CN100493948C - Magnetic suspension thruster - Google Patents
Magnetic suspension thruster Download PDFInfo
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- CN100493948C CN100493948C CNB200510009954XA CN200510009954A CN100493948C CN 100493948 C CN100493948 C CN 100493948C CN B200510009954X A CNB200510009954X A CN B200510009954XA CN 200510009954 A CN200510009954 A CN 200510009954A CN 100493948 C CN100493948 C CN 100493948C
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- magnet
- guide rail
- magnet pulley
- induction guide
- wheel
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Abstract
A magnetic levitation propulsion system for magneti levitation train is disclosed. Its advantages are self-adaptive and self-stabilized levitation force, great magnetic levitation gap, and high safety.
Description
Technical field:
What the present invention relates to is the electromagnetic power technical field, specifically is a kind of magnetic suspension thruster.
Background technology:
Existing magnetic suspension train is divided into often leads type and superconduct two big classes.The type of often leading also claims normal magnetic conduction suction type, is representative with the Germany floating train transrapid of at a high speed normal magnetic conduction, and it is to utilize the principle of conventional DC electromagnet electromagnetic attraction that train is hanged, and the air gap of suspension is less, is generally 10 millimeter.The speed of often leading the type high-speed maglev train can reach per hour 400~500 kilometers, is suitable for intercity length apart from fast traffic.And the superconduct magnetic suspension train also claims the superconduction magnetic expelling type, with Japanese MAGLEV is representative, it is the high-intensity magnetic field that utilizes superconducting magnet to produce, during train operation be arranged in ground coil mutual action, producing electrodynamic repulsion force hangs train, suspension air gap is bigger, is generally 100 millimeter, and speed can reach per hour more than 500 kilometers.Although magnetic suspension train has above-mentioned many advantages, but still come with some shortcomings: (1) is because magnetic suspension system is finished suspension, guiding and driving function with electromagnetic force, braking problem after this has a power failure with regard to problem, the especially train that exists in outage back magnetic suspension safety control remains the problem that will solve; (2) hoverheight of normal magnetic conduction suspension technology is lower, and is therefore higher than superconductor technology to the requirement of planeness, subgrade settlement amount and the switch structure aspect of circuit; (3) the super-conductive magnetic suspension technology is because the normal waveguide technology of eddy effect suspension energy consumption is bigger, and cooling system is heavy, and high-intensity magnetic field is also all influential to human body and environment; (4) adopt linear motor driving, drive efficiency is lower, and the control difficulty is bigger.
Summary of the invention:
The purpose of this invention is to provide a kind of magnetic suspension thruster.The present invention can solve the maglev safety control problem in existing magnetic suspension train outage back, the normal lower problem of magnetic conduction suspension technology hoverheight, and the bigger problem of super-conductive magnetic suspension technology suspension energy consumption.It is made up of dynamic assembly 1, first support wheel 2, second support wheel 3, first rail 4, second rail 5, base 6, first magnet pulley 7, second magnet pulley 8, the first induction guide rail 9, the second induction guide rail 10; First support wheel 2 is socketed in the middle part of the rotating shaft 1-1 left-hand end of dynamic assembly 1, second support wheel 3 is socketed in the middle part of the rotating shaft 1-1 right-hand end of dynamic assembly 1, the bottom of first rail 4, the bottom of second rail 5 all is connected on the upper surface of base 6, and make the periphery of first support wheel 2, the periphery of second support wheel 3 respectively with the upper surface of first rail 4, roll and connect in the upper surface of second rail 5, first magnet pulley 7 is socketed on the termination, rotating shaft 1-1 left side of dynamic assembly 1, second magnet pulley 8 is socketed on the termination, rotating shaft 1-1 right side of dynamic assembly 1, the first induction guide rail, 9 bottoms, the bottom of the second induction guide rail 10 all is connected on the upper surface of base 6, and makes the periphery of first magnet pulley 7, the periphery of second magnet pulley 8 place respectively first the induction guide rail 9 directly over, directly over the second induction guide rail 10.The first induction guide rail 9, the second induction guide rail 10 all are to be made of the double layer of metal material, and its skin is a magnetic material, and internal layer is a non-magnetic material.
The present invention has the following advantages:
1, lift force can self adaptation, self-stabilization, do not need special lift force control setup, therefore not only control simply, safe and reliable, and cost is low, operating efficiency is high;
2, suspension air gap is big, and lift force and propulsive force are stable, and has removed the requirement to guides with high precision from;
3, control owing to adopting on the car, can use for reference the control technology of High-speed Wheel, therefore the converters quantity that needs is few, and the feasible reliability low, system of controlling cost improves.
