CN104118579B - A kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework - Google Patents
A kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework Download PDFInfo
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- CN104118579B CN104118579B CN201410383894.7A CN201410383894A CN104118579B CN 104118579 B CN104118579 B CN 104118579B CN 201410383894 A CN201410383894 A CN 201410383894A CN 104118579 B CN104118579 B CN 104118579B
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Abstract
A kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework; can be used as the attitude control actuator of the Large Spacecraft such as Large-scale satellite, earth observation platform, space station, be made up of four-degree-of-freedom magnetic bearing, high-speed electric expreess locomotive, journal axle integrated transducer, radial transducer, upper protection bearing, lower protection bearing, mandrel, wheel body, base, upper sensor detection ring, lower sensor detection ring, housing, framework mandrel, frame motor, framework, mechanical bearing, position transduser and conducting slip ring.The A end of four-degree-of-freedom magnetic bearing controls radial translation and the deflection of gyro rotor, and the axial translation of gyro rotor is realized by the passive part of four-degree-of-freedom magnetic bearing.Each assembly layout of the present invention is compact, reduces volume and weight, reduces the noise of system, volume and weight, eliminates bearing friction power, thus improves life-span and the control accuracy of single-gimbal control momentum gyro.
Description
Technical field
The present invention relates to a kind of magnetic suspension control moment gyro of single framework, can be used as the attitude control system actuating unit of the Large Spacecraft such as Large-scale satellite, earth observation platform and space station.
Background technology
The attitude control actuator of the Large Spacecraft such as Large-scale satellite, earth observation platform, space station wants that cube is little, lightweight, the life-span is long, low in energy consumption, reliability is high.At present as the control moment gyroscope of spacecraft attitude control system actuating unit, the general mechanical bearing that still adopts supports, and this just fundamentally limits the raising of control moment gyroscope rotating speed, therefore in order to reach required moment of momentum, just have to increase control moment gyroscope weight, increase volume.In addition, there is the problems such as the uncontrollable and zero passage friction moment of mechanical wear, unbalance vibration is large in mechanical bearing, had a strong impact on the service life of control moment gyroscope and the precision of Spacecraft Attitude Control and degree of stability.The existing magnetic suspension control moment gyro of single framework based on magnetic bearing supporting, according to the division of suspension degree of freedom, single degree of freedom magnetic suspension control moment gyro of single framework ~ five degree of freedom magnetic suspension control moment gyro of single framework can be divided into, because suspension degree of freedom is few, control system volume and control moment gyroscope total quality can be reduced, therefore main passive magnetic suspension control moment gyro of single framework obtains and applies comparatively widely, existing four-degree-of-freedom magnetic suspension control moment gyro of single framework adopts two radial direction magnetic bearing supportings, the stator and rotor cores axial length of these two radial direction magnetic bearings is identical, the axis between stators and rotators " dislocation " is utilized to realize the driven suspension of control moment gyroscope rotor, utilize the current control of two radial direction magnetic bearing coils, realize the radial translation of control moment gyroscope rotor and the control of deflection four degree of freedom, but existing structure adopts two radial direction magnetic bearings, axial dimension increases greatly.
Summary of the invention
Technology of the present invention is dealt with problems and is: overcome the deficiencies in the prior art, provides a kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework, to reduce own vol weight and power consumption.
Technical solution of the present invention is: a kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework, by four-degree-of-freedom magnetic bearing (1), high-speed electric expreess locomotive (2), journal axle integrated transducer (3), radial transducer (4), upper protection bearing (5), lower protection bearing (6), mandrel (7), wheel body (8), base (9), upper sensor detection ring (10), lower sensor detection ring (11), housing (12), framework mandrel (13), frame motor (14), framework (15), mechanical bearing (16), position transduser (17) and conducting slip ring (18) composition, wherein four-degree-of-freedom magnetic bearing (1) is positioned at the middle part of control moment gyroscope, its stationary part is arranged on the middle part of mandrel (7), the upper end of four-degree-of-freedom magnetic bearing (1) stator is upper protection bearing (5), upper protection bearing (5) is also fixed on mandrel (7), the radial outside of upper protection bearing (5) is upper sensor detection ring (10), radial portable protective gaps and axial portable protective gaps is formed between upper protection bearing (5) and upper sensor detection ring (10), the radial outside of upper sensor detection ring (10) is journal axle integrated transducer (3), the radial direction of journal axle integrated transducer (3) is popped one's head in and is formed radial direction between axial probe and upper sensor detection ring (10) and detects gap and axial detection gap, journal axle integrated transducer (3) is connected by sensor holder and mandrel (7), the lower end of four-degree-of-freedom magnetic bearing (1) stator is lower protection bearing (6), lower protection bearing (6) is also fixed on mandrel (7), its radial outside is lower sensor detection ring (11), radial portable protective gaps is formed between lower protection bearing (6) and lower sensor detection ring (11), the radial outside of lower sensor detection ring (11) is radial transducer (4), form radial direction between the probe of radial transducer (4) and lower sensor detection ring (11) and detect gap, radial transducer (4) is connected by sensor holder and base (9), the radial outside of the rotor of four-degree-of-freedom magnetic bearing (1) is wheel body (8), both adopt interference fit, the lower end of wheel body (8) is provided with internal rotor iron core and the outer rotor iron core of high-speed electric expreess locomotive (2), magnetic gap is formed between the unshakable in one's determination and outer rotor of the stator of high-speed electric expreess locomotive (2) and internal rotor is unshakable in one's determination, and be fixed on base (9) by connecting panel, housing (12) is connected by screw with base (9), in order to be sealed by wheel body, the two ends of housing (12) are connected with framework mandrel (13), framework mandrel (13) is connected by mechanical bearing (16) and framework (15), one end of framework (15) is connected with the stationary part of frame motor (14), the other end is connected with the stator of position transduser (17), and the stator of position transduser (17) is connected with the stationary part of conducting slip ring (18), the rotor portion of frame motor (14) is connected with framework mandrel (13), and the framework mandrel (13) of the rotor of position transduser (17) and the rotating element of conducting slip ring (18) and the other end is connected.
Described four-degree-of-freedom magnetic bearing (1) is by passive part rotor magnetic guiding loop (101), rotor permanent magnet (102), rotor magnetizer (103), rotor core (104), air gap (105), stator core (106), stator magnetic guiding loop (107), stator permanent magnet (108), coil (109), passive part stator magnetic guiding loop (110) and passive part air gap (111) composition, wherein each stator core (106) is made up of 4 magnetic poles, two stator core (106) composition magnetic bearing 8, upper and lower two ends magnetic poles, form X respectively, the magnetic pole of the positive negative direction of Y-axis, the magnetic pole of each stator core (106) is wound with coil (109), stator core (106) outside is rotor core (104), rotor core (104) outside is rotor magnetizer (103), rotor core (104) inside face and stator core (106) outside face leave certain gap, form air gap (105), the inner radial of stator core (106) is stator magnetic guiding loop (107), two passive part stator magnetic guiding loops (110) are positioned between two stator cores (106), two stator permanent magnets (108) are had between stator core (106) and passive part stator magnetic guiding loop (110), a stator permanent magnet (108) is had between two passive part stator magnetic guiding loops (110), the radially outer of passive part stator magnetic guiding loop (110) is passive part rotor magnetic guiding loop (101), be rotor permanent magnet (102) between two rotor magnetizers (103), certain interval is left between the inside face of passive part rotor magnetic guiding loop (101) and the outside face of passive part stator magnetic guiding loop (110), form passive part air gap (111).
The magnetic pole of described each stator core (106) is wound with coil (109) and controls for independent.
Described rotor permanent magnet (102) and each stator permanent magnet (108) are axial annulus, magnetize vertically, and volume are equal.
Described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are made up of solid domain permeability magnetic material.
Described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are two, four, six or eight.
Described journal axle integrated transducer (3) has the radial direction probe of 4 orthogonal placements and the axial probe of 4 orthogonal placements, axial probe completes the detection of the axial translation of wheel body (8), three generalized displacements of two radial rotatings, the detection of two radial translation generalized displacements of radial wheel body (8) of having popped one's head in.
Described position transduser (17) is magslip, also can be photoelectric code disk.
The principle of such scheme is: the control being completed two radial translations of control moment gyroscope rotor and two radial deflections totally four degree of freedom by the electric current of the magnet coil controlling four-degree-of-freedom magnetic bearing A end in four-degree-of-freedom magnetic suspension control moment gyro of single framework, the rotating part of retentive control moment gyro and stationary part gap uniformity, the passive part of four-degree-of-freedom magnetic bearing realizes the stable suspersion in control moment gyroscope rotor axial direction; Control moment gyroscope wheeling thereof is controlled by high-speed electric expreess locomotive, realize the constant of the angular-momentum vector of high speed rotor, frame motor driver framework mandrel rotates, and then changes the angular-momentum vector direction of high speed rotor, thus the moment achieving magnetic suspension control torque gyroscope exports.Wherein the control principle of four-degree-of-freedom magnetic bearing is: by controlling coil (the i.e. independent electric current controlled in each coil of upper and lower two groups of stator core magnetic poles, that is, " independent control " electric current referred in each coil is not contacted directly, that the detection air gap change detected according to displacement pickup by power amplifier is energized to each magnetic pole of the stator coil), realize the radial translation of magnetic bearing rotating element and radial twisting, stator magnetic guiding loop and the passive part rotor magnetic guiding loop of the passive part in the middle of utilizing realize the axial translation of magnetic bearing rotating element by the magnetic biasing pulling force that longitudinal travel produces.Stator permanent magnet and rotor permanent magnet provide permanent magnet bias magnetic field to magnetic bearing, bear the diametral load suffered by magnetic bearing, the magnetic field that coil produces plays regulatory role, and is used for changing the power often extremely descending magnetic field, keep magnetic bearing rotor air gap even, and make rotor obtain no touch support.Permanent magnetic circuit of the present invention is three parts (as shown in Figure 4), a part is: magnetic flux, from stator permanent magnet N pole, upper end, gets back to the S pole of upper end stator permanent magnet by stator magnetic guiding loop, upper end stator core, upper end air gap, upper end rotor core, upper end rotor magnetizer, upper end passive part rotor magnetic guiding loop, upper end passive part air gap, upper end passive part stator magnetic guiding loop, stator magnetic guiding loop; Part II is: magnetic flux, from stator permanent magnet N pole, lower end, gets back to the S pole of lower end stator permanent magnet by stator magnetic guiding loop, lower end passive part stator magnetic guiding loop, lower end passive part air gap, lower end passive part rotor magnetic guiding loop, lower end rotor magnetizer, lower end rotor core, lower end air gap, lower end stator core, stator magnetic guiding loop; Part III is: magnetic flux is from the stator permanent magnet N pole of centre, by stator magnetic guiding loop, lower end passive part stator magnetic guiding loop, lower end passive part air gap, lower end passive part rotor magnetic guiding loop, lower end rotor magnetizer, rotor permanent magnet S pole, rotor permanent magnet N pole, upper end rotor magnetizer, upper end passive part rotor magnetic guiding loop, upper end passive part air gap, upper end passive part stator magnetic guiding loop, stator magnetic guiding loop, get back to the S pole of intermediate stator permanent magnet.As shown in Figure 3 a and Figure 3 b shows, for the magnetic flux that certain end Y-axis positive dirction coil current produces, its path is: stator core formed Y-axis positive dirction magnetic pole, Y-axis positive dirction air gap to rotor core, then arrive other three direction air gaps, stator core formed other three direction magnetic poles, get back to stator core formation Y-axis positive dirction magnetic pole, formation C/LOOP.
The present invention's advantage is compared with prior art: the present invention utilizes four-degree-of-freedom magnetic bearing to realize the control of magnetic suspension control moment gyro of single framework two radial translations and two radial deflections, and the stator permanent magnet of passive part and rotor permanent magnet realize four-degree-of-freedom magnetic bearing by the raising of dynamic stiffness, A end is not affected, in addition, each stator permanent magnet of the present invention is identical with rotor permanent magnet volume, complete machine residual magnetic moment can be made close to zero, meet the requirement of space flight; Structure axial length of the present invention can be little, overcomes the defect that existing four-degree-of-freedom magnetically levitated flywheel axial length is large; Axial passive part in four-degree-of-freedom magnetic bearing of the present invention is domain structure, and magnetic fluctuation is little, rotates power consumption little.In addition, upper protection bearing of the present invention and lower protection bearing vary in size, and are convenient to the dismounting of the inner wheel body of magnetic suspension control moment gyro of single framework.
Accompanying drawing explanation
Fig. 1 is four-degree-of-freedom magnetic suspension control moment gyro of single framework schematic diagram of the present invention;
Fig. 2 is four-degree-of-freedom magnetic bearing axial section drawing of the present invention;
Fig. 3 a is the four-degree-of-freedom magnetic bearing axial end view drawing of pole shoe form, the four-degree-of-freedom magnetic bearing axial end view drawing that Fig. 3 b is magnetic pole of the stator angle when being 62 degree;
Fig. 4 is the permanent magnetic circuit figure of four-degree-of-freedom magnetic bearing of the present invention;
Fig. 5 is the four-degree-of-freedom magnetic bearing axial section drawing containing four passive part rotor magnetic guiding loops and passive part stator magnetic guiding loop of the present invention;
Fig. 6 is four-degree-of-freedom magnetic suspension control moment gyro of single framework high speed electric machine structure figure of the present invention;
Fig. 7 is the journal axle integrated transducer constructional drawing of four-degree-of-freedom magnetic suspension control moment gyro of single framework of the present invention;
Fig. 8 is the frame motor schematic diagram of four-degree-of-freedom magnetic suspension control moment gyro of single framework of the present invention.
Detailed description of the invention
As shown in Figure 1, a kind of four-degree-of-freedom magnetic suspension control moment gyro of single framework, by four-degree-of-freedom magnetic bearing (1), high-speed electric expreess locomotive (2), journal axle integrated transducer (3), radial transducer (4), upper protection bearing (5), lower protection bearing (6), mandrel (7), wheel body (8), base (9), upper sensor detection ring (10), lower sensor detection ring (11), housing (12), framework mandrel (13), frame motor (14), framework (15), mechanical bearing (16), position transduser (17) and conducting slip ring (18) composition, wherein four-degree-of-freedom magnetic bearing (1) is positioned at the middle part of control moment gyroscope, its stationary part is arranged on the middle part of mandrel (7), the upper end of four-degree-of-freedom magnetic bearing (1) stator is upper protection bearing (5), upper protection bearing (5) is also fixed on mandrel (7), the radial outside of upper protection bearing (5) is upper sensor detection ring (10), radial portable protective gaps and axial portable protective gaps is formed between upper protection bearing (5) and upper sensor detection ring (10), the radial outside of upper sensor detection ring (10) is journal axle integrated transducer (3), the radial direction of journal axle integrated transducer (3) is popped one's head in and is formed radial direction between axial probe and upper sensor detection ring (10) and detects gap and axial detection gap, journal axle integrated transducer (3) is connected by sensor holder and mandrel (7), the lower end of four-degree-of-freedom magnetic bearing (1) stator is lower protection bearing (6), lower protection bearing (6) is also fixed on mandrel (7), its radial outside is lower sensor detection ring (11), radial portable protective gaps is formed between lower protection bearing (6) and lower sensor detection ring (11), the radial outside of lower sensor detection ring (11) is radial transducer (4), form radial direction between the probe of radial transducer (4) and lower sensor detection ring (11) and detect gap, radial transducer (4) is connected by sensor holder and base (9), the radial outside of the rotor of four-degree-of-freedom magnetic bearing (1) is wheel body (8), both adopt interference fit, the lower end of wheel body (8) is provided with internal rotor iron core and the outer rotor iron core of high-speed electric expreess locomotive (2), magnetic gap is formed between the unshakable in one's determination and outer rotor of the stator of high-speed electric expreess locomotive (2) and internal rotor is unshakable in one's determination, and be fixed on base (9) by connecting panel, housing (12) is connected by screw with base (9), in order to be sealed by wheel body, the two ends of housing (12) are connected with framework mandrel (13), framework mandrel (13) is connected by mechanical bearing (16) and framework (15), one end of framework (15) is connected with the stationary part of frame motor (14), the other end is connected with the stator of position transduser (17), and the stator of position transduser (17) is connected with the stationary part of conducting slip ring (18), the rotor portion of frame motor (14) is connected with framework mandrel (13), and the framework mandrel (13) of the rotor of position transduser (17) and the rotating element of conducting slip ring (18) and the other end is connected.
