CN106122361A - A kind of multi-rotor aerocraft intelligent docking equipment - Google Patents
A kind of multi-rotor aerocraft intelligent docking equipment Download PDFInfo
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- CN106122361A CN106122361A CN201610491228.4A CN201610491228A CN106122361A CN 106122361 A CN106122361 A CN 106122361A CN 201610491228 A CN201610491228 A CN 201610491228A CN 106122361 A CN106122361 A CN 106122361A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The present invention relates to a kind of novel UAV Intelligent and stop equipment, including damping device, masking device and stop pedestal；The quantity of described masking device is two, and masking device lays respectively at the damping device left and right sides along the central axis of damping device, stops pedestal and is positioned at directly over damping device, and stops between pedestal and damping device connected.The present invention can provide stop protection in the case of prominent chance thunderstorm weather to unmanned plane during outdoor study; and damping performance is good when stopping; spacing stationarity is high; avoid unmanned plane and easily cause, in thunderstorm weather flight, the problem got an electric shock or be struck by lightning so that the safety of unmanned plane operation is greatly improved.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, a kind of multi-rotor aerocraft intelligent docking equipment.
Background technology
Aircraft be manufactured by the mankind, can fly away from ground, space flight and by people control in endoatmosphere or big
The apparatus flying object that the gas-bearing formation external space (space) is flown, aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also the one of aircraft, and unmanned plane is to utilize radio robot and the presetting apparatus provided for oneself to handle not
Manned aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned from technical standpoint definition
Dirigible and unmanned parasol etc.；Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, unmanned plane can be widely applied to country ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitor,
Traffic patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration, town planning,
Seismic survey, environmental monitoring, forest fire protection, Crop Estimation, the monitoring of protection zone wild animal, air sampling, maritime affairs scouting, limit
Border is maked an inspection tour, the prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water resources development, agriculture
Crop condition monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, forest disease and pest
The fields such as protection and monitoring, digital city.
Aircraft has relatively strong, the motion less than normal, popular of compact conformation, build, and flexibly and the advantage such as flight stability is by extensively
Apply in civil and military, and the most popular；When aircraft operation out of doors, meet thunderstorm situation if prominent, by
Aloft fly in aircraft, it is easy to causing electric shock or thunderbolt, safety is subject to the biggest threat, in consideration of it, the present invention carries
Supply a kind of multi-rotor aerocraft intelligent docking equipment.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of multi-rotor aerocraft intelligent docking equipment.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of multi-rotor aerocraft intelligent docking equipment, including damping device, masking device and stop pedestal；Described screening
The quantity covering device is two, and masking device lays respectively at the damping device left and right sides along the central axis of damping device, stops base
Seat is positioned at directly over damping device, and stops between pedestal and damping device connected.
Further, described damping device includes lower fixed seat, upper fixed seat, redundancy parallel mechanism and damping；Institute
The redundancy parallel mechanism stated is between lower fixed seat and upper fixed seat, and redundancy parallel mechanism lower end is connected with lower fixed seat
Connecing, redundancy parallel mechanism upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at redundant parallel
Outside mechanism, and damping is uniformly arranged circumferentially about along the central axis of redundancy parallel mechanism.
Further, described redundancy parallel mechanism includes fixed platform, moving platform, the first side chain and the second side chain；Described
Fixed platform and moving platform are disc-shaped structure, and moving platform is positioned at directly over fixed platform；The first described side chain and second
The quantity of chain is two, and the first side chain and the second side chain are respectively positioned between fixed platform and moving platform, the first side chain and the second side chain
Two ends be connected with fixed platform and moving platform respectively, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；
The first described side chain includes that the first ear mount, Hooke's hinge, the first electric pushrod, the first spherical hinge, the first connection post and first shake
Move spring；The first described ear mount is fixed on fixed platform upper surface, uses between the first ear mount and the first electric pushrod lower end
Hooke's hinge is attached, and the first electric pushrod upper end is connected with the first spherical hinge, and the first spherical hinge is solid by the first connection post
Being scheduled on the lower surface of moving platform, the first vibrating spring is around being enclosed within the first electric pushrod；Two sides can be carried out by Hooke's hinge
To rotation, the rotation in three directions can be carried out by the first spherical hinge, can be moved up and down by the first electric pushrod,
The form of one side chain employing 2-UPS parallel institution, and the damping performance of the first side chain is added by the first vibrating spring, improve
The damping effect of the present invention；The second described side chain include the second ear mount, rotational pin, the second electric pushrod, the second spherical hinge,
Second connects post and the second vibrating spring；The second described ear mount is fixed on fixed platform upper surface, the second ear mount and the second electricity
Using rotational pin to be attached between dynamic push rod lower end, the second electric pushrod upper end is connected with the second spherical hinge, the second ball pivot
Chain connects post by second and is fixed on the lower surface of moving platform, and the second vibrating spring is around being enclosed within the second electric pushrod；Pass through
Rotational pin can carry out the rotation in a direction, can be carried out the rotation in three directions by the second spherical hinge, electronic pushes away by second
Bar can move up and down, and the second side chain uses the form of 2-RPS parallel institution, and adds second by the second vibrating spring
During chain movement damping performance, improve the damping effect of the present invention；By fixed platform, moving platform, the first side chain and
Two side chains constitute four-degree-of-freedom symmetry redundancy parallel mechanism, and it uses the parallel institution form of 2-UPS-2-RPS, and it can be real
Now move along X-axis and Z axis and around X-axis and moving around rotation totally four degree of freedom directions of Y-axis, and four degree of freedom are the most only
Vertical, by four degree of freedom can also co-ordination, the moving platform track made along the curvilinear motion of predetermined space, stable movement,
Motion flexibly, when aircraft landing is stopped, though attitude of flight vehicle unstable or skewed time, redundancy parallel mechanism passes through
First side chain and the space motion of the second side chain, reach the elimination of displacement difference during aircraft landing and supplement, thus serving and subtract
The good result of shake, it is ensured that the aircraft stability when dropping to stop pedestal, jitter is little, vibration when reducing landing
Damage to aircraft fuselage.
Further, described damping includes mounting post, lower mounting post and damping stage clip；Described upper mounting post and
The lower the most T-shaped structure of mounting post, upper mounting post upper end and lower mounting post lower end are provided with external screw thread, upper mounting post lower end respectively
It is provided with lock sleeve respectively with lower mounting post upper end, between upper mounting post upper end and upper fixed seat, uses the mode of threaded engagement
Being attached, between lower mounting post lower end and lower fixed seat, the mode also by threaded engagement is attached, damping stage clip two ends
It is separately mounted to mounting post lower end and lower mounting post upper end；Damping serves the effect of secondary shock-absorbing to damping device,
Making damping device have the effect of dual shock absorption, damping performance is greatly improved.
Further, described masking device includes connecting base, longitudinal electric push rod, shock-proof spring, lifting support, laterally
Electric pushrod, traversing carriage and mask；Described connection pan frontward end is provided with paliform link, connects base rear end and sets
Being equipped with waist template, longitudinal electric push rod linearly type is equally spaced to be connected between base and lifting support, and longitudinal electric
Push rod bottom is connected with waist template, and longitudinal electric push rod top is connected with lifting support, and shock-proof spring is around being enclosed within longitudinal electricity
On dynamic push rod, lifting support is of an L-shaped structure, and is provided with floor, transverse electric between the vertical of lifting support and horizontal plane
Push rod bottom is fixed on lifting support, uses the mode of threaded engagement to enter between transverse electric push rod and traversing carriage rear end face
Row connects, and traversing carriage rear end is isosceles triangle column structure, and traversing carriage front end is evenly arranged with fixed strip, and mask is solid
Being scheduled on the fixed strip of traversing carriage front end, mask is forme fruste spherical shell structure, and mask front end is provided with rubber
Circle, mask outer surface is evenly arranged with coatings；When unmanned plane operation out of doors prominent chance thunderstorm weather situation, unmanned
The bus stop that machine may be selected by near operating location is hidden, and when unmanned plane lands, transverse electric push rod shrinks
Motion, two masks pull open laterally, and unmanned plane drops to stop on pedestal, by stopping pedestal lower end installation damping dress
Putting, unmanned plane landing is served good cushioning effect, after unmanned plane is stopped and stablized, transverse electric push rod carries out stretching fortune
Dynamic, two inside side closures of mask, and also mask front end is provided with rubber ring, and two rubber rings are under rubber suction
Tightly fitting together, two masks form a hemispherical insulating boot, serve unmanned plane in the case of thunderstorm weather
Well protective effect, and the whole height of masking device can be regulated by longitudinal electric push rod, it is adaptable to different terrain
The use of landforms.
Further, described stop base bottom is octagon slab construction, and stops the left and right two of pedestal upper surface
Side is respectively symmetrically and offers semicircle screens groove, can be entered the unmanned plane dropping to stop on pedestal by semicircle screens groove
Line position is fixed, and the center position stopping pedestal upper surface offers circular hole, and the outside stopping pedestal is provided with surrounding edge, surrounding edge
Outside is evenly arranged with signal lights successively, and signal lights serves the effect at night to position indicating of the present invention.
Compared with prior art, the invention have the advantages that
(1) present invention can provide stop protection in the case of prominent chance thunderstorm weather to unmanned plane during outdoor study, and stops
By time damping performance good, spacing stationarity is high, it is to avoid unmanned plane easily causes in thunderstorm weather flight and gets an electric shock or the asking of thunderbolt
Topic so that the safety of unmanned plane operation is greatly improved.
(2) damping device of the present invention uses redundancy parallel mechanism and damping, has dual shock absorption effect, and redundancy
Parallel institution uses the parallel institution form of 2-UPS-2-RPS, and it can realize moving along X-axis and Z axis and around X-axis with around Y-axis
The motion in rotation totally four degree of freedom directions, and four degree of freedom are all independent, by four degree of freedom can also co-ordination,
The moving platform track made is along the curvilinear motion of predetermined space, stable movement, and motion is flexible, when aircraft landing is stopped, even if
UAV Attitude unstable or skewed time, redundancy parallel mechanism pass through the first side chain and the space motion of the second side chain, reach
To aircraft land time the elimination of displacement difference and supplementing, thus serve the good result of damping, it is ensured that aircraft is in landing
To stability during stop pedestal, jitter is little, the vibration damage to aircraft fuselage when reducing landing.
(3) masking device of the present invention uses opposite opened folding form, opens and closes equal simple and fast, seals during closedown
Property good, insulating properties is high, and whole height scalable, it is adaptable to the use of different terrain landforms, to unmanned plane in thunderstorm weather feelings
Play a very good protection under condition.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view of the present invention；
Fig. 2 is the perspective view of damping device of the present invention；
Fig. 3 is perspective view during two masking devices cooperations of the present invention；
Fig. 4 is the perspective view of masking device of the present invention；
Fig. 5 is the perspective view of redundancy parallel mechanism of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below knot
Conjunction is specifically illustrating, and the present invention is expanded on further.
As shown in Figures 1 to 5, a kind of multi-rotor aerocraft intelligent docking equipment, including damping device 1, masking device 2 and
Stop pedestal 3；The quantity of described masking device 2 is two, and masking device 2 lays respectively at along the central axis of damping device 1 and subtracts
Shake device 1 left and right sides, stops pedestal 3 and is positioned at directly over damping device 1, and stops between pedestal 3 and damping device 1 connected.
As in figure 2 it is shown, described damping device 1 includes lower fixed seat 11, upper fixed seat 12, redundancy parallel mechanism 13 and subtracts
Shake mechanism 14；Described redundancy parallel mechanism 13 is between lower fixed seat 11 and upper fixed seat 12, and redundancy parallel mechanism 13
Lower end is connected with lower fixed seat 11, and redundancy parallel mechanism 13 upper end is connected with upper fixed seat 12, and damping 14 quantity is
Eight, damping 14 lays respectively at outside redundancy parallel mechanism 13, and damping 14 is along the central shaft of redundancy parallel mechanism 13
Line is uniformly arranged circumferentially about.
As it is shown in figure 5, the redundancy parallel mechanism 13 stated includes fixed platform 131, moving platform the 132, first side chain 133 and second
Side chain 134；Described fixed platform 131 and moving platform 132 are disc-shaped structure, and moving platform 132 is positioned at fixed platform 131 and just goes up
Side；The first described side chain 133 and the quantity of the second side chain 134 are two, and the first side chain 133 and the second side chain 134 are respectively positioned on
Between fixed platform 131 and moving platform 132, the two ends of the first side chain 133 and the second side chain 134 respectively with fixed platform 131 and dynamic
Platform 132 is connected, and the horizontal installation angle of the first side chain 133 and the second side chain 134 is 90 degree；The first described side chain
133 include that the first ear mount 1331, Hooke's hinge the 1332, first electric pushrod the 1333, first spherical hinge 1334, first connect post 1335
With the first vibrating spring 1336；The first described ear mount 1331 is fixed on fixed platform 131 upper surface, the first ear mount 1331 and
Hooke's hinge 1332 is used to be attached between one electric pushrod 1333 lower end, the first electric pushrod 1333 upper end and the first spherical hinge
1334 are connected, and the first spherical hinge 1334 is fixed on the lower surface of moving platform 132 by the first connection post 1335, the first vibration
Spring 1336 is around being enclosed within the first electric pushrod 1333；The rotation of both direction can be carried out, by first by Hooke's hinge 1332
Spherical hinge 1334 can carry out the rotation in three directions, can be moved up and down by the first electric pushrod 1333, the first side chain 133
The form of employing 2-UPS parallel institution, and the damping performance of the first side chain 133 is added by the first vibrating spring 1336, carry
The high damping effect of the present invention；The second described side chain 134 includes the second ear mount 1341, rotational pin 1342, second is electronic pushes away
Bar the 1343, second spherical hinge 1344, second connects post 1345 and the second vibrating spring 1346；The second described ear mount 1341 is fixed
On fixed platform 131 upper surface, rotational pin 1342 between the second ear mount 1341 and the second electric pushrod 1343 lower end, is used to carry out
Connecting, the second electric pushrod 1343 upper end is connected with the second spherical hinge 1344, and the second spherical hinge 1344 is by the second connection post
On 1345 lower surfaces being fixed on moving platform 132, the second vibrating spring 1346 is around being enclosed within the second electric pushrod 1343；By turning
Untie-sell 1342 can carry out the rotation in a direction, can be carried out the rotation in three directions by the second spherical hinge 1344, by second
Electric pushrod 1343 can move up and down, and the second side chain 134 uses the form of 2-RPS parallel institution, and by the second vibration
Spring 1346 add when the second side chain 134 moves damping performance, improve the damping effect of the present invention；Pass through fixed platform
131, moving platform the 132, first side chain 133 and the second side chain 134 constitute four-degree-of-freedom symmetry redundancy parallel mechanism 13, and it is adopted
By the parallel institution form of 2-UPS-2-RPS, it can realize moving along X-axis and Z axis and around X-axis with around the rotation totally four of Y-axis
The motion in individual degree of freedom direction, and four degree of freedom are all independent, by four degree of freedom can also co-ordination, the moving platform made
Track is along the curvilinear motion of predetermined space, stable movement, and motion is flexible, when aircraft landing is stopped, even if UAV Attitude
Unstable or skewed time, redundancy parallel mechanism 13, by the first side chain 133 and space motion of the second side chain 134, reaches
The elimination of displacement difference and supplementing during aircraft landing, thus serves the good result of damping, it is ensured that aircraft is when landing
Stability, jitter is little, the vibration damage to aircraft fuselage when reducing landing.
As in figure 2 it is shown, described damping 14 includes mounting post 141, lower mounting post 142 and damping stage clip 143；Institute
The upper mounting post 141 stated and the lower the most T-shaped structure of mounting post 142, upper mounting post 141 upper end and lower mounting post 142 lower end are divided equally
It is not provided with external screw thread, upper mounting post 141 lower end and lower mounting post 142 upper end and is provided with lock sleeve, upper mounting post 141 respectively
The mode using threaded engagement between upper end and upper fixed seat 12 is attached, lower mounting post 142 lower end and lower fixed seat 11 it
Between be attached also by the mode of threaded engagement, damping stage clip 143 two ends are separately mounted to mounting post 141 lower end and lower peace
Dress post 142 upper end；Damping 14 serves the effect of secondary shock-absorbing to damping device so that damping device 1 has dual subtracting
The effect of shake, damping performance is greatly improved.
As shown in Figure 3 and Figure 4, described masking device 2 includes connecting base 21, longitudinal electric push rod 22, shock-proof spring
23, lifting support 24, transverse electric push rod 25, traversing carriage 26 and mask 27；Described connection base 21 front end is provided with
Paliform link, connects base 21 rear end and is provided with waist template, and longitudinal electric push rod 22 linearly type is equally spaced to be positioned at even
Connecing between base 21 and lifting support 24, and longitudinal electric push rod 22 bottom is connected with waist template, longitudinal electric push rod 22 pushes up
End is connected with lifting support 24, and shock-proof spring 23 is around being enclosed within longitudinal electric push rod 22, and lifting support 24 is of an L-shaped structure, and
Being provided with floor between vertical and the horizontal plane of lifting support 24, transverse electric push rod 25 bottom is fixed on lifting support 24
On, use the mode of threaded engagement to be attached between transverse electric push rod 25 and traversing carriage 26 rear end face, traversing carriage 26
Rear end is isosceles triangle column structure, and traversing carriage 26 front end is evenly arranged with fixed strip, and mask 27 is fixed on mobile
On the fixed strip of frame 26 front end, mask 27 is in forme fruste spherical shell structure, and mask 27 front end is provided with rubber ring, hides
Cover and be evenly arranged with coatings on cover 27 outer surface；When unmanned plane operation out of doors prominent chance thunderstorm weather situation, unmanned plane
May be selected by the bus stop near operating location to hide, when unmanned plane lands, transverse electric push rod 25 shrinks
Motion, two masks 27 pull open laterally, and unmanned plane drops to stop on pedestal 3, subtract by installing in stop pedestal 3 lower end
Shake device 1, serves good cushioning effect to unmanned plane landing, and after unmanned plane is stopped and stablized, transverse electric push rod 25 enters
Row stretching, two inside side closures of mask 27, and also mask 27 front end is provided with rubber ring, and two rubber rings are rubber
Tightly fitting together under glue suction, two masks 27 form a hemispherical insulating boot, to unmanned plane at thundery sky
Play a very good protection in the case of gas, and the overall high of masking device 2 can be regulated by longitudinal electric push rod 22
Degree, it is adaptable to the use of different terrain landforms.
As it is shown in figure 1, described stop pedestal 3 bottom is octagon slab construction, and stop a left side for pedestal 3 upper surface
Right both sides are respectively symmetrically and offer semicircle screens groove, can be to dropping to stop the nothing on pedestal 3 by semicircle screens groove
The man-machine position that carries out is fixed, and the center position stopping pedestal 3 upper surface offers circular hole, and the outside stopping pedestal 3 is provided with
Surrounding edge, is evenly arranged with signal lights successively outside surrounding edge, signal lights serves the effect at night to position indicating of the present invention.
The ultimate principle of the present invention, principal character and advantage have more than been shown and described.The technical staff of the industry should
Understanding, the present invention is not restricted to the described embodiments, the simply explanation present invention's of the description in above-described embodiment and description
Principle, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these change and change
Enter to both fall within scope of the claimed invention.Claimed scope is by appending claims and equivalent thereof
Define.
Claims (3)
1. a multi-rotor aerocraft intelligent docking equipment, it is characterised in that: include damping device, masking device and stop base
Seat；The quantity of described masking device is two, and masking device lays respectively at about damping device along the central axis of damping device
Both sides, stop pedestal and are positioned at directly over damping device, and stop between pedestal and damping device connected；Wherein:
Described damping device includes lower fixed seat, upper fixed seat, redundancy parallel mechanism and damping；Described redundant parallel
Mechanism is between lower fixed seat and upper fixed seat, and redundancy parallel mechanism lower end is connected with lower fixed seat, redundant parallel
Structure upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at outside redundancy parallel mechanism, and subtracts
Shake mechanism is uniformly arranged circumferentially about along the central axis of redundancy parallel mechanism；
Described redundancy parallel mechanism includes fixed platform, moving platform, the first side chain and the second side chain；Described fixed platform is flat with dynamic
Platform is disc-shaped structure, and moving platform is positioned at directly over fixed platform；The first described side chain and the quantity of the second side chain are
Two, the first side chain and the second side chain are respectively positioned between fixed platform and moving platform, and the two ends of the first side chain and the second side chain are respectively
It is connected with fixed platform and moving platform, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；