Description of drawings:
Fig. 1 is an integral structure scheme drawing of the present invention, Fig. 2 is the structural representation of the specific embodiment two, Fig. 3 is the structural representation of first magnet pulley 7 in the specific embodiment one, Fig. 4 is the left view of Fig. 3, Fig. 5 is the right elevation of Fig. 3, and Fig. 6 is the structural representation of first magnet pulley 7 in the specific embodiment three, and Fig. 7 is the left view of Fig. 6, Fig. 8 is the structural representation of first magnet pulley 7 in the specific embodiment four, and Fig. 9 is the left view of Fig. 8.
The specific embodiment:
The specific embodiment one: in conjunction with Fig. 1, Fig. 3, Fig. 4, Fig. 5 present embodiment is described, it is made up of dynamic assembly 1, first support wheel 2, second support wheel 3, first rail 4, second rail 5, base 6, first magnet pulley 7, second magnet pulley 8, the first induction guide rail 9, the second induction guide rail 10; First support wheel 2 is socketed in the middle part of the rotating shaft 1-1 left-hand end of dynamic assembly 1, second support wheel 3 is socketed in the middle part of the rotating shaft 1-1 right-hand end of dynamic assembly 1, the bottom of first rail 4, the bottom of second rail 5 all is connected on the upper surface of base 6, and make the periphery of first support wheel 2, the periphery of second support wheel 3 respectively with the upper surface of first rail 4, roll and connect in the upper surface of second rail 5, first magnet pulley 7 is socketed on the termination, rotating shaft 1-1 left side of dynamic assembly 1, second magnet pulley 8 is socketed on the termination, rotating shaft 1-1 right side of dynamic assembly 1, the first induction guide rail, 9 bottoms, the bottom of the second induction guide rail 10 all is connected on the upper surface of base 6, and makes the periphery of first magnet pulley 7, the periphery of second magnet pulley 8 place respectively first the induction guide rail 9 directly over, directly over the second induction guide rail 10.The section form of the described first induction guide rail 9 is the U type, the section form of the second induction guide rail 10 is identical with the section form of the first induction guide rail 9, the periphery of the periphery of first magnet pulley 7, second magnet pulley 8 respectively and first the induction guide rail 9 the U-bottom upper surface, second the induction guide rail 10 the U-bottom upper surface between have air gap L1, air gap L1 is 3mm~20mm; The right side of the left side of first magnet pulley 7, second magnet pulley 8 respectively and first the induction guide rail 9 inboard right side, second the induction guide rail 10 the inside left-end face between have air gap L2; Air gap L2 is 3mm~10mm, the left side of the right side of first magnet pulley 7, second magnet pulley 8 respectively and first the induction guide rail 9 the inside left-end face, second the induction guide rail 10 inboard right side between have air gap L3; Air gap L3 is 3mm~10mm.The first induction guide rail 9, the second induction guide rail 10 all are to be made of the double layer of metal material, and its skin is a magnetic material, and internal layer is a non-magnetic material.First magnet pulley 7 is made up of a plurality of cylindrical permanent magnetism sheet 7-1, a plurality of side permanent magnetism sheet 7-2, main wheel 7-3; The end face of each cylindrical permanent magnetism sheet 7-1 all is connected on the periphery of main wheel 7-3, each cylindrical permanent magnetism sheet 7-1 is evenly distributed side by side, the magnetizing direction of each cylindrical permanent magnetism sheet 7-1 on the main wheel 7-3 all is a radial magnetizing, and the pole polarity of each adjacent cylindrical permanent magnetism sheet 7-1 is opposite; All stud with a plurality of side permanent magnetism sheet 7-2 on the left end face of main wheel 7-3, its right end face, it is evenly distributed that each side permanent magnetism sheet 7-2 centers on the axle center of main wheel 7-3, the magnetizing direction of each side permanent magnetism sheet 7-2 on the main wheel 7-3 all is an axial charging, and the pole polarity of per two adjacent side permanent magnetism sheet 7-2 is opposite; Each cylindrical permanent magnetism sheet 7-1 is identical with the pole polarity of adjacent two side permanent magnetism sheet 7-2; The composition of second magnet pulley 8 is identical with first magnet pulley 7 with annexation.Principle of work: dynamic assembly 1 drives first support wheel 2, second support wheel 3, first magnet pulley 7, second magnet pulley, 8 high speed rotating by rotating shaft 1-1, because of on first magnet pulley 7, second magnet pulley 8 a plurality of cylindrical permanent magnetism sheet 7-1 being arranged, and and the electromagnetic force that produces forward, makes progress between the first induction guide rail 9, the second induction guide rail, whole device is upwards suspended, while can automatic guiding function when operation and have because of also having a plurality of side permanent magnetism sheet 7-2 on first magnet pulley 7, second magnet pulley 8.
