at the blade working of the restriction Imitating voith schneider propeller of cam path, described cam type straight wing suspension magnetic eddy-current coupling also comprises air-gap separation between adjustable left conductor disc and left disk, and the air-gap separation governor motion of air-gap separation between right conductor disc and right disk.Preferably, the center of circle of described cam path and power shaft are on same vertical curve.The concrete shape of cam path and position are by shaft coupling weight, and in corresponding situation, voith schneider propeller blade oscillating rule is determined.
Further, described air-gap separation governor motion comprises inner sleeve, outer sleeve, described outer sleeve connects right disk by the clutch shaft bearing of transmitting thrust, inner sleeve is sleeved on output shaft by the second bearing is rotating, inner sleeve is provided with oblique chute, outer sleeve is provided with the first slide block coordinated with oblique chute, outer sleeve is also provided with outer sleeve can be made to rotate the handle advanced, described air-gap separation governor motion also comprises the locating part of restriction inner sleeve movement, the transmission mechanism that can make left disk and right disk synchronous on-off is provided with between described left disk and right disk.Preferably, described clutch shaft bearing is double-row conical bearing, this double-row conical bearing can transmitting thrust, do not transmit rotation, therefore, when sleeve rotating advances outside, outer sleeve can pull right disk to move axially, can not drive right disc rotation (due to the existence of double-row conical bearing between outer sleeve and right disk, therebetween not transmitting torque).Described second bearing is cylinder roller bearing, and this cylinder roller bearing not transmitting thrust does not also transmit rotation.
Further, described transmission mechanism comprise be vertically fixed on telophragma outer rim slide bar, be slidably sleeved on the second slide block on slide bar, the hinged left connecting rod in left side of described second slide block, the hinged right connecting rod in right side of the second slide block, described left connecting rod and left disk hinged, right connecting rod and right disk hinged.
Preferably, the center of circle of described cam path and the intersection point of power shaft and cam disc are on same vertical curve.
Further, be provided with between described left disk and right disk prevent the magnetic field of left disk and right disk from mutually disturbing every magnetic part.
Further, described left conductor disc is provided with radiator away from the side of left disk, and described right conductor disc is provided with radiator away from the side of right disk.
Preferably, be provided with the transmission mechanism described in three groups between described left disk and right disk, three groups of transmission mechanisms are circumferentially arranged at equal intervals.
Preferably, described oblique chute is helix.
Technical conceive of the present invention is: the power shaft (speed end) of cam type straight wing suspension magnetic eddy-current coupling connects the first motor, and the output shaft (low speed end) of cam type straight wing suspension magnetic eddy-current coupling connects load.After the first electric motor starting, regulate air-gap separation and the air-gap separation between right disk and right conductor disc between left disk and left conductor disc by air-gap separation governor motion, and then the transmitted power of this shaft coupling can be adjusted, and then adjustment output shaft rotating speed.
The transmission process of air-gap separation governor motion is: the handle on rotary sleeve cylinder, the first slide block on outer sleeve slides on the oblique chute of inner sleeve, because inner sleeve limited restriction cannot move axially, therefore handle drives the compound motion that outer sleeve rotates and moves axially, be connected by double-row roller bearing between outer sleeve with right disk, this double-row roller bearing transmitting thrust does not transmit rotation, therefore when sleeve rotating advances outside, outer sleeve can pull right disk to move axially, right disc rotation can not be driven (due to the existence of double-row conical bearing between outer sleeve and right disk, therebetween not transmitting torque).Right disk drives the second slide block to move on slide bar by right connecting rod, and the second slide block drives left disk to move towards the direction relative with right disk by left connecting rod again.When left disk and right disk outwards move, air-gap separation between left disk and left conductor disc reduces, air-gap separation between right disk and right conductor disc reduces, left conductor disc increases the transmitting torque of left disk, right conductor disc increases the transmitting torque of right disk, left and right disk running speed improves, and output shaft rotating speed improves; When left disk and right disk inwardly move, air-gap separation between left disk and left conductor disc increases, air-gap separation between right disk and right conductor disc increases, left conductor disc reduces the transmitting torque of left disk, right conductor disc reduces the transmitting torque of right disk, left and right disk running speed reduces, and output shaft rotating speed reduces.Like this, by the air-gap separation between left disk and left conductor disc and the air-gap separation between right disk and right conductor disc, the speed discrepancy between power shaft and output shaft just can be adjusted.
