CN210852979U - Unmanned aerial vehicle parking support for surveying and mapping - Google Patents
Unmanned aerial vehicle parking support for surveying and mapping Download PDFInfo
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- CN210852979U CN210852979U CN201921959658.XU CN201921959658U CN210852979U CN 210852979 U CN210852979 U CN 210852979U CN 201921959658 U CN201921959658 U CN 201921959658U CN 210852979 U CN210852979 U CN 210852979U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle technique and specifically relates to an unmanned aerial vehicle parking support for surveying and mapping, which comprises a plate body, limiting plates are welded on two sides of the bottom of the plate body, a first sliding rod is welded on the inner side of each limiting plate, a first sliding sleeve is connected on two sides of the surface of the first sliding rod in a sliding manner, and a first buffer mechanism is hinged to the bottom of the first sliding sleeve; the utility model discloses a plate body, the limiting plate, first slide bar, first sliding sleeve, first spring, the slider, first branch, the setting of briquetting and second spring, the effectual and stable good purpose of shock attenuation has been reached, it is poor to have solved current unmanned aerial vehicle and parked the support shock attenuation effect when using, unmanned aerial vehicle receives the striking and destroys easily when descending like this, and current unmanned aerial vehicle parks the support poor stability when falling to the ground, lead to the phenomenon that unmanned aerial vehicle appears rolling like this easily, lead to the problem of unmanned aerial vehicle screw damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle parking support for survey and drawing.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, compared with the unmanned aerial vehicle, the unmanned aerial vehicle is more suitable for tasks too easy, dirty or dangerous, and can be divided into military use and civil use according to the application field, the unmanned aerial vehicle is divided into a reconnaissance plane and a target plane, and the civil use, unmanned aerial vehicle and industrial use are really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, the developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology, and the parking support is an important part of the unmanned aerial vehicle.
Present unmanned aerial vehicle parks support shock attenuation effect when using is poor, and unmanned aerial vehicle receives the striking easily and destroys when descending like this, and current unmanned aerial vehicle parks support poor stability when falling to the ground, leads to unmanned aerial vehicle to appear the phenomenon of rolling like this easily, leads to unmanned aerial vehicle's screw to destroy, for this reason, provides an unmanned aerial vehicle for survey and drawing and parks the support.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle parking support for survey and drawing possesses the effectual advantage with stable good of shock attenuation, and it is poor to have solved current unmanned aerial vehicle parking support shock attenuation effect when using, and unmanned aerial vehicle receives the striking and destroys easily when descending like this, and current unmanned aerial vehicle parking support poor stability when falling to the ground, leads to the phenomenon that unmanned aerial vehicle appears rolling like this easily, leads to the problem of unmanned aerial vehicle screw damage.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle parking support for surveying and mapping comprises a plate body, wherein limiting plates are welded on two sides of the bottom of the plate body, a first sliding rod is welded at the inner side of the limiting plate, a first sliding sleeve is connected with both sides of the surface of the first sliding rod in a sliding manner, the bottom of the first sliding sleeve is hinged with a first buffer mechanism, the first buffer mechanism comprises a first shell, a first spring, a sliding block and a first supporting rod, the bottom of the first buffer mechanism is hinged with a bottom plate, the inner side of the top of the bottom plate is fixedly provided with a second buffer mechanism, the second buffer mechanism comprises a second sliding rod, a block body, a second sliding sleeve, a supporting rod, a pressing block, a second spring and a second shell, the bottom of plate body and the outside welding that is located the limiting plate have the body of rod, the bottom of the body of rod articulates there is third buffer gear, third buffer gear includes third sliding sleeve, third slide bar, handle and third spring.
Preferably, the bottom of the first shell is hinged to the center of the top of the bottom plate, the bottom of the inner cavity of the first shell is welded to the bottom of the first spring, the top of the first spring is welded to the bottom of the sliding block, the side face of the sliding block is connected with the inner wall of the first shell in a sliding mode through the sliding groove, the top of the sliding block is welded to the bottom of the first supporting rod, and the top of the first supporting rod is hinged to the bottom of the first sliding sleeve.
Preferably, the both sides of second slide bar and the inboard welding of block, the bottom of block and the right side welding at bottom plate top, the surface of second slide bar and the inner wall sliding connection of second sliding sleeve, the top of second sliding sleeve is articulated with the bottom of branch, branch runs through the second casing and extends to the inner chamber of second casing and the bottom sliding connection of briquetting, the top of briquetting and the bottom welding of second spring, the top of second spring and the top welding of second casing inner chamber, the top of second casing is articulated with the inboard middle part of first casing.
Preferably, the inner wall of the third sliding sleeve is connected with the surface of a third sliding rod in a sliding mode, the inner end of the third sliding rod is hinged to the middle of the outer side of the first shell, and the center of the top of the third sliding sleeve is hinged to the bottom of the rod body.
Preferably, one side of the third sliding rod, which is far away from the first shell, is welded with a handle, and the surface of the third sliding rod and two sides of the third sliding sleeve are both sleeved with third springs.
Preferably, the number of the limiting plates is four, and the limiting plates are arranged at four corners of the bottom of the plate body in a rectangular shape.
Preferably, the number of the rod bodies is four, and the rod bodies are arranged at four corners of the bottom of the plate body in a rectangular shape.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a plate body, the limiting plate, first slide bar, first sliding sleeve, first spring, the slider, first branch, the setting of briquetting and second spring, the effectual and stable good purpose of shock attenuation has been reached, it is poor to have solved current unmanned aerial vehicle and parked the support shock attenuation effect when using, unmanned aerial vehicle receives the striking and destroys easily when descending like this, and current unmanned aerial vehicle parks the support poor stability when falling to the ground, lead to the phenomenon that unmanned aerial vehicle appears rolling like this easily, lead to the problem of unmanned aerial vehicle screw damage.
2. The utility model discloses a through setting up first buffer gear, the impact force that produces drives the limiting plate through the plate body and moves, the limiting plate drives first slide bar and moves, first slide bar drives first sliding sleeve and moves, first sliding sleeve drives the branch and moves, simultaneously the branch also drives the slip of first sliding sleeve at the surface of first slide bar, the branch drives the slider and slides in first casing, the slider slides and drives the first spring to take place the deformation, through the deformation of first spring, cushion the impact force, reduce the impact force that unmanned aerial vehicle received because of vibrations, through setting up the second buffer gear, when the bottom plate receives the collision, the bottom plate drives the second slide bar through the block body and moves, the second slide bar drives the second sliding sleeve and slides at the surface of second slide bar, the second sliding sleeve drives the second branch and moves, the second branch drives the briquetting and extrudes the second spring, make the second spring take place to shrink, the second spring can produce the reaction force after the shrink and drive the second spring and extend, drives the part and resets to reach and cushion the impact force that the collision produced, improved the stability of plate body.
3. The utility model discloses a set up the third sliding sleeve, the bottom plate drives the body of rod and removes, the body of rod drives the third sliding sleeve and removes, the third sliding sleeve extrudees the third slide bar, it slides in the third sliding sleeve to drive the third slide bar simultaneously, thereby reach and change the direction of impact force, change the direction about by upper and lower direction, through setting up the third spring, extrude the third spring when the third slide bar is gliding, deformation through the third spring, cushion impact force, the impact force that unmanned aerial vehicle received because of vibrations has been reduced, all be provided with the limiting plate through the four corners in plate body bottom, the equilibrium and the stability of plate body have been improved, all be provided with the body of rod through the four corners in plate body bottom, the equilibrium and the stability of plate body have further been improved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic sectional view of a second buffer mechanism of the present invention;
fig. 3 is a schematic cross-sectional structural view of the first buffer mechanism of the present invention;
fig. 4 is an enlarged schematic view of the area a in fig. 1 according to the present invention.
