CN109441716B - Suspension wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator - Google Patents
Suspension wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator Download PDFInfo
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- CN109441716B CN109441716B CN201811176960.8A CN201811176960A CN109441716B CN 109441716 B CN109441716 B CN 109441716B CN 201811176960 A CN201811176960 A CN 201811176960A CN 109441716 B CN109441716 B CN 109441716B
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- 239000000725 suspension Substances 0.000 title claims abstract description 40
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- 238000007667 floating Methods 0.000 claims abstract description 6
- 230000001133 acceleration Effects 0.000 claims description 17
- 230000033228 biological regulation Effects 0.000 claims description 8
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- 238000005452 bending Methods 0.000 claims description 5
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- 241001391944 Commicarpus scandens Species 0.000 description 2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor
- F03D3/06—Rotors
- F03D3/061—Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor
- F03D3/06—Rotors
- F03D3/062—Rotors characterised by their construction elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D7/00—Controlling wind motors
- F03D7/06—Controlling wind motors the wind motors having rotation axis substantially perpendicular to the air flow entering the rotor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02N—ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR
- H02N15/00—Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for
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- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction
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Abstract
The invention provides a suspension wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator, which structurally comprises a connecting sleeve, a supporting rod, a suspension wing type micro-power speed-increasing and breaking device, a set pressure bearing ball, a positive magnetic ring, a negative magnetic ring and an air-floating hollow wind wing plate, wherein the top end of the connecting sleeve is fixedly connected to the bottom end of the supporting rod in an electric welding mode and is positioned at the same axis, because a wind sensing adjusting mechanism and a top limiting and speed increasing mechanism in a speed-increasing wind sensing instantaneous adjusting group are matched with each other, wind power smaller than the starting wind power of an original wind wing can provide rotating power for the wind wing through the wind sensing adjusting mechanism, the inertia breaking mechanism in the inertia protection breaking group is matched with a protection resetting mechanism, the inertia breaking mechanism is unfolded through centrifugal inertia force under the normal working state of the wind wing, and branches and other hard sundries carried during wind blowing are cut and broken when contacting the rotating wind wing, thereby protecting the wind wings.
Description
Technical Field
The invention belongs to the field of generators, and particularly relates to a suspended wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator.
Background
The magnetic suspension generator is generally arranged outdoors and can receive wind power in various directions, wind wings need a certain magnitude of wind power to provide rotating kinetic energy for the wind wings, when the wind power meets requirements, the wind wings rotate by receiving the wind power and perform magnetic induction cutting with internal magnetic rings to convert the wind kinetic energy into electric potential energy, and the magnetic suspension wind wings are arranged in the air outdoors and need to receive the blowing of the wind to the greatest extent, so that the magnetic suspension generator is difficult to protect the wind.
Based on the above description, the inventor finds that the existing magnetic suspension generator with suspended wing type micro-power acceleration and disconnection protection mainly has the following disadvantages, for example:
1. when the wind power is small, the wind wings are difficult to drive, and when the wind power is large, the rotating speed of the wind wings can only be maintained at the balance point of the highest rotating speed, so that the breakthrough is difficult to carry out.
2. When the wind wing performs normal rotation work, the blade of the wind wing is very easy to break because hard sundries such as branches and the like carried by the wind during blowing contact with the rotating wind wing.
Disclosure of Invention
In order to solve the technical problems, the invention provides a suspension wing type micro-power acceleration breaking protection magnetic suspension generator, which aims to solve the problems that the wind wings are difficult to drive when the wind power is small, the rotating speed of the wind wings can only be maintained at the balance point of the highest rotating speed when the wind power is large, the wind wings are difficult to break through, and when the wind wings normally rotate to do work, the blades of the wind wings are extremely easy to break when hard sundries such as branches and the like carried by the wind during blowing contact with the rotating wind wings.