3rd slide block slides in cam path, sharf is rotating around power shaft, due to the misalignment power shaft of cam path, like this, 3rd slide block can drive sharf rotation by dwang, so, blade is while rotating (revolution) around power shaft, also can drive rotation (elevating movement) by the 3rd slide block, this rotation makes attack angle of blade free change, general excursion-30 ° is to 30 °, in running, blade movement rule meets the operation principle of voith schneider propeller, thus produce the satisfactory blade lift of size and Orientation, here size is produced suitable with shaft coupling weight, direction power straight up.The size and Orientation of making a concerted effort that the track of cam path produces according to required blade rotation and given, once the track of cam path is given, in motion process, the size and Orientation of making a concerted effort no longer changes.When design, the weight of shaft coupling to be known in advance, according to the track of this weight configuration cam path, to make the gravity making a concerted effort to balance shaft coupling of blade rotation.Thus, can eliminate due to the moment of flexure that each parts gravity produces on power shaft and output shaft, increase the useful life of cam type straight wing suspension magnetic eddy-current coupling.
The athletic meeting of blade improves the wind speed of interior flow field greatly, obviously improve heat-sinking capability, this is very favorable to the work of Ru-Fe-Mn permanent magnetic material, because the ability to work of Ru-Fe-Mn material is very high to the requirement of temperature, temperature is one of main factor affecting Ru-Fe-Mn material operating efficiency, even can completely lose ability to work when temperature is more than 85 degree.
The buoyancy that blade between left and right conductor disc produces counteracts gravity, power shaft and output shaft are no longer subject to the impact of moment of flexure, also no longer mutually tilt because of gravity between conductor disc and disk and even collide, thus large-scale and ultra-large type magnetic eddy-current coupling disk depth of parallelism problem under gravity, the sag problem of axle can be solved, add the useful life of shaft coupling.
Beneficial effect of the present invention is: (1) carries air-gap separation governor motion, and structure is simple, and stable and reliable for performance, conveniently can realize the speed change requirement of output shaft in operating mode process, adjusting speed accuracy is high; (2) large-scale and ultra-large type magnetic eddy-current coupling disk depth of parallelism problem under gravity, the sag problem of axle, permanent magnetic material heat dissipation problem can be solved; (3) blade movement is controlled by pure mechanical structure, controls simple and reliable and saves energy.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention.
Fig. 2 is that the embodiment of the present invention regulates the schematic diagram of left disk and right disk spacing by handle.
Fig. 3 is the cutaway view of the cam disc of the embodiment of the present invention.
Fig. 4 is the schematic diagram of voith schneider propeller.
Drawing reference numeral: 1-power shaft; 2-output shaft; The left conductor disc of 31-; The right conductor disc of 32-; The left disk of 34-; The right disk of 35-; 36-telophragma; 37-connecting rod; 38-permanent magnet; 39-radiator; 41-inner sleeve; 42-outer sleeve; The oblique chute of 43-; 44-first slide block; 45-handle; 46-clutch shaft bearing; 47-second bearing; 48-thrust bush; 51-slide bar; 52-second slide block; The left connecting rod of 53-; 54-right connecting rod; 61-blade; 62-sharf; 63-cam disc; 64-cam path; 65-the 3rd slide block; 66-dwang.
Embodiment
Below in conjunction with accompanying drawing, the invention will be further described.
