CN106114900B - A kind of safe electric power investigation aircraft stopping platform - Google Patents
A kind of safe electric power investigation aircraft stopping platform Download PDFInfo
- Publication number
- CN106114900B CN106114900B CN201610512060.0A CN201610512060A CN106114900B CN 106114900 B CN106114900 B CN 106114900B CN 201610512060 A CN201610512060 A CN 201610512060A CN 106114900 B CN106114900 B CN 106114900B
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- damping
- mounting post
- mobile
- push rod
- pedestal
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/005—Protective coverings for aircraft not in use
-
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The present invention relates to a kind of safe electric power to investigate aircraft stopping platform, including damping device, masking device and stops pedestal；The quantity of the masking device is two, and masking device is located at left and right sides of damping device respectively along the central axis of damping device, stops pedestal and is located at right over damping device, and stops and be connected between pedestal and damping device.Electric power investigation aircraft when the present invention can be to outdoor study provides stop protection in prominent thunderstorm weather of meeting; and damping performance is good when stopping; it is high to limit stationarity; avoid electric power investigation aircraft thunderstorm weather flight easily cause electric shock or lightning stroke the problem of so that electric power investigation aircraft operation safety be greatly improved.
Description
Technical field
The present invention relates to electric intelligent field of mechanical technique, specifically a kind of safe electric power investigation aircraft stops
By platform.
Background technology
With information-based development, the electric power facilities such as the electric wire for the laying that grows on trees outdoors and signal tower, by
In these electric power facilities all there are some potential safety problems and with damaging often, the failure of current electric power facility is investigated
Detection is mostly carried out using artificial, also there is a small amount of intelligent electric power investigation detection device, the detection device point of intelligent electric power investigation at present
For terrestrial detection device and aerial type detection device, associate power mostly is worn using unmanned plane for aerial type detection device and is detectd
It checks and surveys machine and carry out investigations detection, electric power investigation aircraft can also be referred to as, electric power investigates aircraft and is mainly used for complexity
The patrol and detection for the electric wire being laid at terrain, is then sent back by figure and is checked for electric power service personnel, greatly
Manpower is eliminated, and safe；When electric power investigates aircraft operation outdoors, if prominent meet thunderstorm situation, due to electricity
Power investigation aircraft flies in the air, it is easy to cause to get an electric shock or be struck by lightning, safety is by very big threat, in consideration of it, this hair
It is bright to provide a kind of safe electric power investigation aircraft stopping platform.
Invention content
In order to make up for the deficiencies of the prior art, it is stopped the present invention provides a kind of safe electric power investigation aircraft flat
Platform.
The present invention to be solved its technical problem and be realized using following technical scheme.
A kind of safe electric power investigation aircraft stopping platform, including damping device, masking device and stops pedestal；
The quantity of the masking device is two, and masking device is located at damping device or so two respectively along the central axis of damping device
Side is stopped pedestal and is located at right over damping device, and stops and be connected between pedestal and damping device.
Further, the damping device includes lower fixed seat, upper fixed seat, series-parallel connection vibration-damped table and damping；It is described
Series-parallel connection vibration-damped table between lower fixed seat and upper fixed seat, and series-parallel connection vibration-damped table lower end is connected with lower fixed seat, series-parallel connection
Vibration-damped table upper end is connected with upper fixed seat, and damping quantity is eight, and damping is located on the outside of series-parallel connection vibration-damped table respectively, and
Damping is uniformly arranged circumferentially about along the central axis of series-parallel connection vibration-damped table.