Aiming at the defects of the prior art, the invention discloses the purpose and the effect of a suspended wing type micro-power acceleration and disconnection protection magnetic suspension generator, which are achieved by the following specific technical means: a magnetic suspension generator with suspension wing type micro-power acceleration and disconnection protection structurally comprises a connecting sleeve, a supporting rod, a suspension wing type micro-power acceleration and disconnection device, an integrated pressure bearing ball, a positive magnetic ring, a negative magnetic ring and an air-floating hollow wind wing plate, the top end of the connecting sleeve is fixedly connected to the bottom end of the supporting rod in an electric welding mode, the central axes of the connecting sleeve and the supporting rod are on the same straight line, the three suspension wing type micro-power speed-increasing and breaking devices are arranged, the bottom ends of the three suspension wing type micro-power speed-increasing and breaking devices are fixedly connected to the outer ring surface of the hollow-out air wing plate in an electric welding mode, the top end of the negative magnetic coil is arranged at the bottom end of the positive magnetic coil in an embedded mode, the central axes of the negative magnetic coil and the positive magnetic coil are on the same straight line, the top end of the supporting rod penetrates through the axis of the bottom end of the negative magnetic ring, and the bottom end of the integrated pressure bearing ball is fixedly installed at the top end of the positive magnetic ring through the supporting rod.
Hang wing formula micro-power acceleration rate breakaway device including locking connection core, acceleration sense wind instantaneous regulation group, pterygoid lamina, inertia protection breakaway group, locking connection core is equipped with six altogether, and two locking connection cores are a set of welding respectively on top about the pterygoid lamina, acceleration sense wind instantaneous regulation group is equipped with one hundred forty and evenly distributed at the medial surface of pterygoid lamina altogether, inertia protection breakaway group is equipped with four altogether, and two inertia protection breakoffs group 34 are a set of opposition fixed mounting in both ends about the pterygoid lamina is inside.
Preferably, the speed-increasing wind-sensing instantaneous adjusting group comprises a middle shaft strip, a wind-sensing adjusting mechanism, a top-limiting speed-increasing mechanism, an arc-shaped strip rail and an inwards concave semi-circular groove, the concave semicircular groove and the wing plate are of an integrated structure, the arc-shaped strip rail is arranged at the central position inside the concave semicircular groove and is of an integrated structure with the wing plate, the wind sensing adjusting mechanisms are fixed on the longitudinal inner sides of the concave semicircular grooves through the middle shaft strips, two and one end far away from the axis of each group of the top limiting and speed increasing mechanisms are fixedly arranged on the transverse inner sides of the concave semicircular grooves in each group of speed increasing and wind sensing instantaneous adjusting groups, the concave semicircular grooves are of semicircular groove structures, wherein the arc-shaped strip rail is of an arc-shaped groove strip structure and is filled into the inner concave semicircular groove when wind blows, the semi-circular groove type structure can conduct guiding effect with least energy consumption on wind power, and certain impact force is generated on wing plates while the wind power is poured.
Preferably, the wind sensing adjusting mechanism comprises a friction force weakening moving ejector rod, a wind sensing deformation combined pocket strip, adjusting strips and an outer ring rail, the right end of the friction force weakening moving ejector rod is fixedly connected to the left end of the outer ring rail in an electric welding mode, the adjusting strips are provided with four in a group of the wind sensing adjusting mechanisms, two adjusting strips 3223 are in a group and are respectively and fixedly installed on the front surface and the back surface of the wind sensing deformation combined pocket strip, the wind sensing deformation combined pocket strip is provided with seven in a group of the wind sensing adjusting mechanisms, the seven are different in size in the group of the wind sensing adjusting mechanisms, the seven are mutually embedded and movably installed on the inner ring surface of the outer ring rail, each layer of the wind sensing deformation combined pocket strip is of a flexible arc structure with different sizes, the adjusting strips are connected together through the adjusting strips, the adjusting strips have certain elasticity, and are directly impacted on the wind sensing deformation combined pocket strip under the guidance of the inner concave semicircular, the wind sensing deformation combined pocket strip changes the single-side orientation of the wind sensing deformation combined pocket strip under the impact of wind power, the outer ring rail is pushed to adjust the distance according to the size of the wind power, the wind sensing deformation combined pocket strip can effectively receive the impact of the wind when the wind quantity is small, and the wind wing can effectively do work with smaller wind quantity compared with the original braking wind quantity of the wind wing.