The specific embodiment two: in conjunction with Fig. 2 present embodiment is described, the difference of the present embodiment and the specific embodiment one is that dynamic assembly 1 increase has a rotating shaft 1-2; First support wheel 2 is socketed on the left-hand end of rotating shaft 1-1 of dynamic assembly 1, second support wheel 3 is socketed on the right-hand end of rotating shaft 1-1 of dynamic assembly 1, first magnet pulley 7 is socketed on the termination, rotating shaft 1-2 left side of dynamic assembly 1, and second magnet pulley 8 is socketed on the termination, rotating shaft 1-2 right side of dynamic assembly 1.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment three: in conjunction with Fig. 6, Fig. 7 present embodiment is described, the difference of the present embodiment and the specific embodiment one is that first magnet pulley 7 is made up of a plurality of permanent magnet 7-4, leading magnet-wheel 7-5; The outer round surface of leading magnet-wheel 7-5 evenly has a plurality of groove 7-6, the opening direction of its groove 7-6 parallels with the axial line of leading magnet-wheel 7-5, all be inlaid with a permanent magnet 7-4 among each groove 7-6, the magnetizing direction of each permanent magnet 7-4 on the leading magnet-wheel 7-5 all is a cutting orientation magnetizing, and the pole polarity of per two adjacent permanent magnet 7-4 is identical; The composition of second magnet pulley 8 is identical with first magnet pulley 7 with annexation.Other composition is identical with the specific embodiment one or two with annexation.
The specific embodiment four: in conjunction with Fig. 8, Fig. 9 present embodiment is described, the difference of the present embodiment and the specific embodiment one is that first magnet pulley 7 is made up of a plurality of excitation winding 7-7, leading magnet wheel 7-8; The cylindrical of leading magnet wheel 7-8 is provided with a plurality of excitation pole 7-9, it is evenly distributed side by side that each excitation pole 7-9 centers on the axle center of dominating magnet wheel 7-8, all stud with an excitation winding 7-7 on each excitation pole 7-9, the first and last end of each adjacent excitation winding 7-7 all differential concatenation connects or all reverse parallel connection connections; The composition of second magnet pulley 8 is identical with first magnet pulley 7 with annexation.Other composition is identical with the specific embodiment one or two with annexation.Magnetic-field intensity in the present embodiment can be controlled in real time according to running condition.
Claims (6)
1, a kind of magnetic suspension thruster is characterized in that it is made up of dynamic assembly (1), first support wheel (2), second support wheel (3), first rail (4), second rail (5), base (6), first magnet pulley (7), second magnet pulley (8), the first induction guide rail (9), the second induction guide rail (10); First support wheel (2) is socketed in the middle part of rotating shaft (1-1) left-hand end of dynamic assembly (1), second support wheel (3) is socketed in the middle part of rotating shaft (1-1) right-hand end of dynamic assembly (1), the bottom of first rail (4), the bottom of second rail (5) all is connected on the upper surface of base (6), and make the periphery of first support wheel (2), the periphery of second support wheel (3) respectively with the upper surface of first rail (4), roll and connect in the upper surface of second rail (5), first magnet pulley (7) is socketed on the termination, rotating shaft (1-1) left side of dynamic assembly (1), second magnet pulley (8) is socketed on rotating shaft (1-1) termination, right side of dynamic assembly (1), first induction guide rail (9) bottom, the bottom of the second induction guide rail (10) all is connected on the upper surface of base (6), and make the periphery of first magnet pulley (7), the periphery of second magnet pulley (8) place respectively first the induction guide rail (9) directly over, directly over the second induction guide rail (10), the described first induction guide rail (9), the second induction guide rail (10) all is to be made of the double layer of metal material, its skin is a magnetic material, and internal layer is a non-magnetic material.
2, a kind of magnetic suspension thruster according to claim 1 is characterized in that last the increasing of dynamic assembly (1) has a rotating shaft (1-2); First support wheel (2) is socketed on the left-hand end of rotating shaft (1-1) of dynamic assembly (1), second support wheel (3) is socketed on the right-hand end of rotating shaft (1-1) of dynamic assembly (1), first magnet pulley (7) is socketed on the termination, rotating shaft (1-2) left side of dynamic assembly (1), and second magnet pulley (8) is socketed on rotating shaft (1-2) termination, right side of dynamic assembly (1).
