CN205593528U - Many rotor crafts erection equipment - Google Patents
Many rotor crafts erection equipment Download PDFInfo
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- CN205593528U CN205593528U CN201620048531.2U CN201620048531U CN205593528U CN 205593528 U CN205593528 U CN 205593528U CN 201620048531 U CN201620048531 U CN 201620048531U CN 205593528 U CN205593528 U CN 205593528U
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- horn
- clamping limb
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 10
- 238000009434 installation Methods 0.000 abstract description 10
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 9
- 238000000034 method Methods 0.000 description 3
- 238000011900 installation process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 239000012780 transparent material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
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Abstract
The utility model relates to a many rotor crafts erection equipment belongs to the aircraft and makes technical field. The utility model discloses draw together perpendicular projection arrangement, horizontal projection arrangement, laser projection arrangement, triaxial swivel work head, perpendicular projection arrangement includes perpendicular projection arrangement base, rag bolt, perpendicular projection arrangement support, centre gripping arm, back timber, a T type bubble chi, bubble chi mounting panel, front outline board, the horizontal projection device includes horizontal projection device lower margin, horizontal projection device support, adjusting nut, roof, scale plate, the laser projection device is including rotatory laser device, motor correction laser device, horn correction laser device, the central laser device rectified, triaxial swivel work head includes Z axle revolving stage, X axle revolving stage, Y axle revolving stage, mounting platform. The utility model discloses can realize the accurate installation and the position survey of fire hole of many rotor crafts motor and horn, for having improved production efficiency, improve product quality and lay the basis.
Description
Technical field
This utility model relates to a kind of multi-rotor aerocraft and installs equipment, belongs to aircraft manufacture technical field.
Background technology
Current relatively large multi-rotor aerocraft installs production wastes time and energy, when determining mounting position of motor and horn setting angle, lack the technological equipment of necessity, the number of axle of multi-rotor aerocraft is generally more than four, require during installation that the motor output shaft axis of multi-rotor aerocraft is perpendicular to mounting plane, and require that each motor output shaft axis is equal with the centre distance of aircraft, require to be uniformly distributed on the motor circular arc with aircraft center as the center of circle, require that the angle between all horns and the mounting plane of multi-rotor aerocraft is consistent and meets design requirement, according to requirements above, technological equipment designed by this utility model and process can realize multi-rotor aerocraft motor and horn is accurately installed, and position dimension is measured relatively.
Summary of the invention
The purpose of this utility model is: for the problem of above-mentioned existence, it is provided that a kind of motor that disclosure satisfy that multi-rotor aerocraft and horn installation site adjust, and the technological equipment of position measurement.
Technical solutions of the utility model are: a kind of multi-rotor aerocraft installs equipment, including upright projection device 1, floor projection device 2, laser projection device 3, three axle rotary table 4；
Described upright projection device 1 includes upright projection device pedestal 5, foundation bolt 6, upright projection appliance stand 7, clamping limb 8, back timber the 9, first T-shaped bubble chi 11, bubble chi installing plate 12, upright projection plate 13；Described foundation bolt 6 is supported on the ground by the screwed hole of upright projection device pedestal 5, described upright projection appliance stand 7 is arranged on upright projection device pedestal 5, described clamping limb 8 is arranged on upright projection appliance stand 7, described back timber 9 is arranged on upright projection appliance stand 7 top, described first T-shaped bubble chi 11 is arranged on bubble chi installing plate 12, described bubble chi installing plate 12 is arranged on upright projection plate 13, described upright projection plate 13 is lifted on the hook 52 of back timber 9, clamping limb contact surface 47 side of described clamping limb 8 leans against on upright projection plate 13；Adjustably foot bolt 6 makes the bubble on the first T-shaped bubble chi 11 in an intermediate position, and hook 52 makes upright projection plate 13 be in overhang, and the locked position of regulation clamping limb 8, while making upright projection plate 13 keep overhang so that it is fixing；
