CN109533375A - A kind of unmanned plane stop locking mechanism - Google Patents
A kind of unmanned plane stop locking mechanism Download PDFInfo
- Publication number
- CN109533375A CN109533375A CN201811485910.8A CN201811485910A CN109533375A CN 109533375 A CN109533375 A CN 109533375A CN 201811485910 A CN201811485910 A CN 201811485910A CN 109533375 A CN109533375 A CN 109533375A
- Authority
- CN
- China
- Prior art keywords
- shell
- limit
- unmanned plane
- fixedly connected
- locking mechanism
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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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
- B64F1/12—Anchoring
- B64F1/125—Mooring or ground handling devices for helicopters
Abstract
The invention discloses a kind of unmanned planes to stop locking mechanism, is related to air vehicle technique field.The unmanned plane stops locking mechanism, including pedestal, the two sides at the top of the pedestal are fixedly connected with limited position mechanism, the top of the pedestal and indicator light is provided between two position-limit mechanisms, the controlling terminal of the indicator light and peripheral hardware is electrically connected, the position-limit mechanism includes limiting plate, limit shell is fixedly connected at the top of the limiting plate, guiding device is provided through at the top of the limit shell, the two sides of the limit shell inner cavity pass through spring hinge and are connected with rotating block.The unmanned plane stops locking mechanism, pass through the improvement of position-limit mechanism, transmission device, guiding device and stressing device, so that unmanned plane stops locking mechanism and can be very good that the unmanned plane that will land is guided to corresponding position and conducted the locking operations automatically, the operation difficulty of user is reduced.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of unmanned plane stops locking mechanism.
Background technique
Unmanned plane is a kind of unmanned vehicle manipulated by radio robot or itself presetting apparatus, with
The development in epoch, science and technology be constantly progressive, unmanned plane is gathered around in every field and is held out broad prospects, unmanned plane stop locking
Mechanism is that the mechanism of unmanned plane position is limited when a kind of stop for unmanned plane.
Traditional unmanned plane stops locking mechanism, it is difficult to well automatically guide the unmanned plane that will land to corresponding position
It sets and conducts the locking operations, increase the operation difficulty of user, use while reducing working efficiency to user is brought
It is inconvenient.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides a kind of unmanned planes to stop locking mechanism, solves unmanned plane and stops
The problem of unmanned plane that will land is guided to corresponding position and conducted the locking operations automatically well is difficult to by locking mechanism.
(2) technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs: a kind of unmanned plane stop locking mechanism,
Including pedestal, the two sides at the top of the pedestal are fixedly connected with limited position mechanism, the top of the pedestal and are located at two limits
Indicator light, the controlling terminal electric connection of the indicator light and peripheral hardware are provided between the mechanism of position.
The position-limit mechanism includes limiting plate, and limit shell, the limit are fixedly connected at the top of the limiting plate
Guiding device is provided through at the top of the shell of position, the two sides of the limit shell inner cavity are connected with by spring hinge
Rotating block, the rotating block is inlaid with permanent magnet close to the side of limit outer casing inner wall, described to limit the two of bottom of shell inner cavity
Side is fixedly connected to the coil plate being equipped with permanent magnet, and the two sides of the limit outer casing bottom are fixedly connected to metal
Bar, the top of the metallic rod are fixedly connected with stressing device, and the bottom of the stressing device is fixedly connected with transmission device, institute
The bottom for stating transmission device is provided with driving mechanism, and the bottom end of the metallic rod is fixedly connected with metal plate, the driving mechanism
It is electrically connected with the controlling terminal of peripheral hardware with coil plate.
The transmission device includes transmission shell, and the top of the transmission shell is fixedly connected with the bottom of stressing device,
The inner wall of the transmission shell is provided with transmission teeth, and the inner cavity of the transmission shell is provided with central gear, outside the transmission
The inner cavity of the shell and two sides for being located at central gear are connected with edge gear by shaft, the edge gear respectively with center
Gear and transmission teeth engagement, the output end of the driving mechanism run through the bottom of transmission shell and fix with central gear and connect
It connects.
The guiding device includes guiding shell, and the surface of the guiding shell is arranged with coil pipe, the guiding shell
The two sides of inner cavity are provided with guide rail bolt, and the surface of the guide rail bolt is provided with guide rail crawler belt, and guide rail crawler belt and guiding
The inner wall of shell is parallel, and the controlling terminal of the coil pipe and peripheral hardware is electrically connected.
The stressing device includes stress shell, and the two sides of the stress shell front surface are provided with snap-gauge, the card
Be provided through axis on plate, the bottom end of the axis sequentially pass through stress shell and be driven shell top and with edge gear
It is fixedly connected, the front surface of the stress shell offers the stress slot being equipped with unmanned plane supporting leg, in the stress slot
The bottom of chamber is provided with pressure sensor, the controlling terminal electric connection of the pressure sensor and peripheral hardware.
Preferably, the two sides of the pedestal are provided through installation bolt.
Preferably, the magnetic direction that the coil plate generates after being powered is identical as the magnetic direction of permanent magnet.
Preferably, the rotating block is provided with proof rubber far from the side of limit outer casing inner wall.
Preferably, the bottom of the rotating block is flexibly connected restricted bar by shaft, and the bottom end of the limitation bar is run through
It limits the bottom of shell and extends to the outside of limit shell, the bottom of the rotating block passes through in limited spring and limit shell
The bottom of chamber is fixedly connected, and limited spring is around the surface for being set to limitation bar.
Preferably, the inner cavity of the limit shell is provided with the directing plate being equipped with guiding device.
Preferably, the two sides of the metal plate are provided through rubber rods, the top of the rubber rods and limit shell
Bottom be fixedly connected, be fixedly connected at the top of the bottom end of the rubber rods and pedestal.
Preferably, rubber sleeve is arranged far from the side of axis in the snap-gauge.
(3) beneficial effect
The present invention provides a kind of unmanned planes to stop locking mechanism.Have following the utility model has the advantages that the unmanned plane stops locking
Mechanism, by the improvement of position-limit mechanism, transmission device, guiding device and stressing device, so that unmanned plane stop locking mechanism can
The unmanned plane that will land is guided to corresponding position and be conducted the locking operations automatically well, the operation of user is reduced
Difficulty, the use for the person of being convenient to use while improving working efficiency.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is the structural schematic diagram of position-limit mechanism of the present invention；
Fig. 3 is the structural schematic diagram of transmission device of the present invention；
Fig. 4 is the structural schematic diagram of guiding device of the present invention；
Fig. 5 is the structural schematic diagram of stressing device of the present invention.
In figure: 1, pedestal；2, bolt is installed；3, position-limit mechanism；301, directing plate；302, rotating block；303, proof rubber；
304, transmission device；3041, central gear；3042, edge gear；3043, teeth are driven；3044, it is driven shell；305, it drives
Mechanism；306, rubber rods；307, limiting plate；308, metal plate；309, metallic rod；310, guiding device；3101, guiding is outer
Shell；3102, coil pipe；3103, guide rail bolt；3104, guide rail crawler belt；311, limited spring；312, shell is limited；313, permanent magnetism
Body；314, coil plate；315, stressing device；3151, pressure sensor；3152, axis；3153, stress shell；3154, stress
Slot；3155, rubber sleeve；3156, snap-gauge；316, bar is limited；4, indicator light.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-5 is please referred to, the present invention provides a kind of technical solution: a kind of unmanned plane stop locking mechanism, including pedestal 1,
The two sides of pedestal 1 are provided through installation bolt 2, and the two sides at the top of pedestal 1 are fixedly connected with limited position mechanism 3, pedestal 1
Top and be located between two position-limit mechanisms 3 and be provided with indicator light 4, the controlling terminal of indicator light 4 and peripheral hardware is electrically connected.
Position-limit mechanism 3 includes limiting plate 307, and the top of limiting plate 307 is fixedly connected with limit shell 312, limit
The inner cavity of shell 312 is provided with the directing plate 301 being equipped with guiding device 310, and directing plate 301 is used to limit the shifting of supporting leg
Dynamic range, the top of limit shell 312 are provided through guiding device 310, and the two sides of limit 312 inner cavity of shell pass through spring
Hinge is connected with rotating block 302, and the bottom of rotating block 302 is flexibly connected restricted bar 316 by shaft, limits bar 316
Bottom end through limit shell 312 bottom and extend to limit shell 312 outside, the bottom of rotating block 302 passes through limitation
Spring 311 is fixedly connected with the bottom of limit 312 inner cavity of shell, and limited spring 311 is around the table for being set to limitation bar 316
Face, limited spring 311 and limitation bar 316 for carrying out buffer operation, avoid declining due to supporting leg it is too fast caused by device portion
Part damage, rotating block 302 are provided with proof rubber 303 far from the side of limit 312 inner wall of shell, proof rubber 303 for pair
Rotating block 302 is protected, and rotating block 302 is inlaid with permanent magnet 313 close to the side of limit 312 inner wall of shell, limits shell
The two sides of 312 intracavity bottoms are fixedly connected to the coil plate 314 being equipped with permanent magnet 313, and coil plate 314 produces after being powered
Raw magnetic direction is identical as the magnetic direction of permanent magnet 313, and the two sides of limit 312 bottom of shell are fixedly connected to metallic rod
309, the top of metallic rod 309 is fixedly connected with stressing device 315, and the bottom of stressing device 315 is fixedly connected with transmission device
304, the bottom of transmission device 304 is provided with driving mechanism 305, and the bottom end of metallic rod 309 is fixedly connected with metal plate 308, gold
The two sides for belonging to plate 308 are provided through rubber rods 306, the fixed company in bottom on the top and limit shell 312 of rubber rods 306
It connects, the bottom end of rubber rods 306 is fixedly connected with the top of pedestal 1, and rubber rods 306 are used to increase the stability of device, driving machine
Structure 305 and coil plate 314 are electrically connected with the controlling terminal of peripheral hardware.
Transmission device 304 includes transmission shell 3044, and the bottom at the top and stressing device 315 that are driven shell 3044 is fixed
Connection, the inner wall of transmission shell 3044 are provided with transmission teeth 3043, and the inner cavity of transmission shell 3044 is provided with central gear
3401, it is driven the inner cavity of shell 3044 and edge gear is connected with by shaft positioned at the two sides of central gear 3401
3042, edge gear 3042 is engaged with central gear 3401 and transmission teeth 3043 respectively, and the output end of driving mechanism 305 runs through
It is driven the bottom of shell 3044 and is fixedly connected with central gear 3401.
Guiding device 310 includes guiding shell 3101, and the surface of guiding shell 3101 is arranged with coil pipe 3102, and guiding is outer
The two sides of 3101 inner cavity of shell are provided with guide rail bolt 3103, and the surface of guide rail bolt 3103 is provided with guide rail crawler belt 3104, and
Guide rail crawler belt 3104 is parallel with the guiding inner wall of shell 3101, and the controlling terminal of coil pipe 3102 and peripheral hardware is electrically connected.
Stressing device 315 includes stress shell 3153, and the two sides of 3153 front surface of stress shell are provided with snap-gauge 3156,
Rubber sleeve 3155 is arranged far from the side of axis 3152 in snap-gauge 3156, and rubber sleeve 3155 is for protecting snap-gauge 3156, snap-gauge
Axis 3152 is provided through on 3156, the bottom end of axis 3152 sequentially passes through stress shell 3153 and the top for being driven shell 3044
Portion is simultaneously fixedly connected with edge gear 3042, the front surface of stress shell 3153 offer with unmanned plane supporting leg be equipped with by
Power slot 3154, the bottom of 3154 inner cavity of stress slot are provided with pressure sensor 3151, the control of pressure sensor 3151 and peripheral hardware
Terminal is electrically connected.
Corresponding position is secured the appliance to by installing bolt 2, when needing to carry out the docking operation of unmanned plane, passes through control
The power supply of terminal closing coil pipe 3102 adsorbs the supporting leg of unmanned plane, so that two so that coil pipe 3102 generates magnetic field force
The top of a supporting leg alignment guide device 310 is (if the supporting leg of unmanned plane cannot be needed to be arranged on supporting leg by magnetic field gravitational attraction
Becket), unmanned plane is declined so that supporting leg stretches to and then stops unmanned plane in guiding shell 3101 and work and cut off coil
The power supply of pipe 3102, to make unmanned plane fall under gravity, supporting leg is in track crawler 3104 and directing plate 301
It is fallen under effect in stress slot 3154 and triggers pressure sensor 3151, pressure sensor 3151 is toggled rear controlling terminal
It controls driving mechanism 305 to work, while under the effect of transmission device 304 snap-gauge 3156 is rotated and blocking the bottom of supporting leg,
The position of branch midleg is limited under the action of rotating block 302 simultaneously, controlling terminal control instructions lamp 4 lights, prompts to make with this
User's locking mechanism is completed.
When needs, which unlock, to be operated, by the power supply of controlling terminal closing coil plate 314, so that coil plate
314 generate the magnetic field to attract each other with permanent magnet 313, so that rotating block 302 rotates, release the locking to branch midleg with this,
Controlling terminal control driving mechanism 305 rotates backward, so that snap-gauge 31056 rotates backward, is released with this to supporting leg bottom
Locking, and control unmanned plane and fly up, when pressure sensor 3151 is no longer influenced by triggering, controlling terminal cuts off indicator light 4
Power supply prompts user to unlock and completes with this.
In conclusion the unmanned plane stops locking mechanism, pass through position-limit mechanism 3, transmission device 304,310 and of guiding device
The improvement of stressing device 315, so that unmanned plane stops locking mechanism and can be very good automatically to guide the unmanned plane that will land
It to corresponding position and conducts the locking operations, reduces the operation difficulty of user, be convenient to use while improving working efficiency
The use of person.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of unmanned plane stops locking mechanism, including pedestal (1), it is characterised in that: the two sides at the top of the pedestal (1) are equal
It is fixedly connected limited position mechanism (3), the top of the pedestal (1) and is provided with indicator light between two position-limit mechanisms (3)
(4), the controlling terminal of the indicator light (4) and peripheral hardware is electrically connected；
The position-limit mechanism (3) includes limiting plate (307), and it is outer that limit is fixedly connected at the top of the limiting plate (307)
Shell (312) is provided through guiding device (310) at the top of the limit shell (312), limit shell (312) inner cavity
Two sides pass through spring hinge and be connected with rotating block (302), the rotating block (302) is in limit shell (312)
The side of wall is inlaid with permanent magnet (313), and the two sides of described limit shell (312) intracavity bottom are fixedly connected to and permanent magnet
(313) two sides of the coil plate (314) being equipped with, described limit shell (312) bottom are fixedly connected to metallic rod
(309), the top of the metallic rod (309) is fixedly connected with stressing device (315), and the bottom of the stressing device (315) is solid
Surely it is connected with transmission device (304), the bottom of the transmission device (304) is provided with driving mechanism (305), the metallic rod
(309) bottom end is fixedly connected with metal plate (308), the driving mechanism (305) and coil plate (314) with the control of peripheral hardware
Terminal is electrically connected；
The transmission device (304) includes transmission shell (3044), the top of transmission shell (3044) and stressing device
(315) bottom is fixedly connected, and the inner wall of transmission shell (3044) is provided with transmission teeth (3043), the transmission shell
(3044) inner cavity is provided with central gear (3401), it is described transmission shell (3044) inner cavity and be located at central gear (3401)
Two sides be connected with edge gear (3042) by shaft, the edge gear (3042) respectively with central gear (3401)
With transmission teeth (3043) engagement, the output end of the driving mechanism (305) is through the bottom for being driven shell (3044) and in
Heart gear (3401) is fixedly connected；
The guiding device (310) includes guiding shell (3101), and the surface of guiding shell (3101) is arranged with coil pipe
(3102), the two sides of described guiding shell (3101) inner cavity are provided with guide rail bolt (3103), the guide rail bolt (3103)
Surface be provided with guide rail crawler belt (3104), and guide rail crawler belt (3104) with guiding the inner wall of shell (3101) it is parallel, the line
The controlling terminal of circle pipe (3102) and peripheral hardware is electrically connected；
The stressing device (315) includes stress shell (3153), and the two sides of stress shell (3153) front surface are respectively provided with
Have snap-gauge (3156), be provided through axis (3152) on the snap-gauge (3156), the bottom end of the axis (3152) is successively passed through
It wears stress shell (3153) and is driven the top of shell (3044) and is fixedly connected with edge gear (3042), the stress shell
(3153) front surface offers the stress slot (3154) being equipped with unmanned plane supporting leg, stress slot (3154) inner cavity
Bottom is provided with pressure sensor (3151), and the controlling terminal of the pressure sensor (3151) and peripheral hardware is electrically connected.
2. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the two sides of the pedestal (1)
It is provided through installation bolt (2).
3. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the coil plate (314) is logical
The magnetic direction generated after electricity is identical as the magnetic direction of permanent magnet (313).
4. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the rotating block (302) is remote
Side from limit shell (312) inner wall is provided with proof rubber (303).
5. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the rotating block (302)
Bottom is flexibly connected restricted bar (316) by shaft, and the bottom end of limitation bar (316) is through the bottom of limit shell (312)
The bottom of portion and the outside for extending to limit shell (312), the rotating block (302) is outer by limited spring (311) and limit
The bottom of shell (312) inner cavity is fixedly connected, and limited spring (311) is around the surface for being set to limitation bar (316).
6. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the limit shell (312)
Inner cavity be provided with the directing plate (301) being equipped with guiding device (310).
7. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the metal plate (308)
Two sides are provided through rubber rods (306), the fixed company in the top of the rubber rods (306) and the bottom of limit shell (312)
It connects, is fixedly connected at the top of the bottom end and pedestal (1) of the rubber rods (306).
8. a kind of unmanned plane according to claim 1 stops locking mechanism, it is characterised in that: the snap-gauge (3156) is separate
Rubber sleeve (3155) are arranged in the side of axis (3152).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811485910.8A CN109533375A (en) | 2018-12-06 | 2018-12-06 | A kind of unmanned plane stop locking mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811485910.8A CN109533375A (en) | 2018-12-06 | 2018-12-06 | A kind of unmanned plane stop locking mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109533375A true CN109533375A (en) | 2019-03-29 |
Family
ID=65853093
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811485910.8A Withdrawn CN109533375A (en) | 2018-12-06 | 2018-12-06 | A kind of unmanned plane stop locking mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109533375A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808911A (en) * | 2019-04-01 | 2019-05-28 | 西北工业大学 | The portable sliding race unmanned aerial vehicle of one kind lodges automatically takes turns retaining device |
| FR3106575A1 (en) | 2020-01-27 | 2021-07-30 | Take Air | Device for holding a drone. |
| WO2021255053A1 (en) | 2020-06-19 | 2021-12-23 | Take-Air | Device for mounting a drone |
| CN114348276A (en) * | 2022-01-19 | 2022-04-15 | 河北福莱卡航空科技有限公司 | Ducted fan unmanned aerial vehicle starting drive from taking off hook-shaped formula |
-
2018
- 2018-12-06 CN CN201811485910.8A patent/CN109533375A/en not_active Withdrawn
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808911A (en) * | 2019-04-01 | 2019-05-28 | 西北工业大学 | The portable sliding race unmanned aerial vehicle of one kind lodges automatically takes turns retaining device |
| FR3106575A1 (en) | 2020-01-27 | 2021-07-30 | Take Air | Device for holding a drone. |
| WO2021255053A1 (en) | 2020-06-19 | 2021-12-23 | Take-Air | Device for mounting a drone |
| FR3111622A1 (en) | 2020-06-19 | 2021-12-24 | Take-Air | Rigging device for a drone. |
| CN114348276A (en) * | 2022-01-19 | 2022-04-15 | 河北福莱卡航空科技有限公司 | Ducted fan unmanned aerial vehicle starting drive from taking off hook-shaped formula |
| CN114348276B (en) * | 2022-01-19 | 2024-01-23 | 河北福莱卡航空科技有限公司 | Self-unhooking type ducted fan unmanned aerial vehicle starting device |
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| PB01 | Publication | ||
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Application publication date: 20190329 |