3, a kind of magnetic suspension thruster according to claim 1, the section form that it is characterized in that the first induction guide rail (9) is the U type, the section form of the second induction guide rail (10) is identical with the section form of the first induction guide rail (9), the periphery of the periphery of first magnet pulley (7), second magnet pulley (8) respectively and first the induction guide rail (9) the U-bottom upper surface, second the induction guide rail (10) the U-bottom upper surface between have air gap (L1), air gap (L1) is 3mm~20mm; The right side of the left side of first magnet pulley (7), second magnet pulley (8) respectively and first the induction guide rail (9) inboard right side, second the induction guide rail (10) the inside left-end face between have air gap (L2); Air gap (L2) is 3mm~10mm, the left side of the right side of first magnet pulley (7), second magnet pulley (8) respectively and first the induction guide rail (9) the inside left-end face, second the induction guide rail (10) inboard right side between have air gap (L3); Air gap (L3) is 3mm~10mm.
4, a kind of magnetic suspension thruster according to claim 1 and 2 is characterized in that first magnet pulley (7) is made up of a plurality of cylindrical permanent magnetism sheets (7-1), a plurality of side permanent magnetism sheets (7-2), main wheel (7-3); An end face of each cylindrical permanent magnetism sheet (7-1) all is connected on the periphery of main wheel (7-3), each cylindrical permanent magnetism sheet (7-1) is evenly distributed side by side, the magnetizing direction of each the cylindrical permanent magnetism sheet (7-1) on the main wheel (7-3) all is a radial magnetizing, and the pole polarity of each adjacent cylindrical permanent magnetism sheet (7-1) is opposite; All stud with a plurality of side permanent magnetism sheets (7-2) on the left end face of main wheel (7-3), its right end face, it is evenly distributed that each side permanent magnetism sheet (7-2) all centers on the axle center of main wheel (7-3), the magnetizing direction of each the side permanent magnetism sheet (7-2) on the main wheel (7-3) all is an axial charging, and the pole polarity of per two adjacent side permanent magnetism sheets (7-2) is opposite; Each cylindrical permanent magnetism sheet (7-1) is identical with the pole polarity of adjacent two side permanent magnetism sheets (7-2); The composition of second magnet pulley (8) is identical with first magnet pulley (7) with annexation.
5, a kind of magnetic suspension thruster according to claim 1 and 2 is characterized in that first magnet pulley (7) is made up of a plurality of permanent magnets (7-4), leading magnet-wheel (7-5); The outer round surface of leading magnet-wheel (7-5) evenly has a plurality of grooves (7-6), the opening direction of its groove (7-6) parallels with the axial line of leading magnet-wheel (7-5), all be inlaid with a permanent magnet (7-4) in each groove (7-6), the magnetizing direction of each permanent magnet (7-4) on the leading magnet-wheel (7-5) all is a cutting orientation magnetizing, and the pole polarity of per two adjacent permanent magnet (7-4) is identical; The composition of second magnet pulley (8) is identical with first magnet pulley (7) with annexation.
6, a kind of magnetic suspension thruster according to claim 1 and 2 is characterized in that first magnet pulley (7) is made up of a plurality of excitation winding (7-7), leading magnet wheel (7-8); The cylindrical of leading magnet wheel (7-8) is provided with a plurality of excitation poles (7-9), it is evenly distributed side by side that each excitation pole (7-9) all centers on the axle center of dominating magnet wheel (7-8), all stud with an excitation winding (7-7) on each excitation pole (7-9), the first and last end of each adjacent excitation winding (7-7) all differential concatenation connects or all reverse parallel connection connections; The composition of second magnet pulley (8) is identical with first magnet pulley (7) with annexation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CNB200510009954XA CN100493948C (en) | 2005-04-29 | 2005-04-29 | Magnetic suspension thruster |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CNB200510009954XA CN100493948C (en) | 2005-04-29 | 2005-04-29 | Magnetic suspension thruster |
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CN1686736A CN1686736A (en) | 2005-10-26 |
CN100493948C true CN100493948C (en) | 2009-06-03 |
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CNB200510009954XA Expired - Fee Related CN100493948C (en) | 2005-04-29 | 2005-04-29 | Magnetic suspension thruster |
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Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN103523242A (en) * | 2013-10-25 | 2014-01-22 | 东南大学 | Electromagnetic catapult based on magnetic gear |
CN110406386B (en) * | 2018-04-26 | 2021-04-02 | 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) | Mechanical guide device for magnetic suspension sledge and magnetic suspension sledge with mechanical guide device |
CN109823192B (en) * | 2019-02-20 | 2024-10-15 | 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) | Magnetic suspension system |
CN111572362A (en) * | 2020-06-17 | 2020-08-25 | 济南尚海流体控制设备有限公司 | Wheel-track type magnetic suspension vehicle system and application thereof |
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2005
- 2005-04-29 CN CNB200510009954XA patent/CN100493948C/en not_active Expired - Fee Related
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Granted publication date: 20090603 Termination date: 20120429 |