The first described side chain includes the first ear mount, Hooke's hinge, the first electric pushrod, the first spherical hinge, first connects post and the
One vibrating spring；The first described ear mount is fixed on fixed platform upper surface, between the first ear mount and the first electric pushrod lower end
Employing Hooke's hinge is attached, and the first electric pushrod upper end is connected with the first spherical hinge, and the first spherical hinge is by the first connection
Post is fixed on the lower surface of moving platform, and the first vibrating spring is around being enclosed within the first electric pushrod；
Described stop base bottom is octagon slab construction, and the left and right sides stopping pedestal upper surface is respectively symmetrically out
Being provided with semicircle screens groove, the center position stopping pedestal upper surface offers circular hole, and the outside of stop pedestal is provided with encloses
Limit, is evenly arranged with signal lights successively outside surrounding edge；
Described masking device includes connecting base, longitudinal electric push rod, shock-proof spring, lifting support, transverse electric push rod, shifting
Dynamic support and mask；Described connection pan frontward end is provided with paliform link, connects base rear end and is provided with waist template,
Longitudinal electric push rod linearly type is equally spaced to be connected between base and lifting support, and longitudinal electric push rod bottom and waist
Template is connected, and longitudinal electric push rod top is connected with lifting support, and shock-proof spring, around being enclosed within longitudinal electric push rod, lifts
Bearing is of an L-shaped structure, and is provided with floor between the vertical of lifting support and horizontal plane, and transverse electric push rod bottom is fixed on
On lifting support, the mode of threaded engagement between transverse electric push rod and traversing carriage rear end face, is used to be attached, mobile
Frame rear end is isosceles triangle column structure, and traversing carriage front end is evenly arranged with fixed strip, and mask is fixed on traversing carriage
On the fixed strip of front end, mask is forme fruste spherical shell structure, and mask front end is provided with rubber ring, mask appearance
Coatings it is evenly arranged with on face.
A kind of multi-rotor aerocraft intelligent docking equipment the most according to claim 1, it is characterised in that: described damping machine
Structure includes mounting post, lower mounting post and damping stage clip；Described upper mounting post and the lower the most T-shaped structure of mounting post, upper installation
Post upper end and lower mounting post lower end are provided with external screw thread, upper mounting post lower end and lower mounting post upper end respectively and are provided with respectively
Lock sleeve, uses the mode of threaded engagement to be attached between upper mounting post upper end and upper fixed seat, lower mounting post lower end with under
Between fixing seat, the mode also by threaded engagement is attached, damping stage clip two ends be separately mounted to mounting post lower end and under
Mounting post upper end.
A kind of multi-rotor aerocraft intelligent docking equipment the most according to claim 1, it is characterised in that: described second
Chain includes the second ear mount, rotational pin, the second electric pushrod, the second spherical hinge, the second connection post and the second vibrating spring；Described
Second ear mount is fixed on fixed platform upper surface, uses rotational pin to carry out even between the second ear mount and the second electric pushrod lower end
Connecing, the second electric pushrod upper end is connected with the second spherical hinge, and the second spherical hinge connects post by second and is fixed on moving platform
On lower surface, the second vibrating spring is around being enclosed within the second electric pushrod.
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| CN201610491228.4A CN106122361A (en) | 2016-06-28 | 2016-06-28 | A kind of multi-rotor aerocraft intelligent docking equipment |
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Cited By (5)
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| CN106602786A (en) * | 2017-02-21 | 2017-04-26 | 浙江永发机电有限公司 | Vehicle motor |
| CN106763479A (en) * | 2016-12-20 | 2017-05-31 | 合肥中辰轻工机械有限公司 | A kind of sterilization machine cushioning and supporting device |
| CN107878696A (en) * | 2017-10-08 | 2018-04-06 | 常州工学院 | A kind of unmanned plane detection device for offshore floating photovoltaic module |
| CN110127071A (en) * | 2019-05-21 | 2019-08-16 | 北京三快在线科技有限公司 | A kind of unmanned plane landing platform |
| CN113389834A (en) * | 2021-06-15 | 2021-09-14 | 上海和鸣与行航空科技有限公司 | Cabin damping base for aircraft simulator |
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| CN106602786A (en) * | 2017-02-21 | 2017-04-26 | 浙江永发机电有限公司 | Vehicle motor |
| CN107878696A (en) * | 2017-10-08 | 2018-04-06 | 常州工学院 | A kind of unmanned plane detection device for offshore floating photovoltaic module |
| CN110127071A (en) * | 2019-05-21 | 2019-08-16 | 北京三快在线科技有限公司 | A kind of unmanned plane landing platform |
| CN113389834A (en) * | 2021-06-15 | 2021-09-14 | 上海和鸣与行航空科技有限公司 | Cabin damping base for aircraft simulator |
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Application publication date: 20161116 |