In the figure: 1. a plate body; 2. a limiting plate; 3. a first slide bar; 4. a first sliding sleeve; 5. a first buffer mechanism; 51. a first housing; 52. a first spring; 53. a slider; 54. a first support bar; 6. a base plate; 7. a second buffer mechanism; 71. a second slide bar; 72. a block body; 73. a second sliding sleeve; 74. a second support bar; 75. briquetting; 76. a second spring; 77. a second housing; 8. a rod body; 9. a third buffer mechanism; 91. a third sliding sleeve; 92. a third slide bar; 93. a handle; 94. and a third spring.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, an unmanned aerial vehicle parking stand for surveying and mapping comprises a plate body 1, limiting plates 2 are welded on two sides of the bottom of the plate body 1, first slide bars 3 are welded on the inner sides of the limiting plates 2, first slide sleeves 4 are slidably connected on two sides of the surfaces of the first slide bars 3, first buffer mechanisms 5 are hinged on the bottoms of the first slide sleeves 4, each first buffer mechanism 5 comprises a first shell 51, a first spring 52, a slide block 53 and a first support rod 54, a bottom plate 6 is hinged on the bottom of each first buffer mechanism 5, a second buffer mechanism 7 is fixedly installed on the inner side of the top of the bottom plate 6, each second buffer mechanism 7 comprises a second slide bar 71, a block body 72, a second slide sleeve 73, a support rod 74, a pressing block 75, a second spring 76 and a second shell 77, a rod body 8 is welded on the bottom of the plate body 1 and located on the outer side of the limiting plate 2, third buffer gear 9 includes third sliding sleeve 91, third slide bar 92, handle 93 and third spring 94, through plate body 1, limiting plate 2, first slide bar 3, first sliding sleeve 4, first spring 52, slider 53, first branch 54, branch 74, briquetting 75 and the setting of second spring 76, the effectual and stable good purpose of shock attenuation has been reached, it is poor to have solved current unmanned aerial vehicle parking support shock attenuation effect when using, unmanned aerial vehicle receives the striking and destroys easily when descending like this, and current unmanned aerial vehicle parking support poor stability when falling to the ground, lead to the phenomenon that unmanned aerial vehicle appears rolling like this easily, lead to the problem of unmanned aerial vehicle screw damage.
In this embodiment, specifically, the bottom of the first housing 51 is hinged to the center of the top of the bottom plate 6, the bottom of the inner cavity of the first housing 51 is welded to the bottom of the first spring 52, the top of the first spring 52 is welded to the bottom of the slider 53, the side of the slider 53 is slidably connected to the inner wall of the first housing 51 through the sliding slot, the top of the slider 53 is welded to the bottom of the first support rod 54, the top of the first support rod 54 is hinged to the bottom of the first sliding sleeve 4, by providing the first buffer mechanism 5, the generated impact force drives the limiting plate 2 to move through the plate body 1, the limiting plate 2 drives the first sliding rod 3 to move, the first sliding sleeve 3 drives the first sliding sleeve 4 to move, the first sliding sleeve 4 drives the first support rod 54 to move, meanwhile, the first support rod 54 also drives the first sliding sleeve 4 to slide on the surface of the first sliding sleeve 3, the first support rod 54 drives the slider 53 to slide, slider 53 drives first spring 52 and takes place deformation when gliding, through the deformation of first spring 52, cushions the impact force, has reduced unmanned aerial vehicle because of the impact force that vibrations received.
In this embodiment, specifically, two sides of the second sliding rod 71 are welded to the inner side of the block 72, the bottom of the block 72 is welded to the right side of the top of the bottom plate 6, the surface of the second sliding rod 71 is slidably connected to the inner wall of the second sliding sleeve 73, the top of the second sliding sleeve 73 is hinged to the bottom of the second support rod 74, the second support rod 74 penetrates through the second housing 77 and extends to the inner cavity of the second housing 77 to be slidably connected to the bottom of the pressing block 75, the top of the pressing block 75 is welded to the bottom of the second spring 76, the top of the second spring 76 is welded to the top of the inner cavity of the second housing 77, the top of the second housing 77 is hinged to the middle of the inner side of the first housing 51, by providing the second buffer mechanism 7, when the bottom plate 6 is collided, the bottom plate 6 drives the second sliding rod 71 to move through the block 72, the second sliding rod 71 drives the second sliding sleeve 73 to slide on the surface of the second sliding, the second support rod 74 drives the pressing block 75 to extrude the second spring 76, so that the second spring 76 contracts, the second spring 76 generates a reaction force after contraction to drive the second spring 76 to extend, and parts are driven to reset, so that impact force generated by collision is buffered, and the stability of the plate body 1 is improved.