Described floor projection device 2 includes floor projection device lower margin 14, floor projection appliance stand 15, adjusting nut 16, top board 17, graduated tile 18；Described floor projection device lower margin 14 is placed on work ground, described floor projection appliance stand 15 is arranged on described floor projection device lower margin 14, described adjusting nut 16 is arranged on floor projection appliance stand 15, described top board 17 is arranged on floor projection appliance stand 15 and adjusting nut 16, described graduated tile 18 is placed on top board 17, and the second T-shaped bubble chi 11 is placed on top board 17；Top board 17 uses transparent material, makes laser rays can penetrate top board 17 and be radiated on graduated tile 18, and graduated tile 18 uses trnaslucent materials so that laser rays can produce clear projection；
Described laser projection device 3 includes rotation correction laser aid 10, motor calibration laser aid 19, horn calibration of laser device 20, central laser device 27；Described rotation correction laser aid 10 is arranged on upright projection plate 13, described motor calibration laser aid 19 is arranged on the motor 34 of multi-rotor aerocraft 22, described horn calibration of laser device 20 is arranged on the horn 35 of multi-rotor aerocraft 22, and described central laser device 27 is arranged on the Y-axis turntable 25 of three axle rotary tables 4；
Described three axle rotary tables 4 include Z axis turntable 23, X-axis turntable 24, Y-axis turntable 25, mounting platform 26；Described X-axis turntable 24 is arranged on Z axis turntable 23, described Y-axis turntable 25 is arranged on X-axis turntable 24, described mounting platform 26 is arranged on Y-axis turntable 25, and three axle rotary tables 4 can realize multi-rotor aerocraft 22 and carry out 360 degree of rotations about the z axis, make mounting platform 26 holding level；
Described motor calibration laser aid 19 includes axle bed 28, laser stent 29；Described axle bed 28 is arranged on motor 34 output shaft, and described laser stent 29 is arranged on axle bed 28, described laser stent 29 is provided with the first clamper 30, described first clamper 30 is provided with the first cross laser device 31；First clamper 30 ensures that the laser axis that the first cross laser device 31 sends is coaxial with motor 34 output shaft；
Described horn calibration of laser device 20 includes seat 33 under the horn corrector seat of honour 32 and horn corrector；Under the described horn corrector seat of honour 32 and horn corrector, seat 33 is linked by bolt, it is clamped on horn 35, on the described horn corrector seat of honour 32, second clamper 30 is installed, on described second clamper 30, second cross laser device 31 is installed, under the horn corrector seat of honour 32 and horn corrector, seat 33 is clamped on horn 35, it is possible to adjust position around horn 35；
Described rotation correction laser aid 10 includes rotary laser base 44, rotary laser swing arm 45, described rotary laser swing arm 45 passes through hinge links with rotary laser base 44, in described rotary laser swing arm 45, the 3rd clamper 30 is installed, on described 3rd clamper 30, the 3rd cross laser device 31 is installed, clamping screw on regulation hinge, make to keep between rotary laser swing arm 45 and rotary laser base 44 enough frictional force, when making to manually adjust rotary laser swing arm 45, adjust rotary laser swing arm 45 and can rest on any position；
Described central laser device 27, with central laser base 43, described central laser base 43 is provided with the 4th clamper 30, described 4th clamper 30 is provided with the 4th cross laser device 31.
The adjustment mode of upright projection device described in the utility model is:
Adjust the position of bubble chi installing plate 12 so that bubble chi installing plate guiding ruler 40 overlaps with the horizontal scale line 59 of upright projection plate 13；Adjust the back timber 9 rigging position on upright projection appliance stand 7, the clamping screw in locking back timber screwed hole 53 so that in the first T-shaped bubble chi 11 on bubble chi installing plate 12, bubble 39 is positioned at centre；Ensure that horizontal scale line 59 is horizontal；
Adjust position and the angle of rotary laser swing arm 45 of rotation correction laser aid 10 so that one article in two articles of laser rays that the 3rd cross laser device 31 being arranged on rotation correction laser aid 10 is incident upon on upright projection plate 13 overlaps with the horizontal scale line 59 of upright projection plate 13；One article that on guarantee rotation correction laser aid 10, the 3rd cross laser device 31 of installation sends in two articles of laser rays parallel with upright projection plate 13；
The adjustment mode of floor projection device described in the utility model is:
nullAdjusting nut 16 is adjusted to correct position，Bubble 39 in the on top board 17 second T-shaped bubble chi 11 is made to be positioned at centre，Ensure that top board 17 is in horizontal plane，Then graduated tile 18 is placed on top board 17，Second T-shaped bubble chi 11 is placed on Y-axis turntable 25，Regulation handle on regulation Y-axis turntable 25，Bubble 39 in the second T-shaped bubble chi 11 is made to be positioned at centre，Ensure mounting plane and mounting platform 26 level of Y-axis turntable 25，Then the second T-shaped bubble chi 11 is taken off，Central laser device 27 is placed on the centre of Y-axis turntable 25，Open the 4th cross laser device 31 on central laser device 27，Top board 17 projects，Make laser rays vertical with top board edge，And the graduated tile angle line 54 of graduated tile 18 is overlapped with laser rays，Graduated tile center 57 is overlapped with projection centre；Ensure that the axis by graduated tile center 57 is vertical with graduated tile 18 passes through mounting platform 26 center；
Multi-rotor aerocraft mounting position of motor described in the utility model adjusts mode:
Adjust installation site and the motor calibration laser aid 19 of motor 34, and the second cross laser device 31 on horn calibration of laser device 20, make the longitudinal axis laser rays 62 that each second cross laser device 31 projects on graduated tile 18 all by graduated tile center 57, and overlap with graduated tile angle line 54, then the installation site of all motors 34 is adjusted, make the transverse axis laser rays 63 projecting on graduated tile 18 tangent with same graduated tile concentric circular 55, ensure that the axial line distance graduated tile center 57 of each motor 34 is apart from identical, and make this laser rays length in both sides, point of contact equal；Ensure that motor 34 axis is vertical with top board 17；
Multi-rotor aerocraft horn setting angle metering system described in the utility model is:
Adjust rotary laser swing arm 45 angle on rotation correction laser aid 10, and adjust the position of upright projection device 1, make to be arranged on the rotary laser projection line 61 that on rotation correction laser aid 10, the 3rd cross laser device 31 is incident upon on graduated tile 18 and pass graduated tile center 57, and overlap with graduated tile axis 56, it is ensured that the vertical plane 60 at upright projection plate 13 place is parallel with graduated tile axis 56；
Repeatedly adjust Z axis turntable 23, the longitudinal axis laser rays 62 making each motor calibration laser aid 19 on multi-rotor aerocraft 22 project on graduated tile 18 projects rotary laser projection line 61 with rotation correction laser aid 10 respectively and overlaps, the most repeatedly adjust horn calibration of laser device 20, the laser rays that the second cross laser device 31 being arranged on horn calibration of laser device 20 is cast out intersects with horizontal scale line 59 on upright projection plate 13, and usage amount hornwork measures angle；Adjusting a horn 35 parallel with upright projection plate 13 every time, measure the angle between a horn 35 and horizontal scale line 59, this angle is equal to the angle between horn 35 and aircraft lower cover 37；
Described mounting platform 26 is provided with clamp 21, multi-rotor aerocraft 22 is clamped on mounting platform 26 by clamp 21, one jaw clamping aircraft upper cover 36 of clamp 21, the bottom surface of another jaw clamping mounting platform 26 of clamp 21, when clamp 21 clamps, ensure by aircraft lower cover 37 center, and the axis vertical with aircraft lower cover 37 installed surface with by mounting platform 26 center the dead in line vertical with the installed surface of mounting platform 26.
Described clamping limb 8 is with clamping limb screwed hole 46, described clamping limb 8 is with clamping limb contact surface 47, upright projection plate 13 leans against on clamping limb contact surface 47, described clamping limb 8 is with clamping limb open slot 48, described clamping limb 8 is with clamping limb installing hole 49, upright projection appliance stand 7 is through clamping limb installing hole 49, and described clamping limb 8, with clamping limb locking screw pit 50, uses lock-screw to be locked on upright projection appliance stand 7 by clamping limb 8 by clamping limb locking screw pit 50.
Described back timber 9 is with back timber installing hole 51, and upright projection appliance stand 7 is through back timber installing hole 51, and described back timber 9 is with hook 52, and described back timber 9 is with back timber screwed hole 53.
Described graduated tile 18 is with graduated tile angle line 54, and described graduated tile 18 is with graduated tile concentric circular 55.
Described upright projection plate 13 is with upright projection plate hanging hole 58, and described upright projection plate 13 is with horizontal scale line 59.
With mounting platform boss 41 on described mounting platform 26, the aircraft lower cover 37 of described multi-rotor aerocraft 22 contacts with mounting platform boss 41, with central laser base boss 42 on the central laser base 43 of described central laser device 27, it is ensured that central laser base 43 and the contact precision of Y-axis turntable 25；Described T-shaped bubble chi base band is magnetic, and it can be made to be conveniently installed on Y-axis turntable 25 and bubble chi installing plate 12, and described mounting platform boss 41 ensures the good contact between aircraft lower cover 37 and mounting platform 26.
Work process of the present utility model is:
Upright projection device installation process: bubble chi installing plate 12 is arranged on upright projection plate 13, bubble chi installing plate guiding ruler 40 is alignd with horizontal scale line 59, the regulation back timber 9 position in upright projection appliance stand 7, the most adjustably foot bolt 6, the bubble 39 making the on bubble chi installing plate 12 first T-shaped bubble chi 11 is positioned at centre, when upright projection plate 13 only pendency, regulation clamping limb 8, clamping limb contact surface 47 is contacted with upright projection plate 13, screw the bolt in clamping limb screwed hole 46, clamping upright projection plate 13, upright projection plate 13 is installed rotation correction laser aid 10, adjust rotary laser swing arm 45, the laser rays that 3rd cross laser device 31 is cast out overlaps with horizontal scale line 59；
Floor projection device installation process: install an adjusting nut 16 on each floor projection device lower margin, top board 17 is penetrated the threaded portion on floor projection device lower margin, top board 17 is placed two T-shaped bubble chis and adjusts adjusting nut, make the bubble in T-shaped bubble chi in an intermediate position, one adjusting nut is installed on each floor projection device lower margin again, and locks；T-shaped bubble chi is placed at the Y-axis turntable center of three axle rotary tables, adjust X-axis turntable and Y-axis turntable, make the bubble in T-shaped bubble chi in an intermediate position, locking and regulating device, take off the T-shaped bubble chi of Y-axis turntable center, put into central laser device, cross laser device in regulation central laser device, make its laser rays projected on top board vertical in top board edge, graduated tile is placed on top board, adjust the position of graduated tile, make the laser rays center superposition that the cross laser device on graduated tile Center-to-Center laser aid projects, and graduated tile axis is overlapped with laser rays；
Horn setting angle is measured: be placed on mounting platform by the aircraft lower cover of multi-rotor aerocraft, clamp is used to clamp aircraft upper cover 36 and mounting platform, adjust the motor calibration laser aid being arranged on motor and the horn calibration of laser device being arranged on horn, the laser rays making cross laser device mounted thereto project on graduated tile overlaps, and rotational Z-axis turntable workbench, make laser rays and graduated tile axis that the laser instrument on tested horn projects, then horn calibration of laser device is rotated, the laser rays that the laser instrument of horn calibration of laser device is projected intersects with the horizontal scale line on upright projection plate, bevel protractor is used to measure the angle of cut, i.e. obtain horn setting angle.
Mounting position of motor adjusts: adjust all mounting position of motors, the longitudinal axis laser rays making the cross laser device being arranged on motor calibration laser aid projection overlaps with graduated tile angle line, and be uniformly distributed with graduated tile center so that transverse axis laser rays is tangent with same graduated tile concentric circular.
The beneficial effects of the utility model are: this utility model can realize accurately installation and the position measurement of multi-rotor aerocraft motor and horn, for improve production efficiency, improve product quality and lay the first stone.
Accompanying drawing explanation
Fig. 1 is overall axle geodesic structure schematic diagram of the present utility model；
Fig. 2 is this utility model upright projection apparatus structure schematic diagram；
Fig. 3 is this utility model floor projection apparatus structure schematic diagram；
Fig. 4 is that this utility model removes vertically and horizontally projection arrangement structural representation；
Fig. 5 is the rotary table structural representation that this utility model installs T-shaped bubble chi；
Fig. 6 is the rotary table structural representation that this utility model installs central laser device；
Fig. 7 is this utility model motor calibration laser aid and horn calibration of laser apparatus structure schematic diagram；
Fig. 8 is this utility model multi-rotor aerocraft structural representation；
Fig. 9 is this utility model T-shaped bubble chi structural representation；
Figure 10 is this utility model bubble chi installing plate guiding ruler structural representation；
Figure 11 is this utility model mounting platform structural representation；
Figure 12 is this utility model central laser apparatus structure schematic diagram；
Figure 13 is this utility model rotation correction laser device structure schematic diagram；
Figure 14 is this utility model clamping limb structural representation；
Figure 15 is this utility model beam structure schematic diagram；
Figure 16 is this utility model graduated tile structural representation；
Figure 17 is this utility model upright projection plate structure schematic diagram；
Figure 18 is that this utility model is installed and location method schematic diagram.
nullEach label in Fig. 1-18: 1-upright projection device，2-floor projection device，3-laser projection device，4-tri-axle rotary table，5-upright projection device pedestal，6-foundation bolt，7-upright projection appliance stand，8-clamping limb，9-back timber，10-rotation correction laser aid，11-T type bubble chi，12-bubble chi installing plate，13-upright projection plate，14-floor projection device lower margin，15-floor projection appliance stand，16-adjusting nut，17-top board，18-graduated tile，19-motor calibration laser aid，20-horn calibration of laser device，21-clamp，22-multi-rotor aerocraft，23-Z axle turntable，24-X axle turntable，25-Y axle turntable，26-mounting platform，27-central laser device，28-axle bed，29-laser stent，30-clamper，31-cross laser device，The 32-horn corrector seat of honour，Seat under 33-horn corrector，34-motor，35-horn，36-aircraft upper cover，37-aircraft lower cover，38-T type bubble chi base，39-bubble，40-bubble chi installing plate guiding ruler，41-mounting platform boss，42-central laser base boss，43-central laser base，44-rotary laser base，45-rotary laser swing arm，46-clamping limb screwed hole，47-clamping limb contact surface，48-clamping limb open slot，49-clamping limb installing hole，50-clamping limb locking screw pit，51-back timber installing hole，52-links up with，53-back timber screwed hole，54-graduated tile angle line，55-graduated tile concentric circular，56-graduated tile axis，57-graduated tile center，58-upright projection plate hanging hole，59-horizontal scale line，60-vertical plane，61-rotary laser projection line，62-longitudinal axis laser rays，63-transverse axis laser rays.
Detailed description of the invention
Below in conjunction with the accompanying drawings and specific embodiment, the utility model is described in further detail.
Embodiment 1: as it is shown in figure 1, a kind of multi-rotor aerocraft installs equipment, including upright projection device 1, floor projection device 2, laser projection device 3, three axle rotary table 4；
As shown in Figure 2, a kind of multi-rotor aerocraft installs equipment, and described upright projection device 1 includes upright projection device pedestal 5, foundation bolt 6, upright projection appliance stand 7, clamping limb 8, back timber the 9, first T-shaped bubble chi 11, bubble chi installing plate 12, upright projection plate 13；Described foundation bolt 6 is supported on the ground by the screwed hole of upright projection device pedestal 5, described upright projection appliance stand 7 is arranged on upright projection device pedestal 5, described clamping limb 8 is arranged on upright projection appliance stand 7, described back timber 9 is arranged on upright projection appliance stand 7 top, described first T-shaped bubble chi 11 is arranged on bubble chi installing plate 12, described bubble chi installing plate 12 is arranged on upright projection plate 13, described upright projection plate 13 is lifted on the hook 52 of back timber 9, clamping limb contact surface 47 side of described clamping limb 8 leans against on upright projection plate 13；Adjustably foot bolt 6 makes the bubble on the first T-shaped bubble chi 11 in an intermediate position, and hook 52 makes upright projection plate 13 be in overhang, and the locked position of regulation clamping limb 8, while making upright projection plate 13 keep overhang so that it is fixing；
The adjustment mode of described upright projection device is:
Adjust position and the angle of rotary laser swing arm 45 of rotation correction laser aid 10 so that one article in two articles of laser rays that the 3rd cross laser device 31 being arranged on rotation correction laser aid 10 is incident upon on upright projection plate 13 overlaps with the horizontal scale line 59 of upright projection plate 13；One article that on guarantee rotation correction laser aid 10, the 3rd cross laser device 31 of installation sends in two articles of laser rays parallel with upright projection plate 13；
Adjust the position of bubble chi installing plate 12 so that bubble chi installing plate guiding ruler 40 overlaps with the horizontal scale line 59 of upright projection plate 13；Adjust the back timber 9 rigging position on upright projection appliance stand 7, the clamping screw in locking back timber screwed hole 53 so that in the first T-shaped bubble chi 11 on bubble chi installing plate 12, bubble 39 is positioned at centre；Ensure that horizontal scale line 59 is horizontal；
As it is shown on figure 3, a kind of multi-rotor aerocraft installs equipment, described floor projection device 2 includes floor projection device lower margin 14, floor projection appliance stand 15, adjusting nut 16, top board 17, graduated tile 18；Described floor projection device lower margin 14 is placed on work ground, described floor projection appliance stand 15 is arranged on described floor projection device lower margin 14, described adjusting nut 16 is arranged on floor projection appliance stand 15, described top board 17 is arranged on floor projection appliance stand 15 and adjusting nut 16, described graduated tile 18 is placed on top board 17, and described second T-shaped bubble chi 11 is placed on top board 17；Top board 17 uses transparent material, makes laser rays can penetrate top board 17 and be radiated on graduated tile 18, and graduated tile 18 uses trnaslucent materials so that laser rays can produce clear projection；
As shown in Figure 4, a kind of multi-rotor aerocraft installs equipment, and described laser projection device 3 includes rotation correction laser aid 10, motor calibration laser aid 19, horn calibration of laser device 20, central laser device 27；Described rotation correction laser aid 10 is arranged on upright projection plate 13, described motor calibration laser aid 19 is arranged on the motor 34 of multi-rotor aerocraft 22, described horn calibration of laser device 20 is arranged on the horn 35 of multi-rotor aerocraft 22, and described central laser device 27 is arranged on the Y-axis turntable 25 of three axle rotary tables 4；
Described mounting platform 26 is provided with clamp 21, multi-rotor aerocraft 22 is clamped on mounting platform 26 by clamp 21, one jaw clamping aircraft upper cover 36 of clamp 21, the bottom surface of another jaw clamping mounting platform 26 of clamp 21, when clamp 21 clamps, ensure by aircraft lower cover 37 center, and the axis vertical with aircraft lower cover 37 installed surface with by mounting platform 26 center the dead in line vertical with the installed surface of mounting platform 26.
As it is shown in figure 5, a kind of multi-rotor aerocraft installs equipment, described three axle rotary tables 4 include Z axis turntable 23, X-axis turntable 24, Y-axis turntable 25, mounting platform 26；Described X-axis turntable 24 is arranged on Z axis turntable 23, described Y-axis turntable 25 is arranged on X-axis turntable 24, described mounting platform 26 is arranged on Y-axis turntable 25, and three axle rotary tables 4 can realize multi-rotor aerocraft 22 and carry out 360 degree of rotations about the z axis, make mounting platform 26 holding level；
As shown in Fig. 3, Fig. 5, Fig. 6, a kind of multi-rotor aerocraft installs equipment, and the adjustment mode of floor projection device described in the utility model is:
nullAdjusting nut 16 is adjusted to correct position，Bubble 39 in the on top board 17 second T-shaped bubble chi 11 is made to be positioned at centre，Ensure that top board 17 is in horizontal plane，Then graduated tile 18 is placed on top board 17，Second T-shaped bubble chi 11 is placed on Y-axis turntable 25，Regulation handle on regulation Y-axis turntable 25，Bubble 39 in the second T-shaped bubble chi 11 is made to be positioned at centre，Ensure mounting plane and mounting platform 26 level of Y-axis turntable 25，Then the second T-shaped bubble chi 11 is taken off，Central laser device 27 is placed on the centre of Y-axis turntable 25，Open the 4th cross laser device 31 on central laser device 27，Top board 17 projects，Make laser rays vertical with top board edge，And the graduated tile angle line 54 of graduated tile 18 is overlapped with laser rays，Graduated tile center 57 is overlapped with projection centre；Ensure that the axis by graduated tile center 57 is vertical with graduated tile 18 passes through mounting platform 26 center；
As it is shown in fig. 7, a kind of multi-rotor aerocraft installs equipment, described motor calibration laser aid 19 includes axle bed 28, laser stent 29；Described axle bed 28 is arranged on motor 34 output shaft, and described laser stent 29 is arranged on axle bed 28, described laser stent 29 is provided with the first clamper 30, described first clamper 30 is provided with the first cross laser device 31；First clamper 30 ensures that the laser axis that the first cross laser device 31 sends is coaxial with motor 34 output shaft；
Described horn calibration of laser device 20 includes seat 33 under the horn corrector seat of honour 32 and horn corrector；Under the described horn corrector seat of honour 32 and horn corrector, seat 33 is linked by bolt, it is clamped on horn 35, on the described horn corrector seat of honour 32, second clamper 30 is installed, on described second clamper 30, second cross laser device 31 is installed, under the horn corrector seat of honour 32 and horn corrector, seat 33 is clamped on horn 35, it is possible to adjust position around horn 35；
As shown in Figure 8, a kind of multi-rotor aerocraft installs equipment, and multi-rotor aerocraft includes motor 34, horn 35, aircraft upper cover 36, aircraft lower cover 37, and aircraft lower cover 37 bottom surface is pressed on the mounting platform boss 41 on mounting platform 26 by clamp 21.
As it is shown in figure 9, a kind of multi-rotor aerocraft installs equipment, T-shaped bubble chi base 38 is that band is magnetic.
As shown in Figure 10, a kind of multi-rotor aerocraft installs equipment, and bubble chi installing plate 12 is with bubble chi installing plate guiding ruler 40.
As shown in figure 11, a kind of multi-rotor aerocraft installs equipment, with mounting platform boss 41 on described mounting platform 26, the aircraft lower cover 37 of described multi-rotor aerocraft 22 contacts with mounting platform boss 41, with central laser base boss 42 on the central laser base 43 of described central laser device 27, it is ensured that central laser base 43 and the contact precision of Y-axis turntable 25；Described T-shaped bubble chi base band is magnetic, and it can be made to be conveniently installed on Y-axis turntable 25 and bubble chi installing plate 12, and described mounting platform boss 41 ensures the good contact between aircraft lower cover 37 and mounting platform 26.
As shown in figure 12, a kind of multi-rotor aerocraft installs equipment, and described central laser device 27, with central laser base 43, described central laser base 43 is provided with the 4th clamper 30, described 4th clamper 30 is provided with the 4th cross laser device 31.
As shown in figure 13, a kind of multi-rotor aerocraft installs equipment, described rotation correction laser aid 10 includes rotary laser base 44, rotary laser swing arm 45, described rotary laser swing arm 45 passes through hinge links with rotary laser base 44, in described rotary laser swing arm 45, the 3rd clamper 30 is installed, on described 3rd clamper 30, the 3rd cross laser device 31 is installed, clamping screw on regulation hinge, make to keep between rotary laser swing arm 45 and rotary laser base 44 enough frictional force, when making to manually adjust rotary laser swing arm 45, adjust rotary laser swing arm 45 and can rest on any position；
As shown in figure 14, a kind of multi-rotor aerocraft installs equipment, described clamping limb 8 is with clamping limb screwed hole 46, described clamping limb 8 is with clamping limb contact surface 47, upright projection plate 13 leans against on clamping limb contact surface 47, described clamping limb 8 is with clamping limb open slot 48, described clamping limb 8 is with clamping limb installing hole 49, upright projection appliance stand 7 is through clamping limb installing hole 49, described clamping limb 8, with clamping limb locking screw pit 50, uses lock-screw to be locked on upright projection appliance stand 7 by clamping limb 8 by clamping limb locking screw pit 50.