Described four-degree-of-freedom magnetic bearing (1) is by passive part rotor magnetic guiding loop (101), rotor permanent magnet (102), rotor magnetizer (103), rotor core (104), air gap (105), stator core (106), stator magnetic guiding loop (107), stator permanent magnet (108), coil (109), passive part stator magnetic guiding loop (110) and passive part air gap (111) composition, wherein each stator core (106) is made up of 4 magnetic poles, two stator core (106) composition magnetic bearing 8, upper and lower two ends magnetic poles, form X respectively, the magnetic pole of the positive negative direction of Y-axis, the magnetic pole of each stator core (106) is wound with coil (109), stator core (106) outside is rotor core (104), rotor core (104) outside is rotor magnetizer (103), rotor core (104) inside face and stator core (106) outside face leave certain gap, form air gap (105), the inner radial of stator core (106) is stator magnetic guiding loop (107), two passive part stator magnetic guiding loops (110) are positioned between two stator cores (106), two stator permanent magnets (108) are had between stator core (106) and passive part stator magnetic guiding loop (110), a stator permanent magnet (108) is had between two passive part stator magnetic guiding loops (110), the radially outer of passive part stator magnetic guiding loop (110) is passive part rotor magnetic guiding loop (101), be rotor permanent magnet (102) between two rotor magnetizers (103), certain interval is left between the inside face of passive part rotor magnetic guiding loop (101) and the outside face of passive part stator magnetic guiding loop (110), form passive part air gap (111).
The magnetic pole of described each stator core (106) is wound with coil (109) and controls for independent.
Described rotor permanent magnet (102) and each stator permanent magnet (108) are axial annulus, magnetize vertically, and volume are equal.
Described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are made up of solid domain permeability magnetic material.
Described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are two, four, six or eight.
Described journal axle integrated transducer (3) has the radial direction probe of 4 orthogonal placements and the axial probe of 4 orthogonal placements, axial probe completes the detection of the axial translation of wheel body (8), three generalized displacements of two radial rotatings, the detection of two radial translation generalized displacements of radial wheel body (8) of having popped one's head in.
The magnetic pole of described each stator core (106) is wound with coil (109) and controls for independent, control with radial torsion with the radial translation control realizing magnetic bearing rotating element, namely realize magnetic bearing rotating element along two translational degree of freedom controls in x and y direction and two torsional freedoms control (totally four degree of freedom) around x and y direction.
Described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are made up of solid domain permeability magnetic material, are realized the axis stable (namely axial translational degree of freedom is passive) of magnetic bearing by the axile displacement of passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110).
In order to increase the rigidity of passive part, described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are two, four, six or eight, and wherein Fig. 5 gives the four-degree-of-freedom magnetic bearing section drawing that passive part rotor magnetic guiding loop and passive part stator magnetic guiding loop are four.
In addition, in order to reduce the additional displacement negative stiffness that passive part is brought A end, the magnetic resistance of described passive part air gap (111) is 2 ~ 4 times of air gap (105) magnetic resistance.
Described position transduser (17) is magslip, also can be photoelectric code disk.
The invention described above technical scheme passive part rotor magnetic guiding loop (101), rotor magnetizer (103), stator magnetic guiding loop (107) and passive part stator magnetic guiding loop (110) used is solid construction, the good material of magnetic property is adopted to make, as magnetic materials etc. such as electrical pure iron, various carbon steel, cast iron, cast steel, alloy steel, 1J50 and 1J79.Stator core (106) and the good material of rotor core (104) available magnetic property form as the magnetic material punching presses such as electrical pure iron, electrical steel plate DR510, DR470, DW350,1J50 and 1J79 fold.The material of rotor permanent magnet (102) and stator permanent magnet (108) is the rare-earth permanent magnet that magnetic property is good, Nd-Fe-B permanent magnet or ferrite permanent magnet, rotor permanent magnet (102) and stator permanent magnet (108) are axial annulus, magnetize vertically, and rotor permanent magnet (102) and each stator permanent magnet (108) will ensure that volume is equal, the magnetizing direction of each adjacent stator permanent magnet (108) wants contrary, the magnetizing direction of the stator permanent magnet (108) between passive part stator magnetic guiding loop and the magnetizing direction of the rotor permanent magnet (102) between passive part rotor magnetic guiding loop want contrary.After coil (109) adopts the good electromagnetic wire coiling of conduction, paint-dipping drying forms.In addition, the magnetic field produced due to permanent magnet is size variation by the magnetic field that stator core magnetic pole produces in rotor core, therefore eddy current loss can be produced when rotor high-speed rotates, for reducing this part loss, the magnetic pole of stator core (106) should adopt pole shoe form (as shown in Figure 3 a and Figure 3 b shows) to reduce the eddy current loss at a high speed, wherein Fig. 3 a is the end view drawing of pole shoe form, the end view drawing that Fig. 3 b is magnetic pole of the stator angle when being 62 degree, the stator core end face of two kinds of structures carries out choice for use according to different demand, for the magnetic bearing of small volume, structure shown in Fig. 3 b should be adopted, for the magnetic bearing of the slightly large requirement of volume, then should adopt structure shown in Fig. 3 a.Acute angle in Fig. 3 a between stator core magnetic pole root and stator core yoke portion can cause the intensive middle problems of too of magnetic, now can adopt the stator core end view drawing provided in Fig. 3 b, central angle corresponding to the stator core magnetic pole both sides provided in figure is 62 degree, this structure can effectively reduce magnetic that the acute angle between stator core magnetic pole root and stator core yoke portion causes intensive in.
Fig. 6 is high-speed electric expreess locomotive of the present invention (2) axial section, by motor cup-shaped stator (201), motor outer rotor pressing plate (202), outer rotor lamination (203), magnet steel (204), internal rotor lamination (205) and internal rotor pressing plate (206) composition, the radial outside of magnet steel (204) is outer rotor lamination (203), the lower axial end of outer rotor lamination (203) and magnet steel (204) is provided with motor outer rotor pressing plate (202), the radially inner side of magnet steel (204) is internal rotor lamination (205), the lower axial end of internal rotor lamination (205) is provided with internal rotor pressing plate (206).Wherein cup-shaped stator (201) is motor stationary part, all the other are rotating element, cup-shaped stator (201) is positioned between magnet steel (204) and internal rotor lamination (205), is connected by screw and connecting panel and base (9).
Fig. 7 is the schematic diagram of journal axle integrated transducer (3) of the present invention, this displacement pickup is made up of with sensor outer housing (309) two parts pop one's head in (301) ~ probe (308), wherein pop one's head in (301), probe (303), pop one's head in (305) and pop one's head in (307) on axial end respectively along+y, + x,-y and-x evenly places, form axial probe, probe (302), probe (304), pop one's head in (306) and pop one's head in (308) on radial circumference respectively along+y, + x,-y and-x evenly places, form radial probe.Axial probe completes axial translation and two detections around radial rotating three generalized displacements, the detection of radial two radial translation displacements of having popped one's head in.Sensor outer housing (309) shield electromagnetic interference, inside is testing circuit, completes the extraction of rotor displacement information.The modes of emplacement of sensor probe of the present invention is not unique, if ensure 4 radial probe orthogonals and 4 axial probes orthogonal, the relative position of radial probe and axial probe can be any.
Frame motor (14) shown in Fig. 8 is primarily of stator lamination (141), stator winding (142), rotor magnetic steel (143), rotor core (144), rotor press plate (145), wherein stator lamination (141) and stator winding (142) are frame motor stationary part, and all the other are rotating element.Wherein rotor core (144) adopts the good 1J22 bar of magnet conductivity to make.Stator lamination (141) and framework (15) interference fit, rotor magnetic steel (143) and rotor core (144) interference fit, rotor core (144) is connected by interference fit with framework mandrel (13).
The content be not described in detail in specification sheets of the present invention belongs to the known prior art of professional and technical personnel in the field.
Claims (8)
1. a four-degree-of-freedom magnetic suspension control moment gyro of single framework, is characterized in that: by four-degree-of-freedom magnetic bearing (1), high-speed electric expreess locomotive (2), journal axle integrated transducer (3), radial transducer (4), upper protection bearing (5), lower protection bearing (6), mandrel (7), wheel body (8), base (9), upper sensor detection ring (10), lower sensor detection ring (11), housing (12), framework mandrel (13), frame motor (14), framework (15), mechanical bearing (16), position transduser (17) and conducting slip ring (18) composition, wherein four-degree-of-freedom magnetic bearing (1) is positioned at the middle part of control moment gyroscope, its stationary part is arranged on the middle part of mandrel (7), the upper end of four-degree-of-freedom magnetic bearing (1) stator is upper protection bearing (5), upper protection bearing (5) is also fixed on mandrel (7), the radial outside of upper protection bearing (5) is upper sensor detection ring (10), radial portable protective gaps and axial portable protective gaps is formed between upper protection bearing (5) and upper sensor detection ring (10), the radial outside of upper sensor detection ring (10) is journal axle integrated transducer (3), the radial direction of journal axle integrated transducer (3) is popped one's head in and is formed radial direction between axial probe and upper sensor detection ring (10) and detects gap and axial detection gap, journal axle integrated transducer (3) is connected by sensor holder and mandrel (7), the lower end of four-degree-of-freedom magnetic bearing (1) stator is lower protection bearing (6), lower protection bearing (6) is also fixed on mandrel (7), its radial outside is lower sensor detection ring (11), radial portable protective gaps is formed between lower protection bearing (6) and lower sensor detection ring (11), the radial outside of lower sensor detection ring (11) is radial transducer (4), form radial direction between the probe of radial transducer (4) and lower sensor detection ring (11) and detect gap, radial transducer (4) is connected by sensor holder and base (9), the radial outside of the rotor of four-degree-of-freedom magnetic bearing (1) is wheel body (8), both adopt interference fit, the lower end of wheel body (8) is provided with internal rotor iron core and the outer rotor iron core of high-speed electric expreess locomotive (2), magnetic gap is formed between the unshakable in one's determination and outer rotor of the stator of high-speed electric expreess locomotive (2) and internal rotor is unshakable in one's determination, and be fixed on base (9) by connecting panel, housing (12) is connected by screw with base (9), in order to be sealed by wheel body, the two ends of housing (12) are connected with framework mandrel (13), framework mandrel (13) is connected by mechanical bearing (16) and framework (15), one end of framework (15) is connected with the stationary part of frame motor (14), the other end is connected with the stator of position transduser (17), and the stator of position transduser (17) is connected with the stationary part of conducting slip ring (18), the rotor portion of frame motor (14) is connected with framework mandrel (13), and the framework mandrel (13) of the rotor of position transduser (17) and the rotating element of conducting slip ring (18) and the other end is connected.
2. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 1, it is characterized in that: described four-degree-of-freedom magnetic bearing (1) is by passive part rotor magnetic guiding loop (101), rotor permanent magnet (102), rotor magnetizer (103), rotor core (104), air gap (105), stator core (106), stator magnetic guiding loop (107), stator permanent magnet (108), coil (109), passive part stator magnetic guiding loop (110) and passive part air gap (111) composition, wherein each stator core (106) is made up of 4 magnetic poles, two stator core (106) composition magnetic bearing 8, upper and lower two ends magnetic poles, form X respectively, the magnetic pole of the positive negative direction of Y-axis, the magnetic pole of each stator core (106) is wound with coil (109), stator core (106) outside is rotor core (104), rotor core (104) outside is rotor magnetizer (103), rotor core (104) inside face and stator core (106) outside face leave certain gap, form air gap (105), the inner radial of stator core (106) is stator magnetic guiding loop (107), two passive part stator magnetic guiding loops (110) are positioned between two stator cores (106), two stator permanent magnets (108) are had between stator core (106) and passive part stator magnetic guiding loop (110), a stator permanent magnet (108) is had between two passive part stator magnetic guiding loops (110), the radially outer of passive part stator magnetic guiding loop (110) is passive part rotor magnetic guiding loop (101), be rotor permanent magnet (102) between two rotor magnetizers (103), certain interval is left between the inside face of passive part rotor magnetic guiding loop (101) and the outside face of passive part stator magnetic guiding loop (110), form passive part air gap (111).
3. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 2, is characterized in that: the magnetic pole of described each stator core (106) is wound with coil (109) and controls for independent.
4. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 2, it is characterized in that: described rotor permanent magnet (102) and each stator permanent magnet (108) are axial annulus, magnetize vertically, and volume is equal.
5. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 2, is characterized in that: described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are made up of solid domain permeability magnetic material.
6. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 2, is characterized in that: described passive part rotor magnetic guiding loop (101) and passive part stator magnetic guiding loop (110) are two, four, six or eight.
7. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 1, it is characterized in that: described journal axle integrated transducer (3) has the radial direction probe of 4 orthogonal placements and the axial probe of 4 orthogonal placements, axial probe completes the detection of the axial translation of wheel body (8), three generalized displacements of two radial rotatings, the detection of two radial translation generalized displacements of radial wheel body (8) of having popped one's head in.
8. four-degree-of-freedom magnetic suspension control moment gyro of single framework according to claim 1, is characterized in that: described position transduser (17) is for magslip or for photoelectric code disk.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN104908978B (en) * | 2015-06-05 | 2017-01-11 | 北京航空航天大学 | Five-degree-of-freedom gyro case structure |
| CN105292395B (en) * | 2015-10-29 | 2017-10-27 | 上海矶怃科技有限公司 | A kind of gyrostabilizer peculiar to vessel and its subtract and shake gyrorotor system |
| CN106556385B (en) * | 2016-10-20 | 2019-10-22 | 北京控制工程研究所 | A kind of Novel control moment gyro frame assembly structure |
| CN107741746B (en) * | 2017-10-13 | 2020-10-16 | 北京航空航天大学 | Frame system for control moment gyroscope |
| CN107792397B (en) * | 2017-10-16 | 2020-08-04 | 北京航空航天大学 | Full non-contact double-frame magnetic suspension control moment gyroscope |
| CN109515755B (en) * | 2018-11-26 | 2021-09-17 | 北京航空航天大学 | Five-freedom-degree single-frame magnetic suspension control moment gyroscope |
| CN109597438B (en) * | 2018-11-30 | 2021-09-24 | 上海航天控制技术研究所 | Control moment gyro |
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| US4732353A (en) * | 1985-11-07 | 1988-03-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Three axis attitude control system |
| CN101049861A (en) * | 2007-04-16 | 2007-10-10 | 北京航空航天大学 | Completely non - contacting magnetic suspension control moment gyro of single framework |
| CN101049860A (en) * | 2007-04-16 | 2007-10-10 | 北京航空航天大学 | Single end support type magnetic suspension control moment gyro of single framework |
| CN101219714A (en) * | 2007-12-26 | 2008-07-16 | 北京航空航天大学 | Double-frame magnetic suspension control moment gyro |
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| CN101049861A (en) * | 2007-04-16 | 2007-10-10 | 北京航空航天大学 | Completely non - contacting magnetic suspension control moment gyro of single framework |
| CN101049860A (en) * | 2007-04-16 | 2007-10-10 | 北京航空航天大学 | Single end support type magnetic suspension control moment gyro of single framework |
| CN101219714A (en) * | 2007-12-26 | 2008-07-16 | 北京航空航天大学 | Double-frame magnetic suspension control moment gyro |
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