CN108146649A - A kind of unmanned plane Portable lifting platform - Google Patents
A kind of unmanned plane Portable lifting platform Download PDFInfo
- Publication number
- CN108146649A CN108146649A CN201810137941.8A CN201810137941A CN108146649A CN 108146649 A CN108146649 A CN 108146649A CN 201810137941 A CN201810137941 A CN 201810137941A CN 108146649 A CN108146649 A CN 108146649A
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- Prior art keywords
- lifting platform
- unmanned plane
- pressure
- bearing rod
- fixed block
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- 239000000463 material Substances 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 abstract description 4
- 238000013016 damping Methods 0.000 abstract description 3
- 241000167854 Bourreria succulenta Species 0.000 abstract description 2
- 235000019693 cherries Nutrition 0.000 abstract description 2
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000000872 buffer Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- 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
- B64F1/007—Helicopter portable landing pads
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
Abstract
The invention discloses a kind of unmanned plane Portable lifting platforms, including lifting platform, the upper end of the lifting platform is provided with unmanned plane ontology, and the lower end of lifting platform is provided with pressure-bearing rod, the lower end of the lifting platform is installed with the first fixed block close to the side of pressure-bearing rod, the lower end of the pressure-bearing rod is connected with baffle-box, and the inside of the baffle-box is equipped with second spring close to the side of pressure-bearing rod.Unmanned plane Portable lifting platform, by being provided with floor push and electric hydaulic bar, user can be very easily so that electric hydaulic bar rises or landing, suitable height of taking off can be provided when taking off for unmanned plane ontology, there is provided pulleys, and the position of lower plate and then cherry picker is moved convenient for user, there is provided baffle-boxs and pressure-bearing rod, when lifting platform is shaken, it can play the role of buffering external force and damping, greatly reduce the vibration of lifting platform.
Description
Technical field
The present invention relates to unmanned air vehicle technique field more particularly to a kind of unmanned plane Portable lifting platforms.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled,
Unmanned plane is simple in structure, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably performing for task, and unmanned plane will carry out flight service's reason when taking off on hoistable platform, flight or drop to unmanned plane
It falls and important platform is provided.
But unmanned plane lifting platform currently on the market is complicated, and function is single, is not provided with floor push and electricity
Hydrodynamic compression bar is not easy to lifting platform and adjusts height, and it is suitable using height to be not easy to provide for the flight of unmanned plane, is not provided with
Pulley, the person of being not convenient to use move lower plate, are not provided with pressure-bearing rod and baffle-box, it is impossible to lifting platform by outer masterpiece
Used time buffers external force.
Invention content
The purpose of the present invention is to solve problem in the prior art, and a kind of unmanned plane proposed is put down with Portable lifting
Platform.
To achieve these goals, present invention employs following technical solutions:A kind of unmanned plane Portable lifting platform,
Including lifting platform, the upper end of the lifting platform is provided with unmanned plane ontology, and the lower end of lifting platform is provided with pressure-bearing rod, the liter
The lower end of drop platform is installed with the first fixed block close to the side of pressure-bearing rod, and the lower end of the pressure-bearing rod is connected with baffle-box,
The inside of the baffle-box is equipped with second spring close to the side of pressure-bearing rod, and the lower end of baffle-box is fixedly connected with bottom
Plate, the upper end of the upper plate are provided with the first spring, and the upper end of upper plate is close to the first spring close to the side of baffle-box
Side be provided with the second fixed block, electric hydaulic bar is installed in the middle part of the upper plate, the electric hydaulic bar
Lower end is fixedly connected with lower plate, floor push is provided on front side of the lower plate, and the upper end of lower plate is close to electronic liquid
The side of compression bar is provided with accumulator, and the lower end of the lower plate is provided with pulley, the input terminal and foot of the electric hydaulic bar
The output terminal for stepping on switch is electrically connected, and the input terminal of the floor push and the output terminal of accumulator are electrically connected.
Preferably, the lower end of first fixed block is connected with motion bar, and the first fixed block and the first spring pass through work
Lever is fixedly connected, and the lower end of motion bar is connected with the first spring.
Preferably, first fixed block is rotatablely connected with motion bar by first rotating shaft, second fixed block and work
Lever is rotatablely connected by the second shaft.