As shown in figure 15, a kind of multi-rotor aerocraft installs equipment, and described back timber 9 is with back timber installing hole 51, and upright projection appliance stand 7 is through back timber installing hole 51, and described back timber 9 is with hook 52, and described back timber 9 is with back timber screwed hole 53.
As shown in figure 16, a kind of multi-rotor aerocraft installs equipment, and described graduated tile 18 is with graduated tile angle line 54, and described graduated tile 18 is with graduated tile concentric circular 55.Described graduated tile 18 is with graduated tile axis 56 and graduated tile center 57；
As shown in figure 17, a kind of multi-rotor aerocraft installs equipment, and described upright projection plate 13 is with upright projection plate hanging hole 58, and described upright projection plate 13 is with horizontal scale line 59.
As shown in figure 18, a kind of multi-rotor aerocraft installs equipment, and multi-rotor aerocraft mounting position of motor described in the utility model adjusts mode and is:
Adjust installation site and the motor calibration laser aid 19 of motor 34, and the second cross laser device 31 on horn calibration of laser device 20, make the longitudinal axis laser rays 62 that each second cross laser device 31 projects on graduated tile 18 all by graduated tile center 57, and overlap with graduated tile angle line 54, then the installation site of all motors 34 is adjusted, make the transverse axis laser rays 63 projecting on graduated tile 18 tangent with same graduated tile concentric circular 55, ensure that the axial line distance graduated tile center 57 of each motor 34 is apart from identical, and make this laser rays length in both sides, point of contact equal；Ensure that motor 34 axis is vertical with top board 17；
Multi-rotor aerocraft horn setting angle metering system described in the utility model is:
Adjust rotary laser swing arm 45 angle on rotation correction laser aid 10, and adjust the position of upright projection device 1, make to be arranged on the rotary laser projection line 61 that on rotation correction laser aid 10, the 3rd cross laser device 31 is incident upon on graduated tile 18 and pass graduated tile center 57, and overlap with graduated tile axis 56, it is ensured that the vertical plane 60 at upright projection plate 13 place is parallel with graduated tile axis 56；
Repeatedly adjust Z axis turntable 23, the longitudinal axis laser rays 62 making each motor calibration laser aid 19 on multi-rotor aerocraft 22 project on graduated tile 18 projects rotary laser projection line 61 with rotation correction laser aid 10 respectively and overlaps, the most repeatedly adjust horn calibration of laser device 20, the laser rays that the second cross laser device 31 being arranged on horn calibration of laser device 20 is cast out intersects with horizontal scale line 59 on upright projection plate 13, and usage amount hornwork measures angle；Adjusting a horn 35 parallel with upright projection plate 13 every time, measure the angle between a horn 35 and horizontal scale line 59, this angle is equal to the angle between horn 35 and aircraft lower cover 37；
Above in conjunction with accompanying drawing, specific embodiment of the utility model is explained in detail, but this utility model is not limited to above-described embodiment, in the ken that those of ordinary skill in the art are possessed, it is also possible on the premise of without departing from this utility model objective, various changes can be made.
Claims (10)
1. a multi-rotor aerocraft installs equipment, it is characterised in that: include upright projection device (1), floor projection device (2), laser projection device (3), three axle rotary tables (4)；
Described upright projection device (1) includes upright projection device pedestal (5), foundation bolt (6), upright projection appliance stand (7), clamping limb (8), back timber (9), the first T-shaped bubble chi (11), bubble chi installing plate (12), upright projection plate (13)；Described foundation bolt (6) is supported on the ground by the screwed hole of upright projection device pedestal (5), described upright projection appliance stand (7) is arranged on upright projection device pedestal (5), described clamping limb (8) is arranged on upright projection appliance stand (7), described back timber (9) is arranged on upright projection appliance stand (7) top, described first T-shaped bubble chi (11) is arranged on bubble chi installing plate (12), described bubble chi installing plate (12) is arranged on upright projection plate (13), described upright projection plate (13) is lifted on the hook (52) of back timber (9), clamping limb contact surface (47) side of described clamping limb (8) leans against on upright projection plate (13)；
Described floor projection device (2) includes floor projection device lower margin (14), floor projection appliance stand (15), adjusting nut (16), top board (17), graduated tile (18)；Described floor projection device lower margin (14) is placed on work ground, described floor projection appliance stand (15) is arranged on described floor projection device lower margin (14), described adjusting nut (16) is arranged on floor projection appliance stand (15), described top board (17) is arranged on floor projection appliance stand (15) and adjusting nut (16), described graduated tile (18) is placed on top board (17), and the second T-shaped bubble chi (11) is placed on top board (17)；
Described laser projection device (3) includes rotation correction laser aid (10), motor calibration laser aid (19), horn calibration of laser device (20), central laser device (27)；Described rotation correction laser aid (10) is arranged on upright projection plate (13), described motor calibration laser aid (19) is arranged on the motor (34) of multi-rotor aerocraft (22), described horn calibration of laser device (20) is arranged on the horn (35) of multi-rotor aerocraft (22), and described central laser device (27) is arranged on the Y-axis turntable (25) of three axle rotary tables (4)；
Described three axle rotary tables (4) include Z axis turntable (23), X-axis turntable (24), Y-axis turntable (25), mounting platform (26)；Described X-axis turntable (24) is arranged on Z axis turntable (23), and described Y-axis turntable (25) is arranged on X-axis turntable (24), and described mounting platform (26) is arranged on Y-axis turntable (25).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterised in that: described motor calibration laser aid (19) includes axle bed (28), laser stent (29)；Described axle bed (28) is arranged on motor (34) output shaft, described laser stent (29) is arranged on axle bed (28), first clamper (30) is installed on described laser stent (29), described first clamper (30) is provided with the first cross laser device (31)；
Described horn calibration of laser device (20) includes seat (33) under the horn corrector seat of honour (32) and horn corrector；Under the described horn corrector seat of honour (32) and horn corrector, seat (33) is linked by bolt, it is clamped on horn (35), second clamper (30) is installed on the described horn corrector seat of honour (32), described second clamper (30) is provided with the second cross laser device (31).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: described rotation correction laser aid (10) includes rotary laser base (44), rotary laser swing arm (45), described rotary laser swing arm (45) and rotary laser base (44) pass through hinge links, 3rd clamper (30) is installed on described rotary laser swing arm (45), described 3rd clamper (30) is provided with the 3rd cross laser device (31).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: described central laser device (27) is with central laser base (43), 4th clamper (30) is installed on described central laser base (43), described 4th clamper (30) is provided with the 4th cross laser device (31).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: described mounting platform (26) is provided with clamp (21), multi-rotor aerocraft (22) is clamped on mounting platform (26) by clamp (21), one jaw clamping aircraft upper cover (36) of clamp (21), the bottom surface of another jaw clamping mounting platform (26) of clamp (21).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: described clamping limb (8) is with clamping limb screwed hole (46), described clamping limb (8) is with clamping limb contact surface (47), upright projection plate (13) leans against on clamping limb contact surface (47), described clamping limb (8) is with clamping limb open slot (48), described clamping limb (8) is with clamping limb installing hole (49), upright projection appliance stand (7) passes clamping limb installing hole (49), and described clamping limb (8) is with clamping limb locking screw pit (50).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: described back timber (9) is with back timber installing hole (51), upright projection appliance stand (7) passes back timber installing hole (51), described back timber (9) is with hook (52), and described back timber (9) is with back timber screwed hole (53).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterised in that: described graduated tile (18) is with graduated tile angle line (54), and described graduated tile (18) is with graduated tile concentric circular (55).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterised in that: described upright projection plate (13) is with upright projection plate hanging hole (58), and described upright projection plate (13) is with horizontal scale line (59).
Multi-rotor aerocraft the most according to claim 1 installs equipment, it is characterized in that: with mounting platform boss (41) on described mounting platform (26), the aircraft lower cover (37) of described multi-rotor aerocraft (22) contacts with mounting platform boss (41), with central laser base boss (42) on the central laser base (43) of described central laser device (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620048531.2U CN205593528U (en) | 2016-01-19 | 2016-01-19 | Many rotor crafts erection equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620048531.2U CN205593528U (en) | 2016-01-19 | 2016-01-19 | Many rotor crafts erection equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205593528U true CN205593528U (en) | 2016-09-21 |
Family
ID=56927385
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620048531.2U Withdrawn - After Issue CN205593528U (en) | 2016-01-19 | 2016-01-19 | Many rotor crafts erection equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205593528U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105526923A (en) * | 2016-01-19 | 2016-04-27 | 昆明理工大学 | Mounting equipment for multi-rotor type aircraft |
-
2016
- 2016-01-19 CN CN201620048531.2U patent/CN205593528U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105526923A (en) * | 2016-01-19 | 2016-04-27 | 昆明理工大学 | Mounting equipment for multi-rotor type aircraft |
| CN105526923B (en) * | 2016-01-19 | 2017-11-10 | 昆明理工大学 | A kind of multi-rotor aerocraft installs equipment |
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Granted publication date: 20160921 Effective date of abandoning: 20171110 |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20160921 Effective date of abandoning: 20171110 |