Preferably, the top limiting speed increasing mechanism comprises a transverse resistance plate, a pin lock column and a bending return speed increasing strip, the pin lock column is provided with three pin lock columns in each group of top limiting speed increasing mechanisms, one end of each pin lock column, far away from the wing plate, is fixedly connected to one end of the transverse resistance plate, attached to the wing plate, in an electric welding mode, and the bending return speed increasing strip is provided with twelve pin lock columns in each group of top limiting speed increasing mechanisms, and the top ends of the pin lock columns are fixedly connected with the bottom end of the transverse resistance plate.
Preferably, the inertia protection breaking group comprises four inertia breaking mechanisms and four protection resetting mechanisms, the two inertia breaking mechanisms are respectively fixedly arranged at the upper end and the lower end in the wing plate in a group, the two protection resetting mechanisms are respectively fixedly arranged at the upper end and the lower end in the wing plate in a group, the upper end and the lower end in the wing plate in a group are respectively fixedly arranged at the upper end and the lower end in the wing plate in a group, one end of the inertia breaking mechanism close to the center of the wing plate is movably connected with one end of the protection resetting mechanism far away from the center of the wing plate, the inertia breaking mechanism comprises a single-action breaking knife, a guide rod, a traction lock rod, a tension traction rope, a through hole, a guide groove strip and a fixed vertical guide strip, two ends of the single-action breaking knife in the same group of inertia breaking mechanisms are arranged, the adjacent ends of the single-action breaking knife are respectively fixedly connected, and the two guide rods are a group and are respectively fixed at the upper end and the lower end of the single-action disconnecting knife, the guide groove strip and the wing plate are of an integrated structure, and the back of the fixed vertical guide strip is fixedly connected inside the wing plate in an electric welding mode.
Preferably, the protection reset mechanism comprises a rotary shaft rod, an insulating arc strip, a strong magnetic plate and an unbalanced magnetic strip, wherein the rotary shaft rod penetrates through the insulating arc strip and is installed inside the wing plate in an embedded mode, one end of the rotary shaft rod is far away from the unbalanced magnetic strip and is fixedly connected with the right end of the insulating arc strip, and the bottom end of the strong magnetic plate is installed inside the wing plate in an embedded mode.
Compared with the prior art, the invention has the following beneficial effects:
the wind sensing adjusting mechanism and the top limiting speed increasing mechanism in the speed increasing wind sensing instantaneous adjusting group are matched with each other, so that wind power smaller than the starting wind power of the original wind wing can provide rotating power for the wind wing through the wind sensing adjusting mechanism, reverse wind resistance kinetic energy can be intermittently increased for the wind wing through the top limiting speed increasing mechanism when the wind power is large, the rotating speed is improved, the inertia breaking mechanism in the inertia protection breaking group is matched with the protection resetting mechanism, the inertia breaking mechanism is unfolded through centrifugal inertia force under the normal working state of the wind wing, and hard sundries such as branches and the like carried in the wind blowing process are cut and broken at the moment of contact when the wind wing rotates, so that the wind wing is protected.
Drawings
Fig. 1 is a schematic structural diagram of a suspended wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator.
Fig. 2 is a schematic front structure view of the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 3 is a schematic side structure view of the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 4 is a schematic view of a front cross-sectional structure of the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 5 is a detailed structural schematic diagram of a speed-increasing wind-sensing instantaneous adjusting set in the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 6 is a detailed structural diagram of the wind-sensing adjusting mechanism in the speed-increasing wind-sensing instantaneous adjusting group after being unfolded.
Fig. 7 is a schematic side structure view of a speed-increasing wind-sensing instantaneous adjusting set in the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 8 is a schematic side sectional structure view of a top-limiting speed-increasing mechanism in the suspended wing type micro-power speed-increasing disconnecting device.
Fig. 9 is an enlarged structural schematic diagram of a front section a of the suspension wing type micro-power speed-increasing disconnecting device.
Fig. 10 is an enlarged detailed structural schematic diagram of a front section a of the suspension wing type micro-power speed-increasing disconnecting device.
In the figure: a connecting sleeve-1, a supporting rod-2, a suspended wing type micro-power speed-increasing and breaking device-3, a collective pressure-bearing ball-4, a positive magnetic ring-5, a negative magnetic ring-6, an air-floating hollowed wind wing plate-7, a locking connecting core plate-31, a speed-increasing wind-sensing instantaneous adjusting group-32, a wing plate-33, an inertial protection breaking group-34, a central shaft bar-321, a wind-sensing adjusting mechanism-322, a top-limiting speed-increasing mechanism-323, an arc-shaped bar rail-324, an inner concave semicircular groove-325, a friction force weakening moving ejector rod-3221, a wind-sensing deformation combined pocket bar-3222, an adjusting bar-3223, an outer ring rail-3224, a transverse resistance plate-3231, a pin locking column-3232, a bending return speed-increasing bar-3233, an inertial breaking mechanism-341, a protection resetting mechanism-342, a safety device, A single-action breaking knife-3411, a guide rod-3412, a traction lock rod-3413, a pulling force traction rope-3414, a through hole-3415, a fixed vertical guide strip-3416, a rotating shaft rod-3421, an insulating arc strip-3422, a strong magnetic plate-3423 and an unbalanced magnetic strip-3424.
Detailed Description
The embodiments of the present invention will be described in further detail with reference to the drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Examples
As shown in figures 1 to 10:
the invention provides a magnetic suspension generator with suspension wing type micro-power acceleration and disconnection protection, which structurally comprises a connecting sleeve 1, a supporting rod 2, a suspension wing type micro-power acceleration and disconnection device 3, an integrated pressure bearing ball 4, a positive magnetic ring 5, a negative magnetic ring 6 and an air-floating hollowed-out wind wing plate 7, wherein the top end of the connecting sleeve 1 is fixedly connected to the bottom end of the supporting rod 2 in an electric welding mode, the central axes of the connecting sleeve 1 and the supporting rod 2 are on the same straight line, the suspension wing type micro-power acceleration and disconnection device 3 is provided with three magnetic rings, the bottom ends of the three magnetic rings are fixedly connected to the outer ring surface of the air-floating hollowed-out wind wing plate 7 in an electric welding mode, the top end of the negative magnetic ring 6 is installed at the bottom end of the positive magnetic ring 5 in an embedding mode, the central axes of the negative magnetic ring 6 and the positive magnetic ring 5 are on the same straight line, and the, set pressure ball 4 bottoms are passed through 2 fixed mounting in 5 tops of anodal magnetosphere of bracing piece, hang wing formula micro-power acceleration rate disconnected device 3 and include locking connection core 31, acceleration rate and feel wind instantaneous regulation group 32, pterygoid lamina 33, inertia protection disconnected group 34, locking connection core 31 is equipped with six altogether, and just two locking connection cores 31 are a set of welding respectively on top and bottom of pterygoid lamina 33, acceleration rate and feel wind instantaneous regulation group 32 is equipped with one hundred forty and evenly distributed at the medial surface of pterygoid lamina 33 altogether, inertia protection disconnected group 34 is equipped with four altogether, and two inertia protection disconnected groups 34 are a set of opposition fixed mounting at both ends about pterygoid lamina 33 is inside.
Wherein, the speed-increasing wind-sensing instantaneous adjusting group 32 comprises a middle shaft strip 321, a wind-sensing adjusting mechanism 322, a top-limiting speed-increasing mechanism 323, an arc-shaped strip rail 324 and an inner concave semicircular groove 325, the concave semicircular groove 325 and the wing plate 33 are integrated, the arc-shaped strip rail 324 is arranged at the central position inside the concave semicircular groove 325 and is integrated with the wing plate 33, the wind sensing adjusting mechanism 322 is fixed at the longitudinal inner side of the concave semicircular groove 325 through a central shaft strip 321, the top limiting and speed increasing mechanism 323 is provided with two speed increasing and wind sensing instantaneous adjusting groups 32, one end of each group far away from the axis is fixedly arranged with the transverse inner side of the inner concave semicircular groove 325, the inner concave semicircular groove 325 is of a semicircular groove structure, wherein the arc-shaped strip rail 324 is an arc-shaped groove strip structure, when wind blows through, the wind is poured into the inner concave semicircular groove 325, the semicircular groove type structure can conduct guiding effect with least energy consumption on wind power, and certain impact force is generated on the wing plates 33 when the wind power is poured.
Wherein the wind sensing adjusting mechanism 322 comprises a friction force weakening moving push rod 3221, a wind sensing deformation combined pocket bar 3222, an adjusting bar 3223 and an outer ring rail 3224, the right end of the friction force weakening moving push rod 3221 is fixedly connected to the left end of the outer ring rail 3224 in an electric welding manner, four adjusting bars 3223 are arranged in a group of the wind sensing adjusting mechanism 322, two adjusting bars 3223 are respectively and fixedly arranged on the front and back surfaces of the wind sensing deformation combined pocket bar 3222, the wind sensing deformation combined pocket bar 3222 is provided with seven bars with different sizes in a group of the wind sensing adjusting mechanism 322, the seven bars are mutually embedded and movably arranged on the inner ring surface of the outer ring rail 3224, each layer of the wind sensing deformation combined pocket bar 3222 is in a flexible arc structure with different sizes, the adjusting bars 3223 are connected together, the adjusting bar 3223 has certain elasticity, and is directly impacted on the wind sensing deformation combined pocket bar 3222 under the guidance of the semicircular groove 325 when wind enters the inner concave semicircular groove 325, the wind sensing deformation combined pocket bar 3222 changes the single-side orientation of the wind sensing deformation combined pocket bar 3222 under the impact of wind power, and pushes the outer ring rail 3224 to adjust the distance according to the size of the wind power, the wind sensing deformation combined pocket bar 3222 can effectively receive the impact of the wind when the wind quantity is small, and the wind wing can effectively do work with smaller wind quantity compared with the original braking wind quantity of the wind wing.
Wherein, the top-limiting speed-increasing mechanism 323 comprises three pin lock columns 3231, a pin lock column 3232 and a curved return speed-increasing bar 3233, the pin lock column 3232 is provided with three pin lock columns in each group of top-limiting speed-increasing mechanisms 323, one end of each pin lock column which is far away from the wing plate 33 is fixedly connected with one end of the corresponding cross resistance plate 3231 which is jointed with the wing plate 33 in an electric welding mode, twelve pin lock columns 3233 are provided in each group of top-limiting speed-increasing mechanisms 323, the top end of each pin lock column 3233 is fixedly connected with the bottom end of the corresponding cross resistance plate 3231, the cross resistance plates 3231 are arc-shaped layered hard plates and are fixed on the wing plates 33 through the pin lock columns 3232, so that effective stroke limiting can be carried out on the outer ring rail 3224 pushed after the wind-sensing deformation combined pocket bar 3222 expands to the limit, and the curved return speed-increasing bar 3233 at the lower end has certain elastic potential energy to rebound the outer ring rail 3224 after impacting on the curved return speed-sensing deformation, a small resistive area against the wind is formed, and the combined pocket bar 3222 is deformed by the wind after the phase impact acts on the wing plate 33 with a larger impact force, thereby accomplishing the extreme acceleration.
Wherein, the inertia protection breaking group 34 comprises an inertia breaking mechanism 341 and a protection resetting mechanism 342, the inertia breaking mechanism 341 and the protection resetting mechanism 342 are respectively provided with four, the two inertia breaking mechanisms 341 are respectively fixedly arranged at the upper end and the lower end of the inside of the wing plate 33 in a group, the two protection resetting mechanisms 342 are respectively fixedly arranged at the upper end and the lower end of the inside of the wing plate 33 in a group, one end of the inertia breaking mechanism 341 close to the center of the wing plate 33 is movably connected with one end of the protection resetting mechanism 342 far from the center of the wing plate 33, the inertia breaking mechanism 341 comprises a single-acting breaking knife 3411, a guide rod 3412, a traction lock rod 3, a pulling force traction rope 4, a through hole 3415, a guide groove 3416 and a fixed vertical guide strip 3417, the single-acting breaking knife 3411 is provided with two in the same group of inertia breaking mechanisms 341, and the adjacent ends are respectively fixedly connected with the head end of the traction rope 3414 through, the guide rods 3412 are arranged in the same group of inertia breaking mechanisms 341, the two guide rods 3412 are fixed to the upper end and the lower end of a single-action breaking knife 3411 respectively in a group, the guide groove strips 3416 and the wing plates 33 are of an integrated structure, the back of each fixed vertical guide strip 3417 is fixedly connected to the inside of each wing plate 33 in an electric welding mode, the single-action breaking knife 3411 is in an oval one-way incomplete shape and has a certain weight, the single-action breaking knife 3411 can be swung and extended out through the centrifugal force of each wing plate 33 and the gravitational potential energy of the corresponding wing plate 33 when the wing plates 33 rotate to do work, the pulling force traction rope 3414 is pulled to carry out constraint of a resetting stroke, the single-action breaking knife 3411 can provide effective protection for the wing plates 33 in a working state after being extended out, and rapid cutting blocking can.
Wherein, the protection reset mechanism 342 comprises a rotating shaft 3421, an insulating arc strip 3422, a strong magnetic plate 3423, an unbalanced magnetic strip 3424, the shaft rotating rod 3421 penetrates the insulating arc strip 3422 and is installed inside the wing plate 33 by means of embedding, one end of the unbalanced magnetic strip 3424 away from the rotating shaft 3421 is fixedly connected to the right end of the insulating arc strip 3422, the bottom end of the strong magnetic plate 3423 is embedded in the wing plate 33, the unbalanced magnetic strip 3424 is a drop-shaped strip structure, the internal magnetism of the single-action knife 3411 is changed from strong to weak, when the single-action knife 3411 is in a fully unfolded state, the insulating arc 3422 is in a fixed-point state of ninety degrees, if the wind power is reduced, the centrifugal force is reduced, and it is difficult to maintain the complete state of the single-action knife 3411 to perform clockwise reset rotation under the gravity action of the unbalanced magnetic strip 3424, and to perform reset fixation through mutual attraction with the strong magnetic plate 3423.
The specific use mode and function of the embodiment are as follows:
the invention relates to a hanging wing type micro-power speed-increasing disconnecting device 3 which belongs to six surfaces and receives wind, when wind blows from any direction, the inner concave semi-circular groove 325 in a speed-increasing wind-sensing instantaneous adjusting group 32 fixedly arranged on a wing plate 33 can brake the wing plate 33 through the arc structure, the wind impacts a wind-sensing deformation combined pocket strip 3222 under the guidance of an arc ring when entering, because the friction force weakens the movable push rod 3221 embedded in the arc-shaped track 324 and the friction force applied when the movable push rod is very small, the wind-sensing deformation combined pocket strip 3222 is pushed by the wind to expand towards the wind direction, the friction force weakens the movable push rod 3221 to be propped against the bottom end in the transverse resistance plate 3231 after the complete expansion, the outer annular surface of an outer annular track 3224 is contacted with the bottom end of a curved movement speed-increasing strip 3233, and the wind-sensing adjusting mechanism 3223 is impacted once at the moment when the wind completely expands the wind-sensing adjusting mechanism 322, the wind sensing adjusting mechanism 3223 is passively compressed by a limited stroke and then reset, a certain amount of thrust is generated to the outer ring rail 3224 while resetting, the whole wind sensing adjusting mechanism 322 generates reverse impact with the wind direction, so that the rotating speed of the wing plate 33 is increased, when the wing plate 33 starts to rotate regularly, centrifugal force generated by rotation uniformly acts on the wing plate 33, the strong magnetic plate 3411 follows the direction of the centrifugal force along the track of the wind sensing adjusting mechanism 3416 under the double action of self gravity and inertial potential energy, extends towards the outside of the wing plate 33, when the wind sensing adjusting mechanism 3411 is completely unfolded, the bottom wind sensing adjusting mechanism 3422 passively generates linkage due to connection with the wind sensing adjusting mechanism 3411, rotates around the wind sensing adjusting mechanism 3421 for a quarter of anticlockwise rotation and drives the wing plate 3424 to be separated from the strong magnetic plate 3423, if the wing plate 33 is hit by a foreign object while rotating, the wing plate is instantaneously separated by the single-break separation knife 3411 extending out of the outer side of the wing plate 33, the wing 33 is effectively protected, and the extended single-action disconnecting knife 3411 can break wind while the wing 33 rotates.
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (4)
1. The utility model provides a magnetic suspension generator of protection is disconnected in little power acceleration rate of suspension wing formula, its structure includes connecting sleeve (1), bracing piece (2), little power acceleration rate of suspension wing formula disconnected device (3), set pressure ball (4), anodal magnetosphere (5), negative pole magnetosphere (6), empty fretwork wind pterygoid lamina (7) that floats, its characterized in that: the top end of the connecting sleeve (1) is fixedly connected to the bottom end of the supporting rod (2) in an electric welding mode, the central axes of the connecting sleeve (1) and the supporting rod (2) are on the same straight line, the three suspension wing type micro-power speed-increasing and disconnecting device (3) are arranged, the bottom ends of the three suspension wing type micro-power speed-increasing and disconnecting device are fixedly connected to the outer ring surface of the air floating hollowed-out wind wing plate (7) in an electric welding mode, the top end of the negative magnetic ring (6) is installed at the bottom end of the positive magnetic ring (5) in an embedding mode, the central axes of the negative magnetic ring (6) and the positive magnetic ring (5) are on the same straight line, the top end of the supporting rod (2) penetrates through the axis of the bottom end of the negative magnetic ring (6), and the bottom end of the integrated pressure-bearing ball; the suspended wing type micro-power speed-increasing and breaking device (3) comprises six locking connection core plates (31), a speed-increasing wind-sensing instantaneous regulation group (32), wing plates (33) and two inertia protection breaking groups (34), wherein the two locking connection core plates (31) are in a group and are respectively welded at the upper top end and the lower top end of the wing plates (33), the speed-increasing wind-sensing instantaneous regulation group (32) is in a group of one hundred and forty and are uniformly distributed on the inner side surfaces of the wing plates (33), the inertia protection breaking groups (34) are in four, and the two inertia protection breaking groups (34) are in a group of opposite fixed mounting at the upper end and the lower end in the wing plates (33);
the speed-increasing wind-sensing instantaneous regulation group (32) comprises a central shaft strip (321), a wind-sensing regulation mechanism (322), a top-limiting speed-increasing mechanism (323), an arc-shaped strip rail (324) and an inner concave semicircular groove (325), wherein the inner concave semicircular groove (325) and a wing plate (33) are of an integrated structure, the arc-shaped strip rail (324) is arranged at the central position inside the inner concave semicircular groove (325) and is of an integrated structure with the wing plate (33), the wind-sensing regulation mechanism (322) is fixed on the longitudinal inner side of the inner concave semicircular groove (325) through the central shaft strip (321), and the top-limiting speed-increasing mechanism (323) is provided with two speed-increasing wind-sensing instantaneous regulation groups (32) and is fixedly installed with the transverse inner side of the inner concave semicircular groove (325) at one end far away from;
the inertia protection breaking group (34) comprises inertia breaking mechanisms (341) and protection reset mechanisms (342), the inertia breaking mechanisms (341) and the protection reset mechanisms (342) are respectively provided with four, the two inertia breaking mechanisms (341) are fixedly arranged at the upper end and the lower end of the inside of the wing plate (33) respectively in a group, the two protection reset mechanisms (342) are fixedly arranged at the upper end and the lower end of the inside of the wing plate (33) respectively in a group, one end, close to the center of the wing plate (33), of the inertia breaking mechanism (341) is movably connected with one end, far away from the center of the wing plate (33), of the protection reset mechanism (342), the inertia breaking mechanism (341) comprises a single-action breaking knife (3411), a guide rod (3412), a traction lock rod (3413), a tension traction rope (3414), a through hole (3415), a guide groove strip (3416) and a fixed vertical guide strip (3417), two ends of the single-action breaking knife (3411) are arranged in the same group of the inertia breaking mechanisms (341), and one end is The guide rod (3413) is fixedly connected with the head end of a pulling force traction rope (3414), four guide rods (3412) are arranged in the same group of inertia disconnecting mechanisms (341), the two guide rods (3412) are fixed to the upper end and the lower end of a single-action disconnecting knife (3411) respectively in a group, the guide groove strip (3416) and the wing plate (33) are of an integrated structure, and the back of the fixed vertical guide strip (3417) is fixedly connected to the inside of the wing plate (33) in an electric welding mode.
2. The suspended wing type micro-power speed-increasing and disconnection-protecting magnetic suspension generator according to claim 1, characterized in that: the wind sensing adjusting mechanism (322) comprises a friction force weakening moving ejector rod (3221), a wind sensing deformation combined pocket strip (3222), adjusting strips (3223) and an outer ring rail (3224), wherein the right end of the friction force weakening moving ejector rod (3221) is fixedly connected to the left end of the outer ring rail (3224) in an electric welding mode, four adjusting strips (3223) are arranged in a group of wind sensing adjusting mechanisms (322), the two adjusting strips (3223) are fixedly arranged on the front side and the back side of the wind sensing deformation combined pocket strip (3222) respectively in a group, and the wind sensing deformation combined pocket strip (3222) is provided with seven strips with different sizes in the group of wind sensing adjusting mechanisms (322) and movably arranged on the inner ring surface of the outer ring rail (3224) in an embedding mode.
3. The suspended wing type micro-power speed-increasing and disconnection-protecting magnetic suspension generator according to claim 1, characterized in that: the top limiting speed increasing mechanism (323) comprises a transverse resistance plate (3231), pin lock columns (3232) and a bending return speed increasing strip (3233), wherein the pin lock columns (3232) are arranged in three in each group of top limiting speed increasing mechanisms (323), one ends of the pin lock columns, which are far away from wing plates (33), are fixedly connected to one ends of the transverse resistance plate (3231) and the attachment wing plates (33) in an electric welding mode, and the bending return speed increasing strip (3233) is arranged in twelve in each group of top limiting speed increasing mechanisms (323) and the top ends of the pin lock columns and the bottom end of the transverse resistance plate (3231) are fixedly connected together.
4. The suspended wing type micro-power speed-increasing and disconnection-protecting magnetic suspension generator according to claim 1, characterized in that: the protection reset mechanism (342) comprises a rotary shaft rod (3421), an insulating arc strip (3422), a strong magnetic plate (3423) and an unbalanced magnetic strip (3424), wherein the rotary shaft rod (3421) penetrates through the insulating arc strip (3422) and is installed inside the wing plate (33) in an embedded mode, one end of the unbalanced magnetic strip (3424) far away from the rotary shaft rod (3421) is fixedly connected with the right end of the insulating arc strip (3422), and the bottom end of the strong magnetic plate (3423) is installed inside the wing plate (33) in an embedded mode.
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| CN201811176960.8A CN109441716B (en) | 2018-10-10 | 2018-10-10 | Suspension wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811176960.8A CN109441716B (en) | 2018-10-10 | 2018-10-10 | Suspension wing type micro-power speed-increasing and breaking-off protection magnetic suspension generator |
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| CN109441716B true CN109441716B (en) | 2020-02-25 |
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|---|---|---|---|---|
| CN1721691A (en) * | 2004-07-16 | 2006-01-18 | 邱垂南 | Track wind sail power generation method and device thereof |
| CN101319654A (en) * | 2007-06-07 | 2008-12-10 | 臧铁成 | Power generation wheel by unidirectional blade rotation and expansion action |
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