With reference to Fig. 1-4: cam type straight wing suspension magnetic eddy-current coupling, comprise the power shaft 1 be connected with the first motor, the output shaft 2 be connected with load, on described power shaft 1, fixed cover is equipped with left conductor disc 31, described cam type straight wing suspension magnetic eddy-current coupling also comprises the right conductor disc 32 by connector and left conductor disc 31 synchronous axial system, in the present embodiment, this connector is many steel plates, left disk 34 and right disk 35 is provided with between described left conductor disc 31 and right conductor disc 32, the telophragma 36 be fixedly connected with output shaft 2 is furnished with between left disk 34 and right disk 35, left conductor disc 31, left disk 34, telophragma 36, right disk 35, right conductor disc 32 is arranged in parallel, described left disk 34, telophragma 36, right disk 35 synchronous axial system, blade 61 circumferentially is also connected with between described left conductor disc 31 and right conductor disc 32, the sharf 62 of described blade 61 is rotating to be connected in left conductor disc 31 and right conductor disc 32, sharf 62 is fixedly connected with the dwang 66 of perpendicular layout after stretching out in left conductor disc 31, the upper end of described dwang 66 connects the 3rd slide block 65, 3rd slide block 65 slides in the cam path 64 of a cam disc 63, this cam disc 63 is contained on power shaft 1 by the 3rd bearing holder (housing, cover), cam disc 63 is fixed by fixed mechanism, the misalignment power shaft 1 of cam path 64, blade 61 is at the blade working of the restriction Imitating voith schneider propeller of cam path 64, in the present embodiment, the center of circle of described cam path 64 and the intersection point of power shaft 1 and cam disc 63 are on same vertical curve, the center of circle of cam path 64 is positioned at the top of power shaft 1, described cam type straight wing suspension magnetic eddy-current coupling also comprises air-gap separation between adjustable left conductor disc 31 and left disk 34, and the air-gap separation governor motion of air-gap separation between right conductor disc 32 and right disk 35.In the present embodiment, the 3rd slide block 65 can drive sharf 62 that rotation occurs by dwang 66, and the 3rd slide block 65 is fixedly connected with between dwang 66.The concrete shape of cam path and position are by shaft coupling weight, and in corresponding situation, voith schneider propeller blade oscillating rule is determined.
Described air-gap separation governor motion comprises inner sleeve 41, outer sleeve 42, described outer sleeve 42 connects thrust bush 48 by the clutch shaft bearing 46 of transmitting thrust, thrust bush 48 is fixedly connected with right disk 35, inner sleeve 41 is sleeved on output shaft 2 by the second bearing 47 is rotating, inner sleeve 41 is provided with oblique chute 43, this oblique chute 43 is a part for helix, outer sleeve 42 is provided with the first slide block 44 coordinated with oblique chute 43, outer sleeve 42 is also provided with outer sleeve 42 can be made to rotate the handle 45 advanced, described air-gap separation governor motion also comprises the locating part of restriction inner sleeve 41 movement, in the present embodiment, this locating part is snap ring.The transmission mechanism that can make left disk 34 and right disk 35 synchronous on-off is provided with between described left disk 34 and right disk 35.In the present embodiment, described clutch shaft bearing 46 is double-row conical bearing, this double-row conical bearing can transmitting thrust, do not transmit rotation, therefore, when outer sleeve 42 rotates advance (rotating and move axially the screw of compound), outer sleeve 42 can pull right disk 35 to move axially, right disk 35 can not be driven to rotate (due to the existence of double-row conical bearing between outer sleeve and right disk, therebetween not transmitting torque).Described second bearing 47 is cylinder roller bearing, and this cylinder roller bearing not transmitting thrust does not also transmit rotation.
Described transmission mechanism comprise be vertically fixed on telophragma 36 outer rim slide bar 51, be slidably sleeved on the second slide block 52 on slide bar 51, the hinged left connecting rod 53 in left side of described second slide block 52, the hinged right connecting rod 54 in right side of the second slide block 52, described left connecting rod 53 is hinged with left disk 34, and right connecting rod 54 is hinged with right disk 35.Be provided with the transmission mechanism described in three groups between described left disk 34 and right disk 35, three groups of transmission mechanisms are circumferentially arranged at equal intervals.
Connected by connecting rod 37 between described left disk 34, telophragma 36, right disk 35, connecting rod 37 drives left disk 34, telophragma 36, right disk 35 synchronous axial system.In the present embodiment, described connecting rod 37 has three, and three connecting rods 37 are circumferentially arranged at equal intervals, and connecting rod 37 and left disk 34, telophragma 36, right disk 35 are arranged vertically.
In the present embodiment, described left disk 34 and right disk 35 comprise metal dish, and metal dish pressed on ring is furnished with permanent magnet 38.Be provided with between left disk 34 and right disk 35 prevent the magnetic field of left disk and right disk from mutually disturbing every magnetic part, in the present embodiment, should every magnetic part be every magnetic copper coin.
Described left conductor disc 31 is provided with radiator 39 away from the side of left disk 34, and described right conductor disc 32 is provided with radiator 39 away from the side of right disk 35, and this radiator is mechanical type radiator, and radiator ring is located in left conductor disc 31 and right conductor disc 32.Because left disk 34 produces current vortex in left conductor disc 31, right disk 35 produces current vortex in right conductor disc 32, can reduce by radiator 39 high temperature that current vortex causes, and increases heat radiation.
The operation principle of the present embodiment is: the power shaft 1 (speed end) of cam type straight wing suspension magnetic eddy-current coupling connects the first motor, and the output shaft 2 (low speed end) of cam type straight wing suspension magnetic eddy-current coupling connects load.After the first electric motor starting, air-gap separation and the air-gap separation between right disk 35 and right conductor disc 32 between left disk 34 and left conductor disc 31 is regulated by air-gap separation governor motion, and then the transmitted power of this shaft coupling can be adjusted, and then the rotating speed of adjustment output shaft 2.Specific as follows:
Start the first motor, the power shaft 1 of cam type straight wing suspension magnetic eddy-current coupling and the synchronized rotation of the first motor, power shaft 1 drives left conductor disc 31 and right conductor disc 32 synchronous axial system; Left conductor disc 31 drives left disk 34 to rotate by current vortex, right conductor disc 32 drives right disk 35 to rotate by current vortex, when left disk 34 and left conductor disc 31 are distant with right conductor disc 32 apart from, right disk 35, the current vortex that the magnetic induction line that left disk 34 sends produces in left conductor disc 31 is little, the current vortex that the magnetic induction line that right disk 35 sends produces in right conductor disc 32 is little, thus the transmitting torque of left conductor disc 31 to left disk 34 is little, the transmitting torque of right conductor disc 32 to right disk 35 is little, causes left disk 34, right disk 35 rotating speed lower.Due to left and right disk and telophragma 36 synchronous axial system, telophragma 36 is fixedly connected with output shaft 2 again, and left and right disk running speed reduces just to be equivalent to output shaft 2 rotating speed and reduces.Otherwise, after distance between left disk 34 and left conductor disc 31, the distance between right disk 35 and right conductor disc 32 reduce, left conductor disc 31 improves the transmitting torque of left disk 34, right conductor disc 32 improves the transmitting torque of right disk 35, left and right disk running speed improves, and output shaft 2 rotating speed improves.
The transmission process of air-gap separation governor motion is: the handle 45 on rotary sleeve cylinder 42, the first slide block 44 on outer sleeve 42 slides on the oblique chute 43 of inner sleeve 41, this oblique chute 43 is a part for helix, and inner sleeve 41 limited restrictions cannot move axially, therefore handle 45 drives outer sleeve 42 to rotate and moves axially the screw of compound, be connected by double-row roller bearing between outer sleeve 42 with right disk 35, this double-row roller bearing transmitting thrust does not transmit rotation, when outer sleeve 42 rotates advance (rotating and move axially the screw of compound), outer sleeve 42 can pull right disk 35 to move axially, right disk 35 can not be driven to rotate (due to the existence of double-row conical bearing between outer sleeve and right disk, therebetween not transmitting torque).Right disk 35 drives the second slide block 52 to move on slide bar 51 by right connecting rod 54, and the second slide block 52 drives left disk 34 to move towards the direction relative with right disk 35 by left connecting rod 53 again.When left disk 34 outwards moves with right disk 35, air-gap separation between left disk 34 and left conductor disc 31 reduces, air-gap separation between right disk 35 and right conductor disc 32 reduces, left conductor disc 31 increases the transmitting torque of left disk 34, right conductor disc 32 increases the transmitting torque of right disk 35, left and right disk running speed improves, and output shaft 2 rotating speed improves; When left disk 34 inwardly moves with right disk 35, air-gap separation between left disk 34 and left conductor disc 31 increases, air-gap separation between right disk 35 and right conductor disc 32 increases, left conductor disc 31 reduces the transmitting torque of left disk 34, right conductor disc 32 reduces the transmitting torque of right disk 35, left and right disk running speed reduces, and output shaft 2 rotating speed reduces.Like this, by the air-gap separation between left disk 34 and left conductor disc 31 and the air-gap separation between right disk 35 and right conductor disc 32, the speed discrepancy between power shaft 1 and output shaft 2 can just be adjusted.
3rd slide block 65 slides in cam path 64, sharf 62 is rotating around power shaft 1, due to the misalignment power shaft 1 of cam path 64, like this, 3rd slide block 65 can drive sharf 62 rotation by dwang 66, so, blade 61 is while rotating (revolution) around power shaft 1, also can drive rotation (elevating movement) by the 3rd slide block 65, this rotation makes attack angle of blade change, thus the motion of blade 61 meets the blade movement rule of voith schneider propeller under the control of cam path.The size and Orientation of making a concerted effort that the track of cam path 64 produces according to required blade rotation and given, once the track of cam path is given, in motion process, the size and Orientation of making a concerted effort no longer changes.When design, the weight of shaft coupling to be known in advance, according to the track of this weight configuration cam path 64, to make the gravity making a concerted effort to balance shaft coupling of blade rotation.Thus, can eliminate due to the moment of flexure that each parts gravity produces on power shaft 1 and output shaft 2, increase the useful life of cam type straight wing suspension magnetic eddy-current coupling.In the present embodiment, vane airfoil profile is NACA aerofoil profile.
The principle of voith schneider propeller is described with reference to Fig. 4: Fig. 4 is the schematic diagram of individual blade when diverse location, sharf is by a left side, right conductor disc drives and revolves round the sun centered by power shaft, sharf is equivalent to the A point in Fig. 4, revolution center is O1, 3rd slide block rotates in the cam path that power shaft is departed from the center of circle, 3rd slide block is equivalent to the B point in Fig. 4, the center of cam path is 02, A, line AB between B is equivalent to dwang, as can be seen from the figure, in the process that A Dian Rao center O1 rotates and B Dian Rao center 02 is rotated, AB can rotate, this rotation is the rotation of dwang.In figure, this rotation is presented as the change of angle of attack a.By changing the track of cam path, the namely path of B, can change the size and Orientation of making a concerted effort of blade.
The athletic meeting of blade improves the wind speed of interior flow field greatly, obviously improve heat-sinking capability, this is very favorable to the work of Ru-Fe-Mn permanent magnetic material, because the ability to work of Ru-Fe-Mn material is very high to the requirement of temperature, temperature is one of main factor affecting Ru-Fe-Mn material operating efficiency, even can completely lose ability to work when temperature is more than 85 degree.
The buoyancy that blade between left and right conductor disc produces counteracts gravity, power shaft and output shaft are no longer subject to the impact of moment of flexure, also no longer mutually tilt because of gravity between conductor disc and disk and even collide, thus large-scale and ultra-large type magnetic eddy-current coupling disk depth of parallelism problem under gravity can be solved, the sag problem of axle adds the useful life of shaft coupling.
Above-described embodiment is only enumerating of the technology of the present invention design way of realization; protection scope of the present invention is not limited only to above-described embodiment, and protection scope of the present invention may extend to those skilled in the art according to the thinkable equivalent technologies means of technical conceive of the present invention.
Claims (10)
1. cam type straight wing suspension magnetic eddy-current coupling, this magnetic eddy-current coupling comprises the power shaft be connected with the first motor, the output shaft be connected with load, on described power shaft, fixed cover is equipped with left conductor disc, described cam type straight wing suspension magnetic eddy-current coupling also comprises the right conductor disc with left conductor disc synchronous axial system, left disk and right disk is provided with between described left conductor disc and right conductor disc, the telophragma be fixedly connected with output shaft is furnished with between left disk and right disk, left conductor disc, left disk, telophragma, right disk, right conductor disc is arranged in parallel, described left disk, telophragma, right disk synchronous axial system, it is characterized in that: between described left conductor disc and right conductor disc, be also connected with blade circumferentially, the sharf of described blade is rotating to be connected in left conductor disc and right conductor disc, sharf is fixedly connected with the dwang of perpendicular layout after stretching out in left conductor disc, the upper end of described dwang connects the 3rd slide block, 3rd slide block slides in the cam path of a cam disc, this cam disc is contained on power shaft by the 3rd bearing holder (housing, cover), cam disc is fixed by fixed mechanism, the misalignment power shaft of cam path, described blade has the NACA aerofoil profile of aerial blade, each blade has independently spinning motion rule, whole vane group cooperative motion produces heat radiation flow field and lift is made a concerted effort, the size and Orientation that the position of cam path and shape controlling lift are made a concerted effort.
2. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 1, it is characterized in that: described air-gap separation governor motion comprises inner sleeve, outer sleeve, described outer sleeve connects right disk by the clutch shaft bearing of transmitting thrust, inner sleeve is sleeved on output shaft by the second bearing is rotating, inner sleeve is provided with oblique chute, outer sleeve is provided with the first slide block coordinated with oblique chute, outer sleeve is also provided with outer sleeve can be made to rotate the handle advanced, described air-gap separation governor motion also comprises the locating part of restriction inner sleeve movement, the transmission mechanism that can make left disk and right disk synchronous on-off is provided with between described left disk and right disk.
3. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 2, it is characterized in that: described transmission mechanism comprise be vertically fixed on telophragma outer rim slide bar, be slidably sleeved on the second slide block on slide bar, the hinged left connecting rod in left side of described second slide block, the hinged right connecting rod in right side of the second slide block, described left connecting rod and left disk hinged, right connecting rod and right disk hinged.
4. the cam type straight wing suspension magnetic eddy-current coupling as described in one of claim 1-3, is characterized in that: the intersection point of the center of circle of described cam path and power shaft and cam disc is on same vertical curve.
5. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 4, is characterized in that: be provided with between described left disk and right disk prevent the magnetic field of left disk and right disk from mutually disturbing every magnetic part.
6. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 5, it is characterized in that: described left conductor disc is provided with radiator away from the side of left disk, described right conductor disc is provided with radiator away from the side of right disk.
7. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 3, it is characterized in that: be provided with the transmission mechanism described in three groups between described left disk and right disk, three groups of transmission mechanisms are circumferentially arranged at equal intervals.
8. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 2 or claim 3, is characterized in that: described clutch shaft bearing is double-row conical bearing.
9. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 8, is characterized in that: described second bearing is cylinder roller bearing.
10. cam type straight wing suspension magnetic eddy-current coupling as claimed in claim 9, is characterized in that: described oblique chute is helix.
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| CN201310013056.6A CN103107681B (en) | 2013-01-14 | 2013-01-14 | Cam type straight wing suspended magnetic eddy-current coupling |
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| CN106864716A (en) * | 2017-03-02 | 2017-06-20 | 浙江大学 | New pod propulsion electric propulsion device |
| CN107681869A (en) * | 2017-10-31 | 2018-02-09 | 中科储能（北京）科技有限公司 | Shaft coupling |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1362423A (en) * | 1970-08-11 | 1974-08-07 | Cefilac | Magnetic coupling |
| CN85103046A (en) * | 1985-04-18 | 1986-10-15 | 李仁国 | A kind of voith schneider propeller |
| CN1248354A (en) * | 1997-02-20 | 2000-03-22 | 马格纳福斯公司 | Adjustable magnetic coupler |
| CN101982932A (en) * | 2010-09-21 | 2011-03-02 | 南京大寰控制系统有限公司 | Disc water-cooling permanent magnet eddy current speed regulation device |
| CN102324830A (en) * | 2011-08-31 | 2012-01-18 | 唐委校 | Vertical permanent magnetic variable torque variable speed coupler with radiating device |
| CN202652040U (en) * | 2012-05-15 | 2013-01-02 | 上海普天邮通科技股份有限公司 | Eddy current transmission |
-
2013
- 2013-01-14 CN CN201310013056.6A patent/CN103107681B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1362423A (en) * | 1970-08-11 | 1974-08-07 | Cefilac | Magnetic coupling |
| CN85103046A (en) * | 1985-04-18 | 1986-10-15 | 李仁国 | A kind of voith schneider propeller |
| CN1248354A (en) * | 1997-02-20 | 2000-03-22 | 马格纳福斯公司 | Adjustable magnetic coupler |
| CN101982932A (en) * | 2010-09-21 | 2011-03-02 | 南京大寰控制系统有限公司 | Disc water-cooling permanent magnet eddy current speed regulation device |
| CN102324830A (en) * | 2011-08-31 | 2012-01-18 | 唐委校 | Vertical permanent magnetic variable torque variable speed coupler with radiating device |
| CN202652040U (en) * | 2012-05-15 | 2013-01-02 | 上海普天邮通科技股份有限公司 | Eddy current transmission |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103107681A (en) | 2013-05-15 |
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Effective date of registration: 20160804 Address after: 241311, Wuhu County, Anhui City, Nanling province Yijiang town industrial concentration area Patentee after: Wuhu Mingxin motor energy saving Technology Co.,Ltd. Address before: 241311, Wuhu County, Anhui City, Nanling province Yijiang town industrial concentration area Patentee before: WUHU MINGXIN MACHINERY MANUFACTURING Co.,Ltd. Effective date of registration: 20160804 Address after: 241311, Wuhu County, Anhui City, Nanling province Yijiang town industrial concentration area Patentee after: WUHU MINGXIN MACHINERY MANUFACTURING Co.,Ltd. Address before: 310027 Hangzhou, Zhejiang Province, Xihu District, Zhejiang Road, No. 38, No. Patentee before: Zhejiang University |