CN209814317U - Positioning type take-off and landing platform for mooring unmanned aerial vehicle - Google Patents
Positioning type take-off and landing platform for mooring unmanned aerial vehicle Download PDFInfo
- Publication number
- CN209814317U CN209814317U CN201920404148.XU CN201920404148U CN209814317U CN 209814317 U CN209814317 U CN 209814317U CN 201920404148 U CN201920404148 U CN 201920404148U CN 209814317 U CN209814317 U CN 209814317U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- platform
- pressing
- pulling
- 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.)
- Expired - Fee Related
Links
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a locate mode platform that takes off and land for mooring unmanned aerial vehicle, including unmanned aerial vehicle platform that takes off and land, unmanned aerial vehicle takes off and land and is equipped with the undercarriage flexible casting die all around that is located unmanned aerial vehicle on the bench, when unmanned aerial vehicle lands on unmanned aerial vehicle platform that takes off and land, each flexible casting die shrink and the casting die undercarriage of drawing and pressing fix a position. The lifting platform has the advantages of simple and reliable structure, strong adaptability, automatic fixation and loss prevention.
Description
Technical Field
The utility model mainly relates to the field of unmanned aerial vehicles, especially, relate to a locate mode platform that takes off and land for mooring unmanned aerial vehicle.
Background
With the deepening of informatization and networking degrees, the convenience brought by the network can be enjoyed in all aspects of life. At the same time, network dependence becomes a feature of this information society. The popularity of thumb culture makes the communication demand continuously rise, the communication guarantee capability shows a crucial role, and the necessity demand of emergency communication such as field operation, emergency rescue and the like is more prominent. Under the demand situation, the tethered rotor unmanned aerial vehicle as a high-altitude base station walks into eye curtains of people. Mooring unmanned aerial vehicle system is by many rotor unmanned aerial vehicle, mooring cable, ground take-off and landing platform are constituteed, unmanned aerial vehicle uses the long-time stagnation of ground power supply to hang and stop, simultaneously, data such as the high definition video of airborne equipment collection can be passed back to ground through the built-in optic fibre of mooring cable, have aerial long-time operation, the big advantage of data transmission bandwidth, but entire system stand alone type installation also can on-vehicle installation to can the vehicle movement is followed in automatic synchronization. At present, a tethered unmanned aerial vehicle on the market can supply power through a ground generator, 24-hour all-weather stagnation can be realized, the tethered unmanned aerial vehicle works continuously for 72 hours, and hovers at a fixed point of 200 meters, so that the tethered unmanned aerial vehicle is widely applied to a plurality of wide fields of disaster relief and rescue, border patrol, base safety, scenic spot monitoring, geological survey, field operation, forest fire prevention, emergency communication, public security anti-terrorism, traffic supervision, news interview, engineering monitoring, environment monitoring, movie and television shooting, scientific research, national defense war industry and the like.
On-vehicle mooring unmanned aerial vehicle can meet various road conditions in the vehicle is marchd, and rugged and uneven road surface can lead to the fact the influence to mooring unmanned aerial vehicle, produces the damage even, and unmanned aerial vehicle easily produces in the car or the roof and emptys the upset. Because mooring unmanned aerial vehicle take-off and landing platform is located the roof more or spreads over the car of equipment, the manual fixed of personnel of not being convenient for, consequently need an automatic fixed scheme of on-vehicle mooring unmanned aerial vehicle urgently.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome the not enough of prior art, provide a simple structure reliable, the suitability strong, can realize automatic fixed, can the loss prevention locate mode platform that takes off and land.
In order to solve the technical problem, the utility model discloses a following technical scheme:
the utility model provides a locate mode platform that takes off and land for mooring unmanned aerial vehicle, includes unmanned aerial vehicle platform that takes off and land, unmanned aerial vehicle takes off and land and is equipped with the undercarriage that is located unmanned aerial vehicle flexible all around and draws the casting die on the platform, when unmanned aerial vehicle lands on unmanned aerial vehicle platform that takes off and land, respectively stretch out and draw the casting die to contract and draw and compress the undercarriage and fix a position.
As a further improvement of the above technical solution:
the telescopic tension and compression piece comprises a tension and compression servo motor and a tension and compression rod, the tension and compression servo motor is fixed on an unmanned aerial vehicle lifting platform, the tension and compression rod is connected with the output end of the tension and compression servo motor, and the tension and compression rod contracts under the drive of the tension and compression servo motor to tension and compress an undercarriage.
And the tension and compression rod is provided with a tension and compression buffer block.
And a pulling and pressing groove is formed in the pulling and pressing side of the pulling and pressing buffer block.
The unmanned aerial vehicle takes off and land and is equipped with the undercarriage that is located unmanned aerial vehicle on the platform and bulldozes the piece all around, when unmanned aerial vehicle lands on the unmanned aerial vehicle takes off and land the bench, each is flexible bulldozes the piece and stretches out and bulldozes the undercarriage location.
The telescopic pushing and pressing piece comprises an installation platform, a telescopic servo motor and a pushing and pressing rod, the installation platform is fixedly arranged on an unmanned aerial vehicle lifting platform, the telescopic servo motor is fixed on the installation platform, the pushing and pressing rod is connected with the output end of the telescopic servo motor, and the pushing and pressing rod extends out under the driving of the telescopic servo motor to support and press the undercarriage.
And one end of the pushing rod, which is close to the undercarriage, is provided with a telescopic buffer block.
The telescopic buffer block is provided with a pushing groove at the pushing side.
Compared with the prior art, the utility model has the advantages of:
the utility model discloses a locate mode platform that takes off and land for mooring unmanned aerial vehicle, including unmanned aerial vehicle platform that takes off and land, be equipped with the undercarriage flexible all around that is located unmanned aerial vehicle on the unmanned aerial vehicle platform that takes off and land and draw the casting die, when unmanned aerial vehicle lands on unmanned aerial vehicle platform that takes off and land, respectively stretch out and draw the casting die to contract and draw the casting die to fix a position. In this structure, the installation is located unmanned aerial vehicle's undercarriage flexible casting die all around at unmanned aerial vehicle take off and land the bench, and the extension is stretched out before unmanned aerial vehicle descends, and after unmanned aerial vehicle fell, the flexible casting die shrink was to the undercarriage bottom form all around the location of flat casting down formula. This platform overall structure that takes off and land of locate mode is simple reliable for on-vehicle mooring unmanned aerial vehicle can realize that the automation after falling is fixed, need not manual operation, can adapt to roof or narrow and small car space restriction, makes mooring vehicle can not damage its unmanned aerial vehicle who loads under various road conditions, has improved on-vehicle mooring unmanned aerial vehicle's suitability greatly.
Drawings
Fig. 1 is the utility model discloses a main structure schematic diagram of looking at for mooring unmanned aerial vehicle's locate mode take-off and landing platform.
Fig. 2 is a side view schematic structure for mooring unmanned aerial vehicle's locate mode take-off and landing platform.
Fig. 3 is a schematic view of the positioning type landing platform for mooring the unmanned aerial vehicle.
Fig. 4 is the utility model discloses a spatial structure schematic diagram of a locate mode platform that takes off and land for mooring unmanned aerial vehicle.
The reference numerals in the figures denote:
1. an unmanned aerial vehicle landing platform; 2. an unmanned aerial vehicle; 21. a landing gear; 3. a telescopic pulling and pressing piece; 31. a servo motor is pulled and pressed; 32. pulling and pressing the rod; 321. pulling and pressing the buffer block; 3211. drawing and pressing the groove; 4. a telescoping pusher; 41. an installation table; 42. a telescopic servo motor; 43. a push rod; 431. a telescopic buffer block; 4311. and pushing the groove.
Detailed Description
The invention will be described in further detail with reference to the drawings and specific examples.
Fig. 1 to 4 show the utility model discloses an embodiment of a locate mode take-off and landing platform for mooring unmanned aerial vehicle, including unmanned aerial vehicle take-off and landing platform 1, be equipped with the undercarriage 21 that is located unmanned aerial vehicle 2 on the unmanned aerial vehicle take-off and landing platform 1 flexible all around and draw casting die 3, when unmanned aerial vehicle 2 descends on unmanned aerial vehicle take-off and landing platform 1, each is flexible draws casting die 3 to shrink and draws casting die 21 to fix a position. In this structure, the installation is located unmanned aerial vehicle 2's undercarriage 21 flexible casting die 3 all around on unmanned aerial vehicle take off and land platform 1, and the extension casting die 3 stretches out before unmanned aerial vehicle 2 lands, and after unmanned aerial vehicle 2 landed, the flexible casting die 3 shrink formed the location of flat drawing down type all around to undercarriage 21 bottom. This platform overall structure that takes off and land of locate mode is simple reliable for on-vehicle mooring unmanned aerial vehicle 2 can realize that the automation after falling is fixed, need not manual operation, can adapt to roof or narrow and small car space restriction, makes mooring vehicle can not damage its unmanned aerial vehicle 2 who loads under various road conditions, has improved on-vehicle mooring unmanned aerial vehicle 2's suitability greatly.
In this embodiment, the telescopic pulling and pressing member 3 includes a pulling and pressing servo motor 31 and a pulling and pressing rod 32, the pulling and pressing servo motor 31 is fixed on the unmanned aerial vehicle landing platform 1, the pulling and pressing rod 32 is connected with an output end of the pulling and pressing servo motor 31, and the pulling and pressing rod 32 contracts under the driving of the pulling and pressing servo motor 31 to tighten and press the undercarriage 21. In this structure, draw and press servo motor 31 to fix on unmanned aerial vehicle platform 1 that takes off and land, be located the bottom, draw and press servo motor 31 drive to draw depression bar 32 to the landing gear 21 lower floor realize the location of the pressure formula of flat drawing down.
In this embodiment, the tension/compression rod 32 is provided with a tension/compression buffer block 321. The tension and compression buffer block 321 is made of soft material, such as plastic, to prevent the tension and compression rod 32 from directly pushing and pressing the landing gear 21, so as to effectively protect the landing gear 21.
In this embodiment, a pulling and pressing groove 3211 is formed on the pulling and pressing side of the pulling and pressing buffer block 321. The horizontal thrust and the downward pressure on the undercarriage 21 can be ensured by pulling and pressing the slot 3211, so that the horizontal and vertical freedom of the undercarriage 21 is limited.
In this embodiment, be equipped with the undercarriage 21 that is located unmanned aerial vehicle 2 on the unmanned aerial vehicle platform of taking off and land and stretch out and bulldoze piece 4 all around on 1, when 2 lands on unmanned aerial vehicle platform of taking off and land 1, each stretch out and draw back and bulldoze undercarriage 21 location. Realize the location of a flat push-down formula through flexible bulldozing piece 4 all around to undercarriage 21 upper strata, realized the spacing of upper strata level and vertical direction promptly, prevent it and empty to reach on-vehicle automatic fixed effect of mooring unmanned aerial vehicle 2.
In this embodiment, the telescopic pushing component 4 includes an installation platform 41, a telescopic servo motor 42 and a pushing rod 43, the installation platform 41 is fixedly installed on the unmanned aerial vehicle landing platform 1, the telescopic servo motor 42 is fixed on the installation platform 41, the pushing rod 43 is connected with an output end of the telescopic servo motor 42, and the pushing rod 43 extends out under the driving of the telescopic servo motor 42 to push down the undercarriage 21. In this structure, the mounting table 41 is used for mounting the servo motor 42 and ensuring that the servo motor 42 has a certain height, and the servo motor 42 drives the push rod 43 to realize the flat push and push-down type positioning on the upper layer of the landing gear 41.
In this embodiment, the push rod 43 is provided with a telescopic bumper 431 at an end thereof close to the undercarriage 21. The bumper 431 is made of a soft material, such as plastic, so as to prevent the thrust rod 43 from directly pushing the landing gear 21 rigidly, thereby effectively protecting the landing gear 21.
In this embodiment, the telescopic buffer block 431 is provided with a push groove 4311 on the push side. The horizontal thrust and downward pressure on the undercarriage 21 can be ensured by the push groove 4311, thereby limiting the degree of freedom in the vertical direction of the undercarriage 21.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to limit the present invention. The technical solution of the present invention can be used by anyone skilled in the art to make many possible variations and modifications, or to modify equivalent embodiments, without departing from the scope of the technical solution of the present invention, using the technical content disclosed above. Therefore, any simple modification, equivalent change and modification made to the above embodiments by the technical entity of the present invention should fall within the protection scope of the technical solution of the present invention.
Claims (8)
1. The utility model provides a locate mode platform that takes off and land for mooring unmanned aerial vehicle, includes unmanned aerial vehicle platform (1) that takes off and land, its characterized in that: be equipped with on unmanned aerial vehicle take off and land platform (1) and be located undercarriage (21) of unmanned aerial vehicle (2) flexible casting die (3) all around, when unmanned aerial vehicle (2) descend on unmanned aerial vehicle take off and land platform (1), each is flexible casting die (3) to shrink and draw and press undercarriage (21) to fix a position.
2. The positionable take-off and landing platform for mooring a drone of claim 1, wherein: the telescopic pulling and pressing piece (3) comprises a pulling and pressing servo motor (31) and a pulling and pressing rod (32), the pulling and pressing servo motor (31) is fixed on the unmanned aerial vehicle lifting platform (1), the pulling and pressing rod (32) is connected with the output end of the pulling and pressing servo motor (31), and the pulling and pressing rod (32) contracts under the driving of the pulling and pressing servo motor (31) to pull and press the undercarriage (21).