In this embodiment, specifically, the inner wall of the third sliding sleeve 91 is connected with the surface of the third sliding rod 92 in a sliding manner, the inner end of the third sliding rod 92 is hinged to the middle of the outer side of the first casing 51, the center of the top of the third sliding sleeve 91 is hinged to the bottom of the rod body 8, the bottom plate 6 drives the rod body 8 to move, the rod body 8 drives the third sliding sleeve 91 to move, the third sliding sleeve 91 extrudes the third sliding rod 92, and meanwhile, the third sliding rod 92 is driven to slide in the third sliding sleeve 91, so that the direction of the impact force is changed, and the direction is changed from the up-down direction to the left-.
In this embodiment, it is specific, the welding of the third slide bar 92 is kept away from one side of first casing 51 has handle 93, and the surface of third slide bar 92 and the both sides that are located third sliding sleeve 91 all overlap and are equipped with third spring 94, through setting up third spring 94, extrudees third spring 94 when third slide bar 92 is gliding, through the deformation of third spring 94, cushions the impact force, has reduced unmanned aerial vehicle because of the impact force that vibrations received.
In this embodiment, it is concrete, and the quantity of limiting plate 2 is four, and limiting plate 2 is the four corners of rectangle range setting in plate body 1 bottom, all is provided with limiting plate 2 through the four corners in plate body 1 bottom, has improved plate body 1's equilibrium and stability.
In this embodiment, specifically, the quantity of the body of rod 8 is four, and the body of rod 8 is the four corners of rectangle range setting in plate body 1 bottom, all is provided with the body of rod 8 through the four corners in plate body 1 bottom, has further improved plate body 1's equilibrium and stability.
The working principle is as follows: when the unmanned aerial vehicle is impacted after landing, the generated impact force drives the limiting plate 2 to move through the plate body 1, the limiting plate 2 drives the first sliding rod 3 to move, the first sliding rod 3 drives the first sliding sleeve 4 to move, the first sliding sleeve 4 drives the first supporting rod 54 to move, meanwhile, the first supporting rod 54 also drives the first sliding sleeve 4 to slide on the surface of the first sliding rod 3, the first supporting rod 54 drives the sliding block 53 to slide in the first shell 51, the sliding block 53 drives the first spring 52 to deform while sliding, through the deformation of the first spring 52, the impact force is buffered, the impact force received by the unmanned aerial vehicle due to vibration is reduced, meanwhile, the bottom plate 6 drives the rod body 8 to move, the rod body 8 drives the third sliding sleeve 91 to move, the third sliding sleeve 91 extrudes the third sliding rod 92, simultaneously drives the third sliding rod 92 to slide in the third sliding sleeve 91, the third spring 94 is extruded while the third sliding rod 92 slides, deformation through third spring 94, cushion impact force, the impact force that unmanned aerial vehicle received because of vibrations has been reduced, bottom plate 6 receives when colliding, bottom plate 6 drives second slide bar 71 through block 72 and removes, second slide bar 71 drives second sliding sleeve 73 and slides at the surface of second slide bar 71, second sliding sleeve 73 drives second branch 74 and removes, second branch 74 drives briquetting 75 and extrudees second spring 76, make second spring 76 take place the shrink, second spring 76 can produce reaction force after the shrink and drive second spring 76 and extend, it resets to drive the part, thereby reach the impact force that produces the collision and cushion, the stability of plate body 1 has been improved.
The standard parts used in the present application document can be purchased from the market, and can be customized according to the description of the specification and the accompanying drawings, the specific connection mode of each part adopts the conventional means of mature bolt, rivet, welding and the like in the prior art, the machinery, parts and equipment adopt the conventional models in the prior art, and the structure and principle of the parts known by the skilled person can be known by the technical manual or by the conventional experimental method.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a survey and drawing is with unmanned aerial vehicle support of parking, includes plate body (1), its characterized in that: limiting plates (2) are welded on two sides of the bottom of the plate body (1), a first sliding rod (3) is welded on the inner side of the limiting plate (2), a first sliding sleeve (4) is connected on two sides of the surface of the first sliding rod (3) in a sliding mode, a first buffering mechanism (5) is hinged to the bottom of the first sliding sleeve (4), the first buffering mechanism (5) comprises a first shell (51), a first spring (52), a sliding block (53) and a first supporting rod (54), a bottom plate (6) is hinged to the bottom of the first buffering mechanism (5), a second buffering mechanism (7) is fixedly installed on the inner side of the top of the bottom plate (6), the second buffering mechanism (7) comprises a second sliding rod (71), a block body (72), a second sliding sleeve (73), a second supporting rod (74), a pressing block (75), a second spring (76) and a second shell (77), the bottom of the plate body (1) is located on the outer side of the limiting plate body (8) in a welding mode, the bottom of the rod body (8) is hinged with a third buffer mechanism (9), and the third buffer mechanism (9) comprises a third sliding sleeve (91), a third sliding rod (92), a handle (93) and a third spring (94).
2. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: the bottom of first casing (51) is articulated with the center department at bottom plate (6) top, the bottom of first casing (51) inner chamber and the bottom welding of first spring (52), the top of first spring (52) and the bottom welding of slider (53), the side of slider (53) passes through the spout and the inner wall sliding connection of first casing (51), the top of slider (53) and the bottom welding of first branch (54), the top of first branch (54) is articulated with the bottom of first sliding sleeve (4).
3. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: the both sides of second slide bar (71) and the inboard welding of block (72), the bottom of block (72) and the right side welding at bottom plate (6) top, the surface of second slide bar (71) and the inner wall sliding connection of second sliding sleeve (73), the top of second sliding sleeve (73) is articulated with the bottom of second branch (74), second branch (74) run through second casing (77) and extend to the inner chamber of second casing (77) and the bottom sliding connection of briquetting (75), the top of briquetting (75) and the bottom welding of second spring (76), the top of second spring (76) and the top welding of second casing (77) inner chamber, the top of second casing (77) is articulated with the inboard middle part of first casing (51).
4. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: the inner wall of the third sliding sleeve (91) is in sliding connection with the surface of the third sliding rod (92), the inner end of the third sliding rod (92) is hinged to the middle of the outer side of the first shell (51), and the center of the top of the third sliding sleeve (91) is hinged to the bottom of the rod body (8).
5. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: a handle (93) is welded on one side, away from the first shell (51), of the third sliding rod (92), and third springs (94) are sleeved on the surfaces of the third sliding rod (92) and located on the two sides of the third sliding sleeve (91).
6. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: the number of the limiting plates (2) is four, and the limiting plates (2) are arranged at four corners of the bottom of the plate body (1) in a rectangular mode.
7. The unmanned aerial vehicle parking stand for surveying and mapping of claim 1, wherein: the quantity of the rod bodies (8) is four, and the rod bodies (8) are arranged in a rectangular shape and are arranged at four corners of the bottom of the plate body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921959658.XU CN210852979U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle parking support for surveying and mapping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921959658.XU CN210852979U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle parking support for surveying and mapping |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210852979U true CN210852979U (en) | 2020-06-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921959658.XU Expired - Fee Related CN210852979U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle parking support for surveying and mapping |
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| CN (1) | CN210852979U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
-
2019
- 2019-11-13 CN CN201921959658.XU patent/CN210852979U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
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Granted publication date: 20200626 Termination date: 20201113 |
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| CF01 | Termination of patent right due to non-payment of annual fee |