Further, the series-parallel connection vibration-damped table includes fixed platform, moving platform, damping branch and mobile support saddle, and damping branch
The quantity of chain and mobile support saddle is four；The moving platform is located at right over fixed platform, and damping branch is respectively symmetrically located at dynamic
Between platform and fixed platform, damping branch upper end is connected with moving platform, and damping branch lower end is mounted on mobile support saddle, mobile
Bearing is fixed on fixed platform；The damping branch includes elevating lever, ear mount, shaft, connecting seat, spherical hinge and damping bullet
Spring, elevating lever bottom end by shaft be mounted on ear mount on, elevating lever top is connected with connecting seat one end, the connecting seat other end and
Spherical hinge is connected, and damping spring is around being sleeved on elevating lever；The mobile support saddle includes directive slide track, mobile sliding block and limiting
Spring, directive slide track both ends are respectively arranged with limit card board, and mobile sliding block is mounted on directive slide track, at left and right sides of mobile sliding block
Be respectively arranged with installation ear mount, limit spring one end is connected with the limit card board on directive slide track, the limit spring other end with
Installation ear mount on mobile sliding block is connected；Fixed platform, moving platform and damping branch constitute 4-RPS four-freedom parallels
The movement that a translation three rotates totally four degree of freedom directions can be achieved in structure in space, and space is small, movement velocity is fast,
Kinematic dexterity is good and damping performance is good, when aircraft, which lands, to be stopped, even if attitude of flight vehicle is unstable or skewed,
Series-parallel connection vibration-damped table passes through spatial movement, the elimination of displacement difference and supplement when reaching aircraft landing, so as to play the good of damping
Good effect, it is ensured that stability of the aircraft in landing, jitter is small, and vibration is to the damage of aircraft fuselage when reducing landing
Wound.
Further, the damping includes upper mounting post, lower mounting post and damping compression spring；The upper mounting post and
The lower T-shaped structure of mounting post, upper mounting post upper end and lower mounting post lower end are respectively provided with external screw thread, upper mounting post lower end
Lock sleeve is respectively provided with lower mounting post upper end, between upper mounting post upper end and upper fixed seat by the way of thread fitting
It is attached, is attached between lower mounting post lower end and lower fixed seat also by the mode of thread fitting, damping compression spring both ends
It is separately mounted to mounting post lower end and lower mounting post upper end；Damping plays damping device the effect of secondary shock-absorbing,
So that damping device has the effect of dual shock absorption, damping performance is greatly improved.
Further, the masking device includes connect base, longitudinal electric push rod, shock-proof spring, lifting support, transverse direction
Electric pushrod, mobile stent and mask；The connect base front end is provided with paliform link, and connect base rear end is set
Waist template is equipped with, longitudinal electric push rod is of a straight line type at equal intervals between connect base and lifting support, and longitudinal electric
Push rod bottom end is connected with waist template, and longitudinal electric push rod top is connected with lifting support, and shock-proof spring is around being sleeved on longitudinal electricity
On dynamic push rod, lifting support is of an L-shaped structure, and floor, transverse electric are provided between the vertical plane and horizontal plane of lifting support
Push rod bottom end is fixed on lifting support, between transverse electric push rod and mobile back-end support face by the way of thread fitting into
Row connection, mobile back-end support are isosceles triangle column structure, and mobile stent front end is evenly arranged with fixed strip, and mask is solid
It is scheduled on the fixed strip of mobile stent front end, mask is in forme fruste spherical shell structure, and mask front end is provided with rubber
Circle covers and is evenly arranged with coatings on cover outer surface；When electric power investigation aircraft outdoors operation dash forward meet thunderstorm weather feelings
During condition, the bus stop that electric power investigation aircraft may be selected by near operating location is hidden, when electric power investigation aircraft drop
When falling, transverse electric push rod carries out contractile motion, and two masks pull open outward, and electric power investigation aircraft drops to stop base
On seat, by stopping pedestal lower end installation damping device, good cushioning effect is played to electric power investigation aircraft landing,
After electric power investigation aircraft, which is stopped, to be stablized, transverse electric push rod carries out stretching routine, and two masks are closed inwardly, and
Mask front end is provided with rubber ring, and two rubber rings tightly fit together under rubber suction, two mask shapes
Into a hemispherical insulating boot, play a very good protection to electric power investigation aircraft in thunderstorm weather, and
The whole height of masking device can be adjusted by longitudinal electric push rod, suitable for the use of different terrain landforms.
Further, the stop base bottom is in octagon slab construction, and stops the left and right two of pedestal upper surface
Side respectively symmetrically offers semicircle screens slot, by semicircle screens slot can to drop to stop pedestal on unmanned plane into
Line position puts fixation, and the center position for stopping pedestal upper surface offers circular hole, stops and surrounding edge is provided on the outside of pedestal, surrounding edge
Outside is evenly arranged with signal lamp successively, and signal lamp plays the role of at night to position indicating of the present invention.
Compared with prior art, the present invention has the following advantages：
(1) the electric power investigation aircraft when present invention can be to outdoor study provides to stop in prominent chance thunderstorm weather to be protected
Shield, and damping performance is good when stopping, limiting stationarity is high, avoid electric power investigation aircraft easily caused in thunderstorm weather flight it is tactile
The problem of electricity or lightning stroke so that the safety of electric power investigation aircraft operation is greatly improved.
(2) fixed platform, moving platform and damping branch of the invention constitute 4-RPS four-freedom parallel mechanisms, in space
The interior movement that a translation three can be achieved and rotate totally four degree of freedom directions, and space is small, movement velocity is fast, kinematic dexterity
Good and damping performance is good, when aircraft, which lands, to be stopped, even if attitude of flight vehicle is unstable or skewed, and series-parallel connection vibration-damped table
Pass through spatial movement, the elimination of displacement difference and supplement when reaching aircraft landing, so as to play the good result of damping, it is ensured that
Stability of the aircraft in landing, jitter is small, damage of the vibration to aircraft fuselage when reducing landing.
(3) masking device of the invention is using opposite opened folding form, opens and closes simple and fast, and when closing seals
Property it is good, insulating properties is high, and whole height is adjusted, suitable for the use of different terrain landforms, aircraft is investigated to electric power in thunder
It plays a very good protection in the case of rainy day gas.
Description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the dimensional structure diagram of the present invention；
Fig. 2 is the dimensional structure diagram of damping device of the present invention；
Dimensional structure diagram when Fig. 3 is two masking device cooperations of the present invention；
Fig. 4 is the dimensional structure diagram of masking device of the present invention；
Fig. 5 is the dimensional structure diagram of series-parallel connection vibration-damped table of the present invention；
Fig. 6 is the dimensional structure diagram of damping branch of the present invention.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Figures 1 to 6, a kind of safe electric power investigation aircraft stopping platform, including damping device 1, hides
It covers device 2 and stops pedestal 3；The quantity of the masking device 2 is two, central axis point of the masking device 2 along damping device 1
Not Wei Yu the left and right sides of damping device 1, stop pedestal 3 and be located at right over damping device 1, and stop pedestal 3 and damping device 1 it
Between be connected.
As shown in Fig. 2, the damping device 1 includes lower fixed seat 11, upper fixed seat 12, series-parallel connection vibration-damped table 13 and damping
Mechanism 14；The series-parallel connection vibration-damped table 13 between lower fixed seat 11 and upper fixed seat 12, and 13 lower end of series-parallel connection vibration-damped table with
Lower fixed seat 11 is connected, and 13 upper end of series-parallel connection vibration-damped table is connected with upper fixed seat 12, and 14 quantity of damping is eight, damping machine
Structure 14 is located at the outside of series-parallel connection vibration-damped table 13 respectively, and central axis uniformly circumferentially cloth of the damping 14 along series-parallel connection vibration-damped table 13
It puts.
As shown in Figure 5 and Figure 6, the series-parallel connection vibration-damped table 13 includes fixed platform 131, moving platform 132, damping branch 133
With mobile support saddle 134, and the quantity of damping branch 133 and mobile support saddle 134 is four；The moving platform 132, which is located at, to be allocated
Right over platform 131, damping branch 133 respectively symmetrically positioned at moving platform 132 and fixed platform 131 between, 133 upper end of damping branch and
Moving platform 132 is connected, and 133 lower end of damping branch is mounted on mobile support saddle 134, and mobile support saddle 134 is fixed on fixed platform 131
On；The damping branch 133 includes elevating lever 1331, ear mount 1332, shaft 1333, connecting seat 1334,1335 and of spherical hinge
Damping spring 1336,1331 bottom end of elevating lever are mounted on by shaft 1333 in ear mount 1332, and 1331 top of elevating lever is with connecting
1334 one end of seat are connected, and 1334 other end of connecting seat is connected with spherical hinge 1335, and damping spring 1336 is around being sleeved on elevating lever
On 1331；The mobile support saddle 134 includes directive slide track 1341, mobile sliding block 1342 and limit spring 1343, directive slide track
1341 both ends are respectively arranged with limit card board, and mobile sliding block 1342 is mounted on directive slide track 1341, mobile sliding block 1342 or so
Both sides are respectively arranged with installation ear mount, and 1343 one end of limit spring is connected with the limit card board on directive slide track 1341, limiting
1343 other end of spring is connected with the installation ear mount on mobile sliding block 1342；Fixed platform 131, moving platform 132 and damping branch
133 constitute 4-RPS four-freedom parallel mechanisms, and the fortune that a translation three rotates totally four degree of freedom directions can be achieved in space
It is dynamic, and space is small, movement velocity is fast, kinematic dexterity is good and damping performance is good, when aircraft, which lands, to be stopped, even if flying
When row device posture is unstable or skewed, series-parallel connection vibration-damped table 13 is by spatial movement, displacement difference when reaching aircraft landing
It eliminates and supplements, so as to play the good result of damping, it is ensured that stability of the aircraft in landing, jitter is small, subtracts
Damage of the vibration to aircraft fuselage during small landing.
As shown in Fig. 2, the damping 14 includes upper mounting post 141, lower mounting post 142 and damping compression spring 143；Institute
The upper mounting post 141 and the T-shaped structure of lower mounting post 142 stated, upper 141 upper end of mounting post and lower 142 lower end of mounting post are divided equally
It is not provided with external screw thread, upper 141 lower end of mounting post and lower 142 upper end of mounting post are respectively provided with lock sleeve, upper mounting post 141
Be attached by the way of thread fitting between upper end and upper fixed seat 12, lower 142 lower end of mounting post and lower fixed seat 11 it
Between be attached also by the mode of thread fitting, 143 both ends of damping compression spring are separately mounted to 141 lower end of mounting post and lower peace
Fill 142 upper end of column；Damping 14 plays damping device the effect of secondary shock-absorbing so that damping device 1 has dual subtract
The effect of shake, damping performance are greatly improved.
As shown in Figure 3 and Figure 4, the masking device 2 includes connect base 21, longitudinal electric push rod 22, shock-proof spring
23rd, lifting support 24, transverse electric push rod 25, mobile stent 26 and mask 27；21 front end of connect base is provided with
Paliform link, 21 rear end of connect base are provided with waist template, and longitudinal electric push rod 22, which is of a straight line type to be located at equal intervals, to be connected
It connects between pedestal 21 and lifting support 24, and 22 bottom end of longitudinal electric push rod is connected with waist template, longitudinal electric push rod 22 pushes up
End is connected with lifting support 24, and around being sleeved on longitudinal electric push rod 22, lifting support 24 is of an L-shaped structure shock-proof spring 23, and
Floor is provided between the vertical plane and horizontal plane of lifting support 24,25 bottom end of transverse electric push rod is fixed on lifting support 24
On, it is attached by the way of thread fitting between 26 rear end face of transverse electric push rod 25 and mobile stent, mobile stent 26
Rear end is isosceles triangle column structure, and mobile 26 front end of stent is evenly arranged with fixed strip, and mask 27 is fixed on mobile branch
On the fixed strip of 26 front end of frame, mask 27 is in forme fruste spherical shell structure, and 27 front end of mask is provided with rubber ring, is hidden
It covers and is evenly arranged with coatings on 27 outer surface of cover；When electric power investigation aircraft outdoors operation dash forward meet thunderstorm weather situation
When, the bus stop that electric power investigation aircraft may be selected by near operating location is hidden, when electric power investigation aircraft landing
When, transverse electric push rod 25 carries out contractile motion, and two masks 27 pull open outward, and electric power investigation aircraft drops to stop
On pedestal 3, by stopping 3 lower end of pedestal installation damping device 1, good damping is played to electric power investigation aircraft landing
Effect, after electric power investigation aircraft, which is stopped, to be stablized, transverse electric push rod 25 carries out stretching routine, and two masks 27 are inwardly
It closes, and 27 front end of mask is provided with rubber ring, two rubber rings tightly fit together under rubber suction, and two
A mask 27 forms a hemispherical insulating boot, and good guarantor is played in thunderstorm weather to electric power investigation aircraft
Shield acts on, and the whole height of masking device 2 can be adjusted by longitudinal electric push rod 22, suitable for different terrain landforms
It uses.
As shown in Figure 1,3 bottom end of stop pedestal is in octagon slab construction, and stop a left side for 3 upper surface of pedestal
Right both sides respectively symmetrically offer semicircle screens slot, can be to dropping to the electricity stopped on pedestal 3 by semicircle screens slot
Power investigation aircraft carries out position and fixes, and the center position for stopping 3 upper surface of pedestal offers circular hole, stops the outer of pedestal 3
Side is provided with surrounding edge, is evenly arranged with signal lamp successively on the outside of surrounding edge, signal lamp is played at night to position indicating of the present invention
Effect.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the description in above embodiments and description only illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these change and change
Into all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
It defines.
Claims (1)
1. a kind of safe electric power investigation aircraft stopping platform, it is characterised in that：Including damping device, masking device and
Stop pedestal；The quantity of the masking device is two, and the central axis of masking device along damping device is located at damping and fills respectively
The left and right sides is put, pedestal is stopped and is located at right over damping device, and stops and is connected between pedestal and damping device；Wherein：
The damping device includes lower fixed seat, upper fixed seat, series-parallel connection vibration-damped table and damping；The series-parallel connection vibration-damped table
Between lower fixed seat and upper fixed seat, and series-parallel connection vibration-damped table lower end is connected with lower fixed seat, series-parallel connection vibration-damped table upper end with
Upper fixed seat is connected, and damping quantity is eight, and damping is located on the outside of series-parallel connection vibration-damped table respectively, and damping edge is mixed
The central axis of connection vibration-damped table is uniformly arranged circumferentially about；
The series-parallel connection vibration-damped table includes fixed platform, moving platform, damping branch and mobile support saddle, and damping branch and mobile support saddle
Quantity be four；The moving platform is located at right over fixed platform, and damping branch is respectively symmetrically located at moving platform and fixed platform
Between, damping branch upper end is connected with moving platform, and damping branch lower end is mounted on mobile support saddle, and mobile support saddle is fixed on fixed
On platform；
The damping branch includes elevating lever, ear mount, shaft, connecting seat, spherical hinge and damping spring, and elevating lever bottom end passes through
Shaft is mounted in ear mount, and elevating lever top is connected with connecting seat one end, and the connecting seat other end is connected with spherical hinge, damping
Spring is around being sleeved on elevating lever；
The mobile support saddle includes directive slide track, mobile sliding block and limit spring, directive slide track both ends and is respectively arranged with limiting
Snap-gauge, mobile sliding block are mounted on directive slide track, and installation ear mount, limit spring one end are respectively arranged at left and right sides of mobile sliding block
It is connected with the limit card board on directive slide track, the limit spring other end is connected with the installation ear mount on mobile sliding block；
The masking device includes connect base, longitudinal electric push rod, shock-proof spring, lifting support, transverse electric push rod, moves
Dynamic stent and mask；The connect base front end is provided with paliform link, and connect base rear end is provided with waist template,
Longitudinal electric push rod is of a straight line type at equal intervals between connect base and lifting support, and longitudinal electric push rod bottom end and waist
Template is connected, and longitudinal electric push rod top is connected with lifting support, and shock-proof spring is lifted around being sleeved on longitudinal electric push rod
Bearing is of an L-shaped structure, and floor is provided between the vertical plane and horizontal plane of lifting support, and transverse electric push rod bottom end is fixed on
It on lifting support, is attached by the way of thread fitting between transverse electric push rod and mobile back-end support face, mobile branch
Frame rear end is isosceles triangle column structure, and mobile stent front end is evenly arranged with fixed strip, and mask is fixed on mobile stent
On the fixed strip of front end, mask is in forme fruste spherical shell structure, and mask front end is provided with rubber ring, mask appearance
Coatings are evenly arranged on face；
The stop base bottom is in octagon slab construction, and the left and right sides for stopping pedestal upper surface is respectively symmetrically opened
Equipped with semicircle screens slot, the center position for stopping pedestal upper surface offers circular hole, stops to be provided on the outside of pedestal and enclose
Side, surrounding edge outside are evenly arranged with signal lamp successively；
The damping includes upper mounting post, lower mounting post and damping compression spring；The upper mounting post and lower mounting post are equal
T-shaped structure, upper mounting post upper end and lower mounting post lower end are respectively provided with external screw thread, upper mounting post lower end and lower mounting post
Upper end is respectively provided with lock sleeve, is attached by the way of thread fitting between upper mounting post upper end and upper fixed seat,
It is attached between lower mounting post lower end and lower fixed seat also by the mode of thread fitting, damping compression spring both ends are separately mounted to
Upper mounting post lower end and lower mounting post upper end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610512060.0A CN106114900B (en) | 2016-06-28 | 2016-06-28 | A kind of safe electric power investigation aircraft stopping platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610512060.0A CN106114900B (en) | 2016-06-28 | 2016-06-28 | A kind of safe electric power investigation aircraft stopping platform |
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| Publication Number | Publication Date |
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| CN106114900A CN106114900A (en) | 2016-11-16 |
| CN106114900B true CN106114900B (en) | 2018-06-26 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610512060.0A Active CN106114900B (en) | 2016-06-28 | 2016-06-28 | A kind of safe electric power investigation aircraft stopping platform |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108583898A (en) * | 2018-05-09 | 2018-09-28 | 孙晖 | A kind of independent-suspension damping device of unmanned plane jet pipe |
| US10625876B2 (en) * | 2018-08-08 | 2020-04-21 | Aurora Flight Sciences Corporation | Aircraft landing systems and methods for monitoring a vertical landing of an aircraft |
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| CN202271897U (en) * | 2011-07-06 | 2012-06-13 | 珠海银通新能源有限公司 | Service guarantee vehicle for field operation of electric unmanned helicopter |
| CN104029711A (en) * | 2014-06-25 | 2014-09-10 | 王松豪 | Multi-dimensional shock-absorbing baby carriage |
| CN104154170A (en) * | 2014-08-01 | 2014-11-19 | 安徽工程大学 | Parallel mechanism based multidimensional vibration platform |
| CN104908933A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Protective cover of multi-rotor aircraft |
| CN105240445A (en) * | 2015-11-17 | 2016-01-13 | 哈尔滨工业大学 | Semi-active six-freedom-degree vibration damping platform |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9561871B2 (en) * | 2014-05-07 | 2017-02-07 | Deere & Company | UAV docking system and method |
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2016
- 2016-06-28 CN CN201610512060.0A patent/CN106114900B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202271897U (en) * | 2011-07-06 | 2012-06-13 | 珠海银通新能源有限公司 | Service guarantee vehicle for field operation of electric unmanned helicopter |
| CN104029711A (en) * | 2014-06-25 | 2014-09-10 | 王松豪 | Multi-dimensional shock-absorbing baby carriage |
| CN104154170A (en) * | 2014-08-01 | 2014-11-19 | 安徽工程大学 | Parallel mechanism based multidimensional vibration platform |
| CN104908933A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Protective cover of multi-rotor aircraft |
| CN105240445A (en) * | 2015-11-17 | 2016-01-13 | 哈尔滨工业大学 | Semi-active six-freedom-degree vibration damping platform |
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| CN106114900A (en) | 2016-11-16 |
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