3. The positionable take-off and landing platform for mooring a drone of claim 2, wherein: the tension and compression rod (32) is provided with a tension and compression buffer block (321).
4. The positionable take-off and landing platform for mooring a drone of claim 3, wherein: a pulling and pressing groove (3211) is formed in the pulling and pressing side of the pulling and pressing buffer block (321).
5. The positionable landing platform for mooring a drone of any one of claims 1 to 4, wherein: be equipped with on unmanned aerial vehicle take off and land platform (1) and be located undercarriage (21) of unmanned aerial vehicle (2) flexible bulldozing piece (4) all around, when unmanned aerial vehicle (2) descend on unmanned aerial vehicle take off and land platform (1), each flexible bulldozing piece (4) stretches out and bulldozes undercarriage (21) location.
6. The positionable take-off and landing platform for mooring a drone of claim 5, wherein: the telescopic pushing and pressing piece (4) comprises an installation platform (41), a telescopic servo motor (42) and a pushing and pressing rod (43), the installation platform (41) is fixedly installed on the unmanned aerial vehicle lifting platform (1), the telescopic servo motor (42) is fixed on the installation platform (41), the pushing and pressing rod (43) is connected with the output end of the telescopic servo motor (42), and the pushing and pressing rod (43) stretches out under the driving of the telescopic servo motor (42) to abut against and press the undercarriage (21).
7. The positionable take-off and landing platform for mooring a drone of claim 6, wherein: one end of the push rod (43) close to the landing gear (21) is provided with a telescopic buffer block (431).
8. The positionable take-off and landing platform for mooring a drone of claim 7, wherein: the telescopic buffer block (431) is provided with a pushing groove (4311) at the pushing side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920404148.XU CN209814317U (en) | 2019-03-27 | 2019-03-27 | Positioning type take-off and landing platform for mooring unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920404148.XU CN209814317U (en) | 2019-03-27 | 2019-03-27 | Positioning type take-off and landing platform for mooring unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209814317U true CN209814317U (en) | 2019-12-20 |
Family
ID=68877489
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920404148.XU Expired - Fee Related CN209814317U (en) | 2019-03-27 | 2019-03-27 | Positioning type take-off and landing platform for mooring unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209814317U (en) |
-
2019
- 2019-03-27 CN CN201920404148.XU patent/CN209814317U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209814316U (en) | Positioning type take-off and landing platform suitable for mooring unmanned aerial vehicle | |
| CN209814323U (en) | Be applied to unmanned aerial vehicle's of mooring platform that takes off and land | |
| CN102381234A (en) | Electric power emergency air-ground patrol vehicle | |
| CN209814317U (en) | Positioning type take-off and landing platform for mooring unmanned aerial vehicle | |
| CN104443413A (en) | Unmanned aerial vehicle withdrawing equipment | |
| CN202180773U (en) | Ground-aerial cruiser for power emergency | |
| CN210214608U (en) | Unmanned aerial vehicle supervision platform | |
| CN209814321U (en) | Positioning type take-off and landing platform for mooring unmanned aerial vehicle | |
| CN209815413U (en) | A self-adaptation is received and is released line device for mooring unmanned aerial vehicle | |
| CN208867919U (en) | A kind of emergency rescue vehicle | |
| CN209814322U (en) | Take-off and landing platform suitable for mooring unmanned aerial vehicle | |
| CN109775482A (en) | For being tethered at the adaptive take-up and pay-off device of unmanned plane | |
| CN210364423U (en) | Improved generation unmanned aerial vehicle cloud platform | |
| CN202534980U (en) | Imaging apparatus used for electric line patrol unmanned helicopter | |
| CN209814324U (en) | Be applied to unmanned aerial vehicle's of mooring platform that takes off and land | |
| CN212530099U (en) | Unmanned aerial vehicle shoots and uses camera protector | |
| CN205525014U (en) | Pulling equipment, recovery unit and parachuting recovery system | |
| CN209993276U (en) | Can turn to LED screen that removes | |
| CN210592477U (en) | A platform that takes off and land charges for mooring unmanned aerial vehicle | |
| CN207208490U (en) | One kind blocks formula fixed-wing unmanned plane retracting device | |
| CN205554555U (en) | It is alert with multi -functional superficial empty optimal in structure | |
| CN216424764U (en) | Aircraft mounting carrier connecting mechanism | |
| CN214356692U (en) | Unmanned aerial vehicle for geotechnical engineering investigation | |
| CN213502902U (en) | Unmanned aerial vehicle who possesses face identification function | |
| CN218022178U (en) | Intelligent forest fire monitoring equipment |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191220 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |