CN105526923B - A kind of multi-rotor aerocraft installs equipment - Google Patents
A kind of multi-rotor aerocraft installs equipment Download PDFInfo
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- CN105526923B CN105526923B CN201610033243.4A CN201610033243A CN105526923B CN 105526923 B CN105526923 B CN 105526923B CN 201610033243 A CN201610033243 A CN 201610033243A CN 105526923 B CN105526923 B CN 105526923B
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- laser
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- upright projection
- rotor aerocraft
- horn
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- 210000000078 claw Anatomy 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 29
- 238000005259 measurement Methods 0.000 abstract description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 239000004575 stone Substances 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 10
- 210000000080 chela (arthropods) Anatomy 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000012780 transparent material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000009187 flying Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C15/00—Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
- G01C15/002—Active optical surveying means
- G01C15/008—Active optical surveying means combined with inclination sensor
Abstract
The present invention relates to a kind of multi-rotor aerocraft to install equipment, belongs to aircraft manufacture technical field.The present invention includes upright projection device, floor projection device, laser projection device, three axle rotary tables；Upright projection device includes upright projection device pedestal, foundation bolt, upright projection appliance stand, clamping limb, back timber, the first T-shaped bubble chi, bubble chi installing plate, upright projection plate；Floor projection device includes floor projection device lower margin, floor projection appliance stand, adjusting nut, top plate, scale plate；Laser projection device includes rotation correction laser aid, motor calibration laser aid, horn calibration of laser device, central laser device；Three axle rotary tables include Z axis turntable, X-axis turntable, Y-axis turntable, mounting platform.The present invention can realize the accurate installation and position measurement of multi-rotor aerocraft motor and horn, to improve production efficiency, improve product quality and lay the first stone.
Description
Technical field
The present invention relates to a kind of multi-rotor aerocraft to install equipment, belongs to aircraft manufacture technical field.
Background technology
Relatively large multi-rotor aerocraft installation production is wasted time and energy at present, it is determined that mounting position of motor and horn established angle
When spending, lack necessary technological equipment, the number of axle of multi-rotor aerocraft is generally more than four, requires more rotor flyings during installation
The motor output shaft axis of device requires the centre distance of each motor output shaft axis and aircraft perpendicular to mounting plane
It is equal, it is desirable to which that motor is using aircraft center to be uniformly distributed on the circular arc in the center of circle, it is desirable to all horns of multi-rotor aerocraft with
Angle between mounting plane is consistent and meets design requirement, according to requirements above, technological equipment and work designed by the present invention
Process can realize that multi-rotor aerocraft motor and horn are accurately installed, and relative position dimensional measurement.
The content of the invention
It is an object of the invention to：For above-mentioned problem, there is provided a kind of electricity that disclosure satisfy that multi-rotor aerocraft
Machine and the adjustment of horn installation site, and the technological equipment of position measurement.
The technical scheme is that：A kind of multi-rotor aerocraft installs equipment, including upright projection device 1, floor projection
Device 2, laser projection device 3, three axle rotary tables 4；
The upright projection device 1 includes upright projection device pedestal 5, foundation bolt 6, upright projection appliance stand 7, folder
Gripping arm 8, back timber 9, the first T-shaped bubble chi 11, bubble chi installing plate 12, upright projection plate 13；The foundation bolt 6 is by vertical
On the ground, the upright projection appliance stand 7 is arranged on upright projection device pedestal for the screwed hole support of projection arrangement base 5
On 5, the clamping limb 8 is arranged on upright projection appliance stand 7, and the back timber 9 pushes up installed in upright projection appliance stand 7
Portion, the first T-shaped bubble chi 11 are arranged on bubble chi installing plate 12, and the bubble chi installing plate 12 is arranged on upright projection
On plate 13, the upright projection plate 13 is lifted on the hook 52 of back timber 9, the side of clamping limb contact surface 47 of the clamping limb 8
Lean against on upright projection plate 13；Adjust foundation bolt 6 and make it that the bubble on the first T-shaped bubble chi 11 is in an intermediate position, hook
52 cause upright projection plate 13 to be in overhang, adjust the locked position of clamping limb 8, upright projection plate 13 is kept catenary
While state, fix it；
The floor projection device 2 includes floor projection device lower margin 14, floor projection appliance stand 15, adjusting nut
16th, top plate 17, scale plate 18；The floor projection device lower margin 14 is placed on work ground, the floor projection device branch
Frame 15 is arranged on the floor projection device lower margin 14, and the adjusting nut 16 is arranged on floor projection appliance stand 15,
The top plate 17 is arranged on floor projection appliance stand 15 and adjusting nut 16, and the scale plate 18 is placed on top plate 17,
The second T-shaped bubble chi 11 is placed on top plate 17；Top plate 17 uses transparent material, laser rays is penetrated top plate 17 simultaneously
It is radiated on scale plate 18, scale plate 18 uses trnaslucent materials so that laser rays can produce clear projection；
The laser projection device 3 swashs including rotation correction laser aid 10, motor calibration laser aid 19, horn correction
Electro-optical device 20, central laser device 27；The rotation correction laser aid 10 is arranged on upright projection plate 13, the motor school
Positive laser aid 19 is arranged on the motor 34 of multi-rotor aerocraft 22, and the horn calibration of laser device 20 is arranged on more rotors
On the horn 35 of aircraft 22, the central laser device 27 is arranged on the Y-axis turntable 25 of three axle rotary tables 4；
The three axles rotary table 4 includes Z axis turntable 23, X-axis turntable 24, Y-axis turntable 25, mounting platform 26；The X
Axle turntable 24 is arranged on Z axis turntable 23, and the Y-axis turntable 25 is arranged on X-axis turntable 24, and the mounting platform 26 is arranged on
On Y-axis turntable 25, three axle rotary tables 4 can realize that multi-rotor aerocraft 22 carries out 360 degree of rotations about the z axis, put down installation
The keep level of platform 26；
The motor calibration laser aid 19 includes axle bed 28, laser stent 29；The axle bed 28 is arranged on motor 34
On output shaft, the laser stent 29 is arranged on axle bed 28, and the first clamper 30 is provided with the laser stent 29,
First cross laser device 31 is installed on first clamper 30；First clamper 30 ensures that the first cross laser device 31 is sent
Laser axis and the output shaft of motor 34 it is coaxial；
The horn calibration of laser device 20 includes seat 33 under the horn adjuster seat of honour 32 and horn adjuster；The horn
Seat 33 is linked by bolt under the adjuster seat of honour 32 and horn adjuster, is clamped on horn 35, the horn adjuster seat of honour
Second clamper 30 is installed on 32, the second cross laser device 31 is installed on second clamper 30, on horn adjuster
Seat 33 is clamped on horn 35 under seat 32 and horn adjuster, and can be around the adjustment position of horn 35；
The rotation correction laser aid 10 includes rotary laser base 44, rotary laser swing arm 45, the rotation
Laser swing arm 45 and rotary laser base 44 are provided with the 3rd folder by hinge links in the rotary laser swing arm 45
Holder 30, the 3rd cross laser device 31 is installed on the 3rd clamper 30, adjusts the clamping screw on hinge, swash rotation
Enough frictional force is kept between light device swing arm 45 and rotary laser base 44 so that manually adjusts rotary laser swing arm 45
When, adjustment rotary laser swing arm 45 can rest on any position；
The central laser device 27 carries central laser base 43, and the 4th folder is provided with the central laser base 43
Holder 30, the 4th cross laser device 31 is installed on the 4th clamper 30.
The adjustment mode of upright projection device of the present invention is：
Adjust the position of bubble chi installing plate 12 so that the horizontal quarter of bubble chi installing plate guiding ruler 40 and upright projection plate 13
Degree line 59 overlaps；Rigging position of the back timber 9 on upright projection appliance stand 7 is adjusted, locks the locking in back timber screwed hole 53
Bolt so that bubble 39 is positioned at centre in the first T-shaped bubble chi 11 on bubble chi installing plate 12；Ensure at horizontal scale line 59
In horizontal level；
Adjust the position of rotation correction laser aid 10 and the angle of rotary laser swing arm 45 so that installed in rotation school
The 3rd cross laser device 31 on positive laser aid 10 is incident upon one article in two articles of laser rays on upright projection plate 13 with hanging down
The horizontal scale line 59 of straight projection plate 13 overlaps；The 3rd cross laser device 31 for ensureing to install on rotation correction laser aid 10 is sent out
One gone out in two laser rays is parallel with upright projection plate 13；
The adjustment mode of floor projection device of the present invention is：
Adjusting nut 16 is adjusted to correct position so that bubble 39 is located in the second T-shaped bubble chi 11 on top plate 17
Centre, ensure that top plate 17 is in horizontal plane, then scale plate 18 is placed on top plate 17, the second T-shaped bubble chi 11 is put
Put on Y-axis turntable 25, the regulation handle on regulation Y-axis turntable 25 so that during bubble 39 is located in the second T-shaped bubble chi 11
Between, ensure that the mounting plane of Y-axis turntable 25 and mounting platform 26 are horizontal, the second T-shaped bubble chi 11 is then removed, by central laser
Device 27 is placed on the centre of Y-axis turntable 25, the 4th cross laser device 31 on central laser device 27 is opened, on top plate 17
Projection, makes laser rays vertical with top plate edge, and the scale plate angle line 54 of scale plate 18 is overlapped with laser rays, by scale plate
Center 57 overlaps with projection centre；Ensure to pass through in mounting platform 26 by the axis vertical with scale plate 18 of scale plate center 57
The heart；
Multi-rotor aerocraft mounting position of motor adjustment mode of the present invention is：
Adjust the installation site and motor calibration laser aid 19 of motor 34, and the on horn calibration of laser device 20
Two cross laser devices 31 so that the longitudinal axis laser rays 62 that each second cross laser device 31 is projected on scale plate 18 all passes through
Scale plate center 57, and overlapped with scale plate angle line 54, then adjust the installation site of all motors 34 so that project quarter
The transverse axis laser rays 63 and same scale plate concentric circles 55 spent on plate 18 are tangent, ensure the axial line distance scale of each motor 34
Plate center 57 causes this laser rays in the equal length of point of contact both sides apart from identical；Ensure the axis of motor 34 and top plate 17
Vertically；
Multi-rotor aerocraft horn setting angle metering system of the present invention is：
The angle of rotary laser swing arm 45 on rotation correction laser aid 10 is adjusted, and adjusts upright projection device 1
Position so that the 3rd cross laser device 31 is incident upon the rotary laser on scale plate 18 on rotation correction laser aid 10
Projection line 61 passes through scale plate center 57, and is overlapped with scale plate axis 56, ensures the upright projection where upright projection plate 13
Face 60 is parallel with scale plate axis 56；
Repeatedly adjustment Z axis turntable 23 so that each motor calibration laser aid 19 on multi-rotor aerocraft 22 projects
Longitudinal axis laser rays 62 on scale plate 18 projects rotary laser projection line 61 with rotation correction laser aid 10 respectively and overlapped, then
Repeatedly adjustment horn calibration of laser device 20 so that the second cross laser device 31 on horn calibration of laser device 20 is thrown
The laser rays shot out intersects with horizontal scale line 59 on upright projection plate 13, uses protractor measurement angle；Adjustment one every time
Individual horn 35 is parallel with upright projection plate 13, measures the angle, this angle etc. between a horn 35 and horizontal scale line 59
Angle between horn 35 and aircraft lower cover 37；
The mounting platform 26 is provided with clamp 21, the mounting platform 26 that multi-rotor aerocraft 22 is clamped in by clamp 21
On, lid 36 on the clamping jaw clamping aircraft of clamp 21, the bottom surface of another clamping jaw clamping mounting platform 26 of clamp 21, folder
When pincers 21 clamp, it is ensured that by the center of aircraft lower cover 37, and the axis vertical with the mounting surface of aircraft lower cover 37 is with passing through
The center of the mounting platform 26 and axis vertical with the mounting surface of mounting platform 26 overlaps.
The clamping limb 8 carries clamping limb screwed hole 46, and the clamping limb 8 carries clamping limb contact surface 47, upright projection
Plate 13 is leaned against on clamping limb contact surface 47, and the clamping limb 8 carries clamping limb open slot 48, and the clamping limb 8 carries clamping limb
Mounting hole 49, upright projection appliance stand 7 pass through clamping limb mounting hole 49, and the clamping limb 8 carries clamping limb locking screw pit
50, clamping limb 8 is locked on upright projection appliance stand 7 by clamping limb locking screw pit 50 using lock-screw.
The back timber 9 carries back timber mounting hole 51, and upright projection appliance stand 7 passes through back timber mounting hole 51, the back timber 9
With hook 52, the back timber 9 carries back timber screwed hole 53.
The scale plate 18 carries scale plate angle line 54, and the scale plate 18 carries scale plate concentric circles 55.
The upright projection plate 13 carries upright projection plate hanging hole 58, and the upright projection plate 13 carries horizontal scale line
59。
Carry mounting platform boss 41 on the mounting platform 26, the aircraft lower cover 37 of the multi-rotor aerocraft 22 with
Mounting platform boss 41 is contacted, and central laser base boss is carried on the central laser base 43 of the central laser device 27
42, ensure the contact precision of central laser base 43 and Y-axis turntable 25；The T-shaped bubble chi base band is magnetic, and can make it
Be conveniently installed on Y-axis turntable 25 and bubble chi installing plate 12, the mounting platform boss 41 ensure aircraft lower cover 37 with
Good contact between mounting platform 26.
The present invention the course of work be：
Upright projection device installation process：Bubble chi installing plate 12 is arranged on upright projection plate 13 so that bubble chi
Installing plate guiding ruler 40 aligns with horizontal scale line 59, position of the regulation back timber 9 in upright projection appliance stand 7, adjusts simultaneously
Foundation bolt 6 so that the bubble 39 of the first T-shaped bubble chi 11 on bubble chi installing plate 12 is positioned at centre, in upright projection plate
In the state of 13 only dangle, clamping limb 8 is adjusted so that clamping limb contact surface 47 contacts with upright projection plate 13, screws clamping
Bolt in arm screwed hole 46, upright projection plate 13 is clamped, rotation correction laser aid 10 is installed on upright projection plate 13, adjusted
Whole rotary laser swing arm 45 so that the laser rays that the 3rd cross laser device 31 is cast out and the weight of horizontal scale line 59
Close；
Floor projection device installation process：One adjusting nut 16 is installed on each floor projection device lower margin, will be pushed up
The threaded portion that plate 17 is penetrated on floor projection device lower margin, two T-shaped bubble chi adjustment adjusting nuts are placed on top plate 17,
So that the bubble in T-shaped bubble chi is in an intermediate position, then installs an adjusting nut on each floor projection device lower margin,
And lock；T-shaped bubble chi is placed at the Y-axis turntable center of three axle rotary tables, adjusts X-axis turntable and Y-axis turntable, make
The bubble obtained in T-shaped bubble chi is in an intermediate position, locking and regulating device, removes the T-shaped bubble chi of Y-axis turntable center, is put into
Central laser device, the cross laser device in central laser device is adjusted, makes the laser rays that it is projected on top plate in top plate side
Along vertically, scale plate is placed on top plate, adjusts the position of scale plate so that on scale plate Center-to-Center laser aid
The laser rays center superposition of cross laser device projection, and scale plate axis is overlapped with laser rays；
Horn setting angle measures：The aircraft lower cover of multi-rotor aerocraft is placed on mounting platform, pressed from both sides using clamp
Firmly lid 36 and mounting platform on aircraft, adjustment are arranged on the motor calibration laser aid on motor and the machine on horn
Arm calibration of laser device so that the laser rays that cross laser device mounted thereto is projected on scale plate overlaps, and rotational Z-axis
Turntable workbench so that the laser rays and scale plate axis of the laser projection on tested horn, then rotate horn correction and swash
Electro-optical device so that the laser rays of the laser projection of horn calibration of laser device and the horizontal scale line phase on upright projection plate
Hand over, measure the angle of cut using bevel protractor, that is, obtain horn setting angle.
Mounting position of motor adjusts：Adjust all mounting position of motor so that on motor calibration laser aid
The longitudinal axis laser rays of cross laser device projection overlaps with scale plate angle line, and is uniformly distributed with scale plate center so that transverse axis
Laser rays and same scale plate concentric circles are tangent.
The beneficial effects of the invention are as follows：The present invention can realize multi-rotor aerocraft motor and the accurate installation of horn and position
Measurement, to improve production efficiency, improve product quality and lay the first stone.
Brief description of the drawings
Fig. 1 is the overall axle geodesic structure schematic diagram of the present invention；
Fig. 2 is upright projection apparatus structure schematic diagram of the present invention；
Fig. 3 is floor projection apparatus structure schematic diagram of the present invention；
Fig. 4 is that the present invention removes vertically and horizontally projection arrangement structural representation；
Fig. 5 is the rotary table structural representation that the present invention installs T-shaped bubble chi；
Fig. 6 is the rotary table structural representation of installation center laser aid of the present invention；
Fig. 7 is motor calibration laser aid and horn calibration of laser apparatus structure schematic diagram of the present invention；
Fig. 8 is multi-rotor aerocraft structural representation of the present invention；
Fig. 9 is the T-shaped bubble chi structural representation of the present invention；
Figure 10 is bubble chi installing plate guiding ruler structural representation of the present invention；
Figure 11 is mounting platform structural representation of the present invention；
Figure 12 is central laser apparatus structure schematic diagram of the present invention；
Figure 13 is rotation correction laser device structure schematic diagram of the present invention；
Figure 14 is clamping limb structural representation of the present invention；
Figure 15 is beam structure schematic diagram of the present invention；
Figure 16 is scale plate structure schematic diagram of the present invention；
Figure 17 is upright projection plate structure schematic diagram of the present invention；
Figure 18 is present invention installation and location method schematic diagram.
Each label in Fig. 1-18：1- upright projection devices, 2- floor projection devices, 3- laser projection devices, the rotation of the axles of 4- tri-
Revolving worktable, 5- upright projection device pedestals, 6- foundation bolts, 7- upright projection appliance stands, 8- clamping limbs, 9- back timbers, 10-
Rotation correction laser aid, 11-T type bubble chis, 12- bubble chi installing plates, 13- upright projection plates, 14- floor projection devices
Pin, 15- floor projection appliance stands, 16- adjusting nuts, 17- top plates, 18- scale plates, 19- motor calibration laser aids, 20-
Horn calibration of laser device, 21- clamps, 22- multi-rotor aerocrafts, 23-Z axle turntables, 24-X axle turntables, 25-Y axle turntables, 26-
Mounting platform, 27- central laser devices, 28- axle beds, 29- laser stents, 30- clampers, 31- cross laser devices, 32- machines
The arm adjuster seat of honour, seat under 33- horn adjusters, 34- motors, 35- horns, cover on 36- aircraft, 37- aircraft lower covers,
38-T type bubble chi bases, 39- bubbles, 40- bubble chi installing plate guiding rulers, 41- mounting platform boss, 42- central laser bases
Boss, 43- central laser bases, 44- rotary laser bases, 45- rotary laser swing arms, 46- clamping limb screwed holes, 47-
Clamping limb contact surface, 48- clamping limb open slots, 49- clamping limb mounting holes, 50- clamping limb locking screw pits, the installation of 51- back timbers
Hole, 52- hooks, 53- back timber screwed holes, 54- scale plate angle lines, 55- scale plate concentric circles, 56- scale plate axis, 57- are carved
Spend plate center, 58- upright projection plate hanging holes, 59- horizontal scale lines, 60- vertical planes, 61- rotary laser projection lines, 62-
Longitudinal axis laser rays, 63- transverse axis laser rays.
Embodiment
Below in conjunction with the accompanying drawings and specific embodiment, the invention will be further described.
Embodiment 1：As shown in figure 1, a kind of multi-rotor aerocraft installation equipment, including upright projection device 1, floor projection
Device 2, laser projection device 3, three axle rotary tables 4；
As shown in Fig. 2 a kind of multi-rotor aerocraft installation equipment, the upright projection device 1 include upright projection device
Base 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
12nd, upright projection plate 13；The foundation bolt 6 is supported on the ground by the screwed hole of upright projection device pedestal 5, described to hang down
Image device support 7 is delivered directly on upright projection device pedestal 5, the clamping limb 8 is arranged on upright projection appliance stand 7
On, the back timber 9 is arranged on the top of upright projection appliance stand 7, and the first T-shaped bubble chi 11 is arranged on bubble chi installing plate
On 12, the bubble chi installing plate 12 is arranged on upright projection plate 13, and the upright projection plate 13 is lifted on the hook of back timber 9
On 52, the side of clamping limb contact surface 47 of the clamping limb 8 is leaned against on upright projection plate 13；Adjust foundation bolt 6 and cause the first T
Bubble on type bubble chi 11 is in an intermediate position, and hook 52 causes upright projection plate 13 to be in overhang, adjusts clamping limb 8
Locked position, make upright projection plate 13 keep overhang while, fix it；
The adjustment mode of the upright projection device is：
Adjust the position of rotation correction laser aid 10 and the angle of rotary laser swing arm 45 so that installed in rotation school
The 3rd cross laser device 31 on positive laser aid 10 is incident upon one article in two articles of laser rays on upright projection plate 13 with hanging down
The horizontal scale line 59 of straight projection plate 13 overlaps；The 3rd cross laser device 31 for ensureing to install on rotation correction laser aid 10 is sent out
One gone out in two laser rays is parallel with upright projection plate 13；
Adjust the position of bubble chi installing plate 12 so that the horizontal quarter of bubble chi installing plate guiding ruler 40 and upright projection plate 13
Degree line 59 overlaps；Rigging position of the back timber 9 on upright projection appliance stand 7 is adjusted, locks the locking in back timber screwed hole 53
Bolt so that bubble 39 is positioned at centre in the first T-shaped bubble chi 11 on bubble chi installing plate 12；Ensure at horizontal scale line 59
In horizontal level；
As shown in figure 3, a kind of multi-rotor aerocraft installation equipment, the floor projection device 2 include floor projection device
Lower margin 14, floor projection appliance stand 15, adjusting nut 16, top plate 17, scale plate 18；The floor projection device lower margin 14 is put
Put on work ground, the floor projection appliance stand 15 is arranged on the floor projection device lower margin 14, the regulation
Nut 16 is arranged on floor projection appliance stand 15, and the top plate 17 is arranged on floor projection appliance stand 15 and adjusting nut
On 16, the scale plate 18 is placed on top plate 17, and the second T-shaped bubble chi 11 is placed on top plate 17；Top plate 17 uses
Transparent material, laser rays is penetrated top plate 17 and be radiated on scale plate 18, scale plate 18 uses trnaslucent materials so that
Laser rays can produce clear projection；
As shown in figure 4, a kind of multi-rotor aerocraft installation equipment, the laser projection device 3 include rotation correction laser
Device 10, motor calibration laser aid 19, horn calibration of laser device 20, central laser device 27；The rotation correction laser
Device 10 is arranged on upright projection plate 13, and the motor calibration laser aid 19 is arranged on the motor 34 of multi-rotor aerocraft 22
On, the horn calibration of laser device 20 is arranged on the horn 35 of multi-rotor aerocraft 22, and the central laser device 27 is pacified
On the Y-axis turntable 25 of three axle rotary tables 4；
The mounting platform 26 is provided with clamp 21, the mounting platform 26 that multi-rotor aerocraft 22 is clamped in by clamp 21
On, lid 36 on the clamping jaw clamping aircraft of clamp 21, the bottom surface of another clamping jaw clamping mounting platform 26 of clamp 21, folder
When pincers 21 clamp, it is ensured that by the center of aircraft lower cover 37, and the axis vertical with the mounting surface of aircraft lower cover 37 is with passing through
The center of the mounting platform 26 and axis vertical with the mounting surface of mounting platform 26 overlaps.
As shown in figure 5, a kind of multi-rotor aerocraft installation equipment, the three axles rotary table 4 include Z axis turntable 23, X
Axle turntable 24, Y-axis turntable 25, mounting platform 26；The X-axis turntable 24 is arranged on Z axis turntable 23, and the Y-axis turntable 25 is pacified
On X-axis turntable 24, the mounting platform 26 is arranged on Y-axis turntable 25, and three axle rotary tables 4 can realize more rotors
Aircraft 22 carries out 360 degree of rotations about the z axis, makes the keep level of mounting platform 26；
As shown in Fig. 3, Fig. 5, Fig. 6, a kind of multi-rotor aerocraft installs equipment, the tune of floor projection device of the present invention
Perfect square formula is：
Adjusting nut 16 is adjusted to correct position so that bubble 39 is located in the second T-shaped bubble chi 11 on top plate 17
Centre, ensure that top plate 17 is in horizontal plane, then scale plate 18 is placed on top plate 17, the second T-shaped bubble chi 11 is put
Put on Y-axis turntable 25, the regulation handle on regulation Y-axis turntable 25 so that during bubble 39 is located in the second T-shaped bubble chi 11
Between, ensure that the mounting plane of Y-axis turntable 25 and mounting platform 26 are horizontal, the second T-shaped bubble chi 11 is then removed, by central laser
Device 27 is placed on the centre of Y-axis turntable 25, the 4th cross laser device 31 on central laser device 27 is opened, on top plate 17
Projection, makes laser rays vertical with top plate edge, and the scale plate angle line 54 of scale plate 18 is overlapped with laser rays, by scale plate
Center 57 overlaps with projection centre；Ensure to pass through in mounting platform 26 by the axis vertical with scale plate 18 of scale plate center 57
The heart；
As shown in fig. 7, a kind of multi-rotor aerocraft installation equipment, the motor calibration laser aid 19 include axle bed 28,
Laser stent 29；The axle bed 28 is arranged on the output shaft of motor 34, and the laser stent 29 is arranged on axle bed 28, institute
State and the first clamper 30 is installed on laser stent 29, the first cross laser device 31 is installed on first clamper 30；
The laser axis and the output shaft of motor 34 that first clamper 30 the first cross laser device 31 of guarantee is sent are coaxial；
The horn calibration of laser device 20 includes seat 33 under the horn adjuster seat of honour 32 and horn adjuster；The horn
Seat 33 is linked by bolt under the adjuster seat of honour 32 and horn adjuster, is clamped on horn 35, the horn adjuster seat of honour
Second clamper 30 is installed on 32, the second cross laser device 31 is installed on second clamper 30, on horn adjuster
Seat 33 is clamped on horn 35 under seat 32 and horn adjuster, and can be around the adjustment position of horn 35；
As shown in figure 8, a kind of multi-rotor aerocraft installation equipment, multi-rotor aerocraft include motor 34, horn 35, flight
The bottom surface of aircraft lower cover 37 is pressed in the mounting platform boss on mounting platform 26 by lid 36, aircraft lower cover 37 on device, clamp 21
On 41.
As shown in figure 9, a kind of multi-rotor aerocraft installation equipment, T-shaped bubble chi base 38 is that band is magnetic.
As shown in Figure 10, a kind of multi-rotor aerocraft installation equipment, bubble chi installing plate 12 lean on bubble chi installing plate
Chi 40.
As shown in figure 11, a kind of multi-rotor aerocraft installs equipment, and mounting platform boss is carried on the mounting platform 26
41, the aircraft lower cover 37 of the multi-rotor aerocraft 22 contacts with mounting platform boss 41, the central laser device 27
Central laser base boss 42 is carried on central laser base 43, ensures the essence of the contact with Y-axis turntable 25 of central laser base 43
Degree；The 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,
The 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 installation equipment, the central laser device 27 carry central laser bottom
Seat 43, the 4th clamper 30 is installed on the central laser base 43, the 4th cross is installed on the 4th clamper 30
Laser 31.
As shown in figure 13, a kind of multi-rotor aerocraft installation equipment, the rotation correction laser aid 10 include rotation and swashed
Light device base 44, rotary laser swing arm 45, the rotary laser swing arm 45 pass through hinge chain with rotary laser base 44
Connect, the 3rd clamper 30 is installed in the rotary laser swing arm 45, the 3rd cross is installed on the 3rd clamper 30
Laser 31, the clamping screw on hinge is adjusted, make to keep foot between rotary laser swing arm 45 and rotary laser base 44
Enough frictional force so that when manually adjusting rotary laser swing arm 45, adjustment rotary laser swing arm 45 can rest on any
Position；
As shown in figure 14, a kind of multi-rotor aerocraft installation equipment, the clamping limb 8 carry clamping limb screwed hole 46, institute
State clamping limb 8 and carry clamping limb contact surface 47, upright projection plate 13 is leaned against on clamping limb contact surface 47, and the clamping limb 8 carries
Clamping limb open slot 48, the clamping limb 8 carry clamping limb mounting hole 49, and upright projection appliance stand 7 is installed through clamping limb
Hole 49, the clamping limb 8 carry clamping limb locking screw pit 50, will be pressed from both sides by clamping limb locking screw pit 50 using lock-screw
Gripping arm 8 is locked on upright projection appliance stand 7.
As shown in figure 15, a kind of multi-rotor aerocraft installation equipment, the back timber 9 carries back timber mounting hole 51, vertical to throw
Image device support 7 passes through back timber mounting hole 51, and for the back timber 9 with hook 52, the back timber 9 carries back timber screwed hole 53.
As shown in figure 16, a kind of multi-rotor aerocraft installation equipment, the scale plate 18 carry scale plate angle line 54, institute
State scale plate 18 and carry scale plate concentric circles 55.The scale plate 18 carries scale plate axis 56 and scale plate center 57；
As shown in figure 17, a kind of multi-rotor aerocraft installation equipment, the upright projection plate 13 are hung with upright projection plate
Hole 58, the upright projection plate 13 carry horizontal scale line 59.
As shown in figure 18, a kind of multi-rotor aerocraft installation equipment, multi-rotor aerocraft motor installation position of the present invention
Putting adjustment mode is：
Adjust the installation site and motor calibration laser aid 19 of motor 34, and the on horn calibration of laser device 20
Two cross laser devices 31 so that the longitudinal axis laser rays 62 that each second cross laser device 31 is projected on scale plate 18 all passes through
Scale plate center 57, and overlapped with scale plate angle line 54, then adjust the installation site of all motors 34 so that project quarter
The transverse axis laser rays 63 and same scale plate concentric circles 55 spent on plate 18 are tangent, ensure the axial line distance scale of each motor 34
Plate center 57 causes this laser rays in the equal length of point of contact both sides apart from identical；Ensure the axis of motor 34 and top plate 17
Vertically；
Multi-rotor aerocraft horn setting angle metering system of the present invention is：
The angle of rotary laser swing arm 45 on rotation correction laser aid 10 is adjusted, and adjusts upright projection device 1
Position so that the 3rd cross laser device 31 is incident upon the rotary laser on scale plate 18 on rotation correction laser aid 10
Projection line 61 passes through scale plate center 57, and is overlapped with scale plate axis 56, ensures the upright projection where upright projection plate 13
Face 60 is parallel with scale plate axis 56；
Repeatedly adjustment Z axis turntable 23 so that each motor calibration laser aid 19 on multi-rotor aerocraft 22 projects
Longitudinal axis laser rays 62 on scale plate 18 projects rotary laser projection line 61 with rotation correction laser aid 10 respectively and overlapped, then
Repeatedly adjustment horn calibration of laser device 20 so that the second cross laser device 31 on horn calibration of laser device 20 is thrown
The laser rays shot out intersects with horizontal scale line 59 on upright projection plate 13, uses protractor measurement angle；Adjustment one every time
Individual horn 35 is parallel with upright projection plate 13, measures the angle, this angle etc. between a horn 35 and horizontal scale line 59
Angle between horn 35 and aircraft lower cover 37.
The specific embodiment of the present invention is explained in detail above in conjunction with accompanying drawing, but the present invention is not limited to above-mentioned reality
Example is applied, can also be on the premise of present inventive concept not be departed from those of ordinary skill in the art's possessed knowledge
Various changes can be made.
Claims (10)
1. a kind of multi-rotor aerocraft installs equipment, it is characterised in that：Including upright projection device（1）, floor projection device
（2）, laser projection device（3）, three axle rotary tables（4）；
The upright projection device（1）Including 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）；It is described
Foundation bolt（6）Pass through upright projection device pedestal（5）Screwed hole support on the ground, the upright projection appliance stand
（7）Installed in upright projection device pedestal（5）On, the clamping limb（8）Installed in upright projection appliance stand（7）On, it is described
Back timber（9）Installed in upright projection appliance stand（7）Top, the first T-shaped bubble chi（11）Installed in bubble chi installing plate
（12）On, the bubble chi installing plate（12）Installed in upright projection plate（13）On, the upright projection plate（13）It is lifted on top
Beam（9）Hook（52）On, the clamping limb（8）Clamping limb contact surface（47）Side leans against upright projection plate（13）On；
The floor projection device（2）Including floor projection device lower margin（14）, floor projection appliance stand（15）, adjusting nut
（16）, top plate（17）, scale plate（18）；The floor projection device lower margin（14）It is placed on work ground, the horizontal throwing
Image device support（15）Installed in the floor projection device lower margin（14）On, the adjusting nut（16）Installed in floor projection
Appliance stand（15）On, the top plate（17）Installed in floor projection appliance stand（15）And adjusting nut（16）On, the quarter
Spend plate（18）It is placed on top plate（17）On, the second T-shaped bubble chi（11）It is placed on top plate（17）On；
The laser projection device（3）Including rotation correction laser aid（10）, motor calibration laser aid（19）, horn correction
Laser aid（20）, central laser device（27）；The rotation correction laser aid（10）Installed in upright projection plate（13）On,
The motor calibration laser aid（19）Installed in multi-rotor aerocraft（22）Motor（34）On, the horn calibration of laser dress
Put（20）Installed in multi-rotor aerocraft（22）Horn（35）On, the central laser device（27）Work is rotated installed in three axles
Make platform（4）Y-axis turntable（25）On；
The three axles rotary table（4）Including Z axis turntable（23）, X-axis turntable（24）, Y-axis turntable（25）, mounting platform
（26）；The X-axis turntable（24）Installed in Z axis turntable（23）On, the Y-axis turntable（25）Installed in X-axis turntable（24）On, institute
State mounting platform（26）Installed in Y-axis turntable（25）On.
2. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The motor calibration laser aid
（19）Including axle bed（28）, laser stent（29）；The axle bed（28）Installed in motor（34）On output shaft, the laser
Support（29）Installed in axle bed（28）On, the laser stent（29）On the first clamper is installed（30）, first folder
Holder（30）On the first cross laser device is installed（31）；
The horn calibration of laser device（20）Including the horn adjuster seat of honour（32）With seat under horn adjuster（33）；The machine
The arm adjuster seat of honour（32）With seat under horn adjuster（33）Linked by bolt, be clamped in horn（35）On, the horn school
The positive device seat of honour（32）On the second clamper is installed（30）, second clamper（30）On the second cross laser device is installed
（31）.
3. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The rotation correction laser aid
（10）Including rotary laser base（44）, rotary laser swing arm（45）, the rotary laser swing arm（45）Swash with rotating
Light device base（44）By hinge links, the rotary laser swing arm（45）On the 3rd clamper is installed（30）, described
Three clampers（30）On the 3rd cross laser device is installed（31）.
4. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The central laser device（27）
With central laser base（43）, the central laser base（43）On the 4th clamper is installed（30）, the 4th clamping
Device（30）On the 4th cross laser device is installed（31）.
5. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The mounting platform（26）On set
There is clamp（21）, clamp（21）By multi-rotor aerocraft（22）The mounting platform being clamped in（26）On, clamp（21）One folder
Claw clip is held to be covered on aircraft（36）, clamp（21）Another clamping jaw clamping mounting platform（26）Bottom surface.
6. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The clamping limb（8）With folder
Gripping arm screwed hole（46）, the clamping limb（8）With clamping limb contact surface（47）, upright projection plate（13）Lean against clamping arm contact
Face（47）On, the clamping limb（8）With clamping limb open slot（48）, the clamping limb（8）With clamping limb mounting hole（49）,
Upright projection appliance stand（7）Through clamping limb mounting hole（49）, the clamping limb（8）With clamping limb locking screw pit
（50）.
7. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The back timber（9）With back timber
Mounting hole（51）, upright projection appliance stand（7）Through back timber mounting hole（51）, the back timber（9）With hook（52）, it is described
Back timber（9）With back timber screwed hole（53）.
8. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The scale plate（18）With quarter
Spend plate angle line（54）, the scale plate（18）With scale plate concentric circles（55）.
9. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The upright projection plate（13）Band
There is upright projection plate hanging hole（58）, the upright projection plate（13）With horizontal scale line（59）.
10. multi-rotor aerocraft according to claim 1 installs equipment, it is characterised in that：The mounting platform（26）On
With mounting platform boss（41）, the multi-rotor aerocraft（22）Aircraft lower cover（37）With mounting platform boss（41）Connect
Touch, the central laser device（27）Central laser base（43）It is upper to carry central laser base boss（42）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610033243.4A CN105526923B (en) | 2016-01-19 | 2016-01-19 | A kind of multi-rotor aerocraft installs equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610033243.4A CN105526923B (en) | 2016-01-19 | 2016-01-19 | A kind of multi-rotor aerocraft installs equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105526923A CN105526923A (en) | 2016-04-27 |
| CN105526923B true CN105526923B (en) | 2017-11-10 |
Family
ID=55769297
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610033243.4A Expired - Fee Related CN105526923B (en) | 2016-01-19 | 2016-01-19 | A kind of multi-rotor aerocraft installs equipment |
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Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108036723B (en) * | 2017-12-28 | 2024-02-23 | 顺丰科技有限公司 | Two-axis rotating device |
| CN107938729B (en) * | 2018-01-02 | 2023-04-11 | 沈阳建筑大学 | Device for detecting embedding position of pile casing and checking method thereof |
| CN110040262B (en) * | 2019-04-30 | 2021-12-14 | 中北大学 | Mechanical fault debugging device for rotor craft |
| CN113739749B (en) * | 2021-08-25 | 2022-10-25 | 成都飞机工业（集团）有限责任公司 | Angle measuring device for electric connector and bent accessory |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2867291Y (en) * | 2005-09-16 | 2007-02-07 | 领域开发科技有限公司 | Light beam projector structure for laser measuring instrument |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| CN205593528U (en) * | 2016-01-19 | 2016-09-21 | 昆明理工大学 | Many rotor crafts erection equipment |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2289932B1 (en) * | 2006-07-03 | 2009-03-01 | INSTITUTO NACIONAL DE TECNICA AEROESPACIAL "ESTEBAN TERRADAS" | AIRCRAFT WITH CONVERTIBLE FLIGHT SYSTEM. |
-
2016
- 2016-01-19 CN CN201610033243.4A patent/CN105526923B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2867291Y (en) * | 2005-09-16 | 2007-02-07 | 领域开发科技有限公司 | Light beam projector structure for laser measuring instrument |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| CN205593528U (en) * | 2016-01-19 | 2016-09-21 | 昆明理工大学 | Many rotor crafts erection equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105526923A (en) | 2016-04-27 |
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Granted publication date: 20171110 |