Preferably, there are four the pulley is set altogether, and the bottom end side of pulley is both provided with brake, the pulley with
Lower plate is bolted to connection.
Preferably, the lower end of the pressure-bearing rod is connected with second spring, and pressure-bearing rod is a kind of component of PC plastic material.
Preferably, the electric hydaulic bar is fixedly connected with upper plate by upper fixed block, and electric hydaulic bar and bottom
Plate is fixedly connected by lower fixed block.
Compared with prior art, the present invention provides a kind of unmanned plane Portable lifting platform, have following
Advantageous effect:
1st, unmanned plane Portable lifting platform, by being provided with floor push and electric hydaulic bar, user can be with
Very easily so that electric hydaulic bar rises or landing, when in use, electric hydaulic bar rises, and can be that unmanned plane ontology exists
Height of suitably taking off is provided when taking off.
2nd, by being provided with pulley, lower plate and then shifting are moved convenient for user for unmanned plane Portable lifting platform
The position of dynamic lifting platform uses, time saving and energy saving, Portable high-efficiency convenient for the promotion of lifting platform.
3rd, unmanned plane Portable lifting platform, by being provided with baffle-box and pressure-bearing rod, when lifting platform is shaken
When, by the gearing of baffle-box and the first spring and motion bar, it can play the role of buffering external force and damping, drop significantly
The low vibration of lifting platform.
It is same as the prior art or the prior art can be used realized that part is not directed in the device, structure of the present invention
It is scientific and reasonable, it is simple to operate.
Description of the drawings
Fig. 1 is the structural diagram of the present invention;
Fig. 2 is the plan view of the present invention.
In figure:1st, lifting platform;2nd, unmanned plane ontology;3rd, the first fixed block;4th, pressure-bearing rod;5th, baffle-box;6th, second spring;
7th, the first spring;8th, the second fixed block;9th, upper plate;10th, electric hydaulic bar;11st, lower plate;12nd, floor push;13rd, electric power storage
Pond;14th, pulley.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.
In the description of the present invention, it is to be understood that term " on ", " under ", "front", "rear",
The orientation or position relationship of the instructions such as "left", "right", " top ", " bottom ", " interior ", " outer " are based on side shown in the drawings
Position or position relationship are for only for ease of the description present invention and simplify description rather than instruction or imply signified device or member
Part must have specific orientation, with specific azimuth configuration and operation, therefore be not considered as limiting the invention.
With reference to Fig. 1-2, a kind of unmanned plane Portable lifting platform, including lifting platform 1, the upper end of lifting platform 1 is provided with
Unmanned plane ontology 2, and the lower end of lifting platform 1 is provided with pressure-bearing rod 4, the lower end of lifting platform 1 is fixed close to the side of pressure-bearing rod 4 pacifies
Equipped with the first fixed block 3, the lower end of pressure-bearing rod 4 is connected with baffle-box 5, and the inside of baffle-box 5 is installed close to the side of pressure-bearing rod 4
There is second spring 6, and the lower end of baffle-box 5 is fixedly connected with upper plate 9, the upper end of upper plate 9 is set close to the side of baffle-box 5
The first spring 7 is equipped with, and the upper end of upper plate 9 is provided with the second fixed block 8 close to the side of the first spring 7, in upper plate 9
Portion is installed with electric hydaulic bar 10, and the lower end of electric hydaulic bar 10 is fixedly connected with lower plate 11, the front side of lower plate 11
Floor push 12 is provided with, and the upper end of lower plate 11 is provided with accumulator 13, lower plate close to the side of electric hydaulic bar 10
11 lower end is provided with pulley 14, and the input terminal of electric hydaulic bar 10 is electrically connected with the output terminal of floor push 12, foot-operated to open
12 input terminal is closed to be electrically connected with the output terminal of accumulator 13.
It is shaken to reduce lifting platform 1 by external force generation, in the present embodiment, it is preferred that the lower end of the first fixed block 3
Motion bar is connected with, and the first fixed block 3 is fixedly connected with the first spring 7 by motion bar, the lower end of motion bar is connected with
One spring 7.
For the ease of realizing the effect of buffering, in the present embodiment, it is preferred that the first fixed block 3 passes through first with motion bar
Shaft is rotatablely connected, and the second fixed block 8 is rotatablely connected with motion bar by the second shaft.
For the ease of mobile lower plate 11, in the present embodiment, it is preferred that pulley 14 is altogether there are four settings, and pulley 14
Bottom end side is both provided with brake, and pulley 14 is bolted to connection with lower plate 11.
In order to which baffle-box 5 works normally, in the present embodiment, it is preferred that the lower end of pressure-bearing rod 4 is connected with second spring 6, and
Pressure-bearing rod 4 is a kind of component of PC plastic material.
For the ease of electric hydaulic bar 10 is fixedly mounted, in the present embodiment, it is preferred that electric hydaulic bar 10 and upper plate 9
It is fixedly connected by upper fixed block, and electric hydaulic bar 10 is fixedly connected with lower plate 11 by lower fixed block.
The operation principle and process for using of the present invention:First user with floor push 12 to the height of electric hydaulic bar 10
It is adjusted, suitable height of taking off can be provided for unmanned plane ontology 2 when taking off, user can very easily utilize electricity
Hydrodynamic compression bar 10 rises or lands, and when in use, electric hydaulic bar 10 rises, and the lower end of lifting platform 1 is provided with pressure-bearing
Bar 4, the lower end of pressure-bearing rod 4 are connected with baffle-box 5, and the inside of baffle-box 5 is equipped with second spring 6 close to the side of pressure-bearing rod 4,
First fixed block 3 is rotatablely connected with motion bar by first rotating shaft, and the second fixed block 8 is rotated with motion bar by the second shaft to be connected
It connects, it, can by baffle-box with 5 and the gearing of 6 and first spring 7 of second spring and motion bar when lifting platform 1 is shaken
Play the role of buffering external force and damping, greatly reduce the vibration of lifting platform 1, and the lower end of lower plate 11 is provided with cunning
Wheel 14 can be convenient for user to move the position of lower plate 11 and then cherry picker 1, convenient for user's pushing away to lifting platform 1
It is dynamic to use, time saving and energy saving, Portable high-efficiency.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
- A kind of 1. unmanned plane Portable lifting platform, including lifting platform (1), which is characterized in that the upper end of the lifting platform (1) Unmanned plane ontology (2) is provided with, and the lower end of lifting platform (1) is provided with pressure-bearing rod (4), the lower end of the lifting platform (1) is close The side of pressure-bearing rod (4) is installed with the first fixed block (3), and the lower end of the pressure-bearing rod (4) is connected with baffle-box (5), institute The inside for stating baffle-box (5) is equipped with second spring (6), and the lower end of baffle-box (5) is fixed and connected close to the side of pressure-bearing rod (4) Upper plate (9) is connected to, the upper end of the upper plate (9) is provided with the first spring (7), and upper bottom close to the side of baffle-box (5) The upper end of plate (9) is provided with the second fixed block (8) close to the side of the first spring (7), and peace is fixed at the middle part of the upper plate (9) Equipped with electric hydaulic bar (10), the lower end of the electric hydaulic bar (10) is fixedly connected with lower plate (11), the lower plate (11) floor push (12) is provided on front side of, and the upper end of lower plate (11) is provided with close to the side of electric hydaulic bar (10) Accumulator (13), the lower end of the lower plate (11) are provided with pulley (14), the input terminal and foot of the electric hydaulic bar (10) The output terminal for stepping on switch (12) is electrically connected, and the output terminal of the input terminal and accumulator (13) of the floor push (12) electrically connects It connects.
- A kind of 2. unmanned plane Portable lifting platform according to claim 1, which is characterized in that first fixed block (3) lower end is connected with motion bar, and the first fixed block (3) is fixedly connected with the first spring (7) by motion bar, motion bar Lower end is connected with the first spring (7).
- A kind of 3. unmanned plane Portable lifting platform according to claim 1, which is characterized in that first fixed block (3) it is rotatablely connected with motion bar by first rotating shaft, second fixed block (8) is rotated with motion bar by the second shaft to be connected It connects.
- 4. a kind of unmanned plane Portable lifting platform according to claim 1, which is characterized in that the pulley (14) is altogether There are four settings, and the bottom end side of pulley (14) is both provided with brake, and the pulley (14) passes through spiral shell with lower plate (11) Bolt is fixedly connected.
- A kind of 5. unmanned plane Portable lifting platform according to claim 1, which is characterized in that the pressure-bearing rod (4) Lower end be connected with second spring (6), and pressure-bearing rod (4) be a kind of component of PC plastic material.
- A kind of 6. unmanned plane Portable lifting platform according to claim 1, which is characterized in that the electric hydaulic bar (10) it is fixedly connected with upper plate (9) by upper fixed block, and electric hydaulic bar (10) passes through lower fixed block with lower plate (11) It is fixedly connected.
Priority Applications (1)
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CN201810137941.8A CN108146649A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane Portable lifting platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810137941.8A CN108146649A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane Portable lifting platform |
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CN108146649A true CN108146649A (en) | 2018-06-12 |
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CN201810137941.8A Pending CN108146649A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane Portable lifting platform |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109141704A (en) * | 2018-11-08 | 2019-01-04 | 广西玉柴机器股份有限公司 | A kind of tractor PTO testing stand with raising speed case |
CN110077614A (en) * | 2019-04-24 | 2019-08-02 | 山东大学 | A kind of electromagnetic survey unmanned plane hoistable platform and working method |
CN110635393A (en) * | 2019-10-25 | 2019-12-31 | 江苏电卫士电力服务有限公司 | Electric power inspection system |
CN111409846A (en) * | 2020-04-30 | 2020-07-14 | 赵呈印 | Aircraft lifting device |
CN111924057A (en) * | 2020-07-13 | 2020-11-13 | 中南林业科技大学 | A landing aid device for a marine drone |
CN112373327A (en) * | 2020-10-23 | 2021-02-19 | 刘占波 | Unmanned aerial vehicle is with platform that charges |
FR3107036A1 (en) * | 2020-02-11 | 2021-08-13 | Naval Group | AIRCRAFT HANDLING SYSTEM AND NAVAL PLATFORM EQUIPPED WITH SUCH A SYSTEM |
CN113650797A (en) * | 2021-08-27 | 2021-11-16 | 广东电网有限责任公司 | Unmanned aerial vehicle patrols and examines operation platform |
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CN106564610A (en) * | 2016-10-26 | 2017-04-19 | 中国电子科技集团公司第四十八研究所 | Auxiliary taking-off and landing system for rotor unmanned plane |
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CN107215465A (en) * | 2017-06-28 | 2017-09-29 | 深圳市雷凌广通技术研发有限公司 | It is a kind of to be applied to the unmanned plane with shatter-resistant function of taking photo by plane |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
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CN109141704A (en) * | 2018-11-08 | 2019-01-04 | 广西玉柴机器股份有限公司 | A kind of tractor PTO testing stand with raising speed case |
CN110077614A (en) * | 2019-04-24 | 2019-08-02 | 山东大学 | A kind of electromagnetic survey unmanned plane hoistable platform and working method |
CN110077614B (en) * | 2019-04-24 | 2022-11-08 | 山东大学 | Electromagnetic exploration unmanned aerial vehicle lifting platform and working method |
CN110635393A (en) * | 2019-10-25 | 2019-12-31 | 江苏电卫士电力服务有限公司 | Electric power inspection system |
FR3107036A1 (en) * | 2020-02-11 | 2021-08-13 | Naval Group | AIRCRAFT HANDLING SYSTEM AND NAVAL PLATFORM EQUIPPED WITH SUCH A SYSTEM |
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CN111409846A (en) * | 2020-04-30 | 2020-07-14 | 赵呈印 | Aircraft lifting device |
CN111924057A (en) * | 2020-07-13 | 2020-11-13 | 中南林业科技大学 | A landing aid device for a marine drone |
CN112373327A (en) * | 2020-10-23 | 2021-02-19 | 刘占波 | Unmanned aerial vehicle is with platform that charges |
CN113650797A (en) * | 2021-08-27 | 2021-11-16 | 广东电网有限责任公司 | Unmanned aerial vehicle patrols and examines operation platform |
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Application publication date: 20180612 |