CN212605839U - Unmanned aerial vehicle aircraft capable of delivering goods - Google Patents
Unmanned aerial vehicle aircraft capable of delivering goods Download PDFInfo
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- CN212605839U CN212605839U CN202021345250.6U CN202021345250U CN212605839U CN 212605839 U CN212605839 U CN 212605839U CN 202021345250 U CN202021345250 U CN 202021345250U CN 212605839 U CN212605839 U CN 212605839U
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- 230000006835 compression Effects 0.000 claims description 16
- 238000007906 compression Methods 0.000 claims description 16
- 210000000078 claw Anatomy 0.000 claims description 8
- 230000003139 buffering effect Effects 0.000 description 12
- 230000035939 shock Effects 0.000 description 7
- 230000000694 effects Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
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- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009313 farming Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle aircraft that can deliver goods, including unmanned aerial vehicle body, buffer gear, camera, jack catch and support frame, two sets of support frames are installed to the bottom of unmanned aerial vehicle body, and the top of support frame all with unmanned aerial vehicle body fixed connection to the bottom of support frame all is equipped with the swing arm, the top of swing arm is articulated mutually with the support frame, and the bottom of swing arm all is equipped with the jack catch to jack catch and swing arm fixed connection, the top of swing arm all is equipped with and drives actuating block, and drives the bottom and swing arm fixed connection of actuating block to drive the unmanned aerial vehicle body bottom of actuating block one side and install two sets of actuating cylinders that drive, actuating cylinder's one end and unmanned aerial vehicle body fixed connection, actuating cylinder's the other end with drive actuating block. The utility model discloses not only realized that the unmanned aerial vehicle aircraft unloads to the stable transport of goods, reduced the impact force that the unmanned aerial vehicle organism received, stability when having improved the freight moreover.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle aircraft technical field specifically is an unmanned aerial vehicle aircraft of can delivering goods.
Background
Unmanned aerial vehicle for short is unmanned aerial vehicle, utilizes radio remote control equipment and self-contained program control device to fly, and wide application in fields such as aerial reconnaissance, supervision, communication, electronic interference, farming pasture and fishery, and unmanned aerial vehicle leaves more and more popular in the commodity circulation field, carries the parcel through the unmanned low-altitude aircraft that utilizes radio remote control equipment to control, reaches the destination automatically, in the great improvement delivery efficiency of remote area and the cost of labor has been reduced.
This type of unmanned aerial vehicle aircraft on the market today is various, can satisfy people's user demand basically, but still has certain problem, and specific problem has following several:
(1) the expansion buffering of supporting legs when present this type of unmanned aerial vehicle aircraft generally is not convenient for to descend when using to serious influence the degree of convenience when unmanned aerial vehicle aircraft uses.
(2) The buffering protection to the camera when present this type of unmanned aerial vehicle aircraft generally is not convenient for descend when using to great influence the security when unmanned aerial vehicle aircraft uses.
(3) The existing unmanned aerial vehicle aircraft is not convenient for stable transportation and unloading of cargoes when in use, thereby bringing great troubles to people.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle aircraft that can deliver goods to the expansion buffering of supporting leg when providing unmanned aerial vehicle aircraft and be not convenient for descend in solving above-mentioned background art, to the buffer protection of camera during the descending, be not convenient for the problem of the stable transport unloading of goods.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle aircraft capable of delivering goods comprises an unmanned aerial vehicle body, a buffer mechanism, a camera, a clamping jaw and support frames, wherein two groups of support frames are installed at the bottom end of the unmanned aerial vehicle body, the top ends of the support frames are fixedly connected with the unmanned aerial vehicle body, swing arms are arranged at the bottom ends of the support frames, the top ends of the swing arms are hinged with the support frames, the bottom ends of the swing arms are provided with the clamping jaws, the clamping jaws are fixedly connected with the swing arms, the top ends of the swing arms are provided with driving blocks, the bottom ends of the driving blocks are fixedly connected with the swing arms, two groups of driving cylinders are installed at the bottom end of the unmanned aerial vehicle body on one side of each driving block, one ends of the driving cylinders are fixedly connected with the unmanned aerial vehicle body, the other ends of the driving cylinders are hinged with the driving blocks, two, and the supporting seat is installed on the unmanned aerial vehicle body top of folding mechanism top, the top of supporting seat is equipped with the camera, and the inside buffer gear that is equipped with of supporting seat of camera below.
Preferably, buffer gear's inside has set gradually supporting spring, spacing axle, compression spring, catch bar and clamp plate, the inside of supporting seat is equipped with spacing axle, and the both ends of spacing axle all with supporting seat inner wall fixed connection to the surface cover of spacing axle is equipped with two sets of compression spring, has realized the buffering protection to the camera when unmanned aerial vehicle aircraft descends.
Preferably, the supporting seat top of spacing epaxial side is established friendly clamp plate, and the bottom of clamp plate is equipped with two sets of catch bars to the top of catch bar is articulated mutually with the clamp plate, and the bottom of catch bar is articulated mutually through the slider with compression spring, has reduced the impact force that the unmanned aerial vehicle organism received, has avoided the strong vibration of camera during operation to cause electronic component's damage.
Preferably, four groups of supporting springs are arranged at the top end of the supporting seat on one side of the limiting shaft, the bottom ends of the supporting springs are fixedly connected with the supporting seat, and the top ends of the supporting springs are fixedly connected with the pressing plate, so that the stable structure of the supporting springs is realized.
Preferably, folding mechanism's inside has set gradually miniature cylinder, hinge pin, auxiliary spring, gangbar and holder, the bottom mounting of unmanned aerial vehicle body has two sets of holders, and the bottom of holder all is equipped with the gangbar to the top of gangbar is articulated mutually with the holder, has realized the expansion buffering of supporting leg when the unmanned aerial vehicle aircraft descends.
Preferably, the bottom of gangbar is equipped with the hinge pin, and the gangbar is articulated mutually with the supporting leg through the hinge pin to the top of supporting leg is equipped with miniature cylinder, and miniature cylinder's bottom is articulated mutually with the supporting leg, and miniature cylinder's top is articulated mutually with the unmanned aerial vehicle body, be fixed with auxiliary spring on the outer wall of supporting leg one side, and auxiliary spring's top is articulated mutually with the gangbar, has improved unmanned aerial vehicle's shock attenuation effect.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle aircraft has not only realized that the unmanned aerial vehicle aircraft unloads to the stable transport of goods, has reduced the impact force that the unmanned aerial vehicle organism received, has improved the stability when freight moreover.
(1) Two sets of actuating cylinder movements of driving through unmanned aerial vehicle body received signal operation, promote by driving actuating cylinder and drive the piece and remove, under the support of support frame, by driving actuating block drive swing arm and removing, thereby take place the removal of angle by swing arm drive jack catch, the removal that another group's jack catch took place the angle is driven by another group to this principle, pick the centre gripping to the goods, transport automatic unloading after appointed destination when the goods, realized that the unmanned aerial vehicle aircraft unloads the stable transport of goods, stability when the freight has been improved.
(2) Through being provided with micro cylinder, the hinge pin, auxiliary spring, gangbar and holder, open two sets of micro cylinder through staff's remote operation, the rotation of angle takes place by micro cylinder drive supporting leg, the holder supports the supporting leg, under auxiliary spring's elasticity, under the articulated of hinge pin, the gangbar carries out folding support to the supporting leg, thereby it is folding by two sets of micro cylinder drive supporting legs, the buffering of expanding of supporting leg when having realized unmanned aerial vehicle aircraft descending, the impact force that the unmanned aerial vehicle organism received has been reduced, unmanned aerial vehicle's shock attenuation effect has been improved.
(3) Through being provided with supporting spring, spacing axle, compression spring, catch bar and clamp plate, run into the air current unstability through unmanned aerial vehicle body flight in-process, avoid the camera to produce strong vibration during perhaps descending, cushion the shock attenuation by buffer gear to the camera, four supporting spring of group support to clamp plate and supporting seat, when needs vibrations, the clamp plate promotes the catch bar and removes, the catch bar promotes compression spring and slides at the surface compression of spacing axle, carry out elastic support to the clamp plate jointly under four supporting spring's of group cooperation, the buffer protection to the camera when having realized unmanned aerial vehicle aircraft descending, avoided the strong vibration of camera during operation to cause electronic component's damage.
Drawings
Fig. 1 is a schematic view of the front view cross-sectional structure of the present invention.
Fig. 2 is a schematic side view of the cross-sectional structure of the present invention.
Fig. 3 is a schematic view of the sectional enlarged structure of the buffering mechanism of the present invention.
Fig. 4 is a schematic view of the cross-sectional enlarged structure of the folding mechanism of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a buffer mechanism; 201. a support spring; 202. a limiting shaft; 203. a compression spring; 204. a push rod; 205. pressing a plate; 3. a camera; 4. a supporting seat; 5. a drive block; 6. swinging arms; 7. a claw; 8. a support frame; 9. a driving cylinder; 10. supporting legs; 11. a folding mechanism; 1101. a micro cylinder; 1102. a hinge pin; 1103. an auxiliary spring; 1104. a linkage rod; 1105. a cage.
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, the present invention provides an embodiment: an unmanned aerial vehicle aircraft capable of delivering goods comprises an unmanned aerial vehicle body 1, a buffer mechanism 2, a camera 3, a claw 7 and support frames 8, wherein two groups of support frames 8 are installed at the bottom end of the unmanned aerial vehicle body 1, the top ends of the support frames 8 are fixedly connected with the unmanned aerial vehicle body 1, the bottom ends of the support frames 8 are respectively provided with a swing arm 6, the top ends of the swing arms 6 are hinged with the support frames 8, the bottom ends of the swing arms 6 are respectively provided with the claw 7, the claw 7 is fixedly connected with the swing arms 6, the top ends of the swing arms 6 are respectively provided with a driving block 5, the bottom ends of the driving blocks 5 are fixedly connected with the swing arms 6, two groups of driving cylinders 9 are installed at the bottom end of the unmanned aerial vehicle body 1 on one side of the driving block 5, one end of each driving cylinder 9 is fixedly connected with the unmanned aerial vehicle body 1, the, and 1 bottom of unmanned aerial vehicle body above supporting leg 10 is equipped with two sets of folding mechanism 11 to supporting seat 4 is installed on 1 top of unmanned aerial vehicle body above folding mechanism 11, and the top of supporting seat 4 is equipped with camera 3, and inside buffer gear 2 that is equipped with of supporting seat 4 below camera 3.
Two sets of actuating cylinder 9 motions of driving through the 1 received signal operation of unmanned aerial vehicle body during the use, promote by driving actuating cylinder 9 and drive actuating block 5 and remove, under the support of support frame 8, by driving actuating block 5 drive swing arm 6 and remove, thereby take place the removal of angle by swing arm 6 drive jack catch 7, the same principle is driven another set of jack catch 7 and takes place the removal of angle by another set of actuating cylinder 9 drive, pick the centre gripping to the goods, automatic unloading after appointed destination is transported to the goods, the unmanned aerial vehicle aircraft has been realized unloading to the stable transport of goods, stability when the freight has been improved.
The buffer mechanism 2 is internally provided with a support spring 201, a limit shaft 202, a compression spring 203, a push rod 204 and a pressing plate 205 in sequence, the inside of the support seat 4 is provided with the limit shaft 202, two ends of the limit shaft 202 are fixedly connected with the inner wall of the support seat 4, the surface of the limit shaft 202 is sleeved with two sets of compression springs 203, the top of the support seat 4 above the limit shaft 202 is provided with the pressing plate 205, the bottom end of the pressing plate 205 is provided with two sets of push rods 204, the top end of the push rod 204 is hinged with the pressing plate 205, the bottom end of the push rod 204 is hinged with the compression spring 203 through a sliding block, the top end of the support seat 4 on one side of the limit shaft 202 is provided with four sets of support springs 201, the bottom ends of the support springs 201 are fixedly connected with the.
Open two sets of microcylinders 1101 through staff's remote operation during the use, take place the rotation of angle by microcylinder 1101 drive supporting leg 10, holder 1105 supports supporting leg 10, under the elasticity of auxiliary spring 1103, under the articulated of hinge pin 1102, linkage 1104 carries out folding support to supporting leg 10, thereby it is folding to drive supporting leg 10 by two sets of microcylinders 1101, the buffering of expansion of supporting leg 10 when having realized that the unmanned aerial vehicle aircraft descends, the impact force that the unmanned aerial vehicle organism received has been reduced, unmanned aerial vehicle's shock attenuation effect has been improved.
The inside of folding mechanism 11 has set gradually miniature cylinder 1101, hinge pin 1102, auxiliary spring 1103, gangbar 1104 and holder 1105, the bottom mounting of unmanned aerial vehicle body 1 has two sets of holders 1105, and the bottom of holder 1105 all is equipped with gangbar 1104, and the top of gangbar 1104 is articulated with holder 1105, the bottom of gangbar 1104 is equipped with hinge pin 1102, and gangbar 1104 is articulated with supporting leg 10 through hinge pin 1102, and the top of supporting leg 10 is equipped with miniature cylinder 1101, the bottom of miniature cylinder 1101 is articulated with supporting leg 10, the top of miniature cylinder 1101 is articulated with unmanned aerial vehicle body 1, be fixed with auxiliary spring 1103 on the outer wall of supporting leg 10 one side, and the top of auxiliary spring 1103 is articulated with gangbar 1104.
Run into the air current unstable through unmanned aerial vehicle body 1 flight in-process during the use, perhaps take place violent vibration in order to avoid camera 3 when descending, cushion the shock attenuation by buffer gear 2 to camera 3, four group's supporting spring 201 support clamp plate 205 and supporting seat 4, when needs shake, clamp plate 205 promotes catch bar 204 and removes, catch bar 204 promotes compression spring 203 and slides at spacing shaft 202's surface compression, carry out elastic support to clamp plate 205 jointly under four group's supporting spring 201 cooperation, the buffer protection to camera 3 when having realized unmanned aerial vehicle aircraft descends, avoided the strong vibration of camera 3 during operation to cause electronic component's damage.
The working principle is as follows: when the unmanned aerial vehicle is used, firstly, two groups of driving cylinders 9 are operated to move by receiving signals through the unmanned aerial vehicle body 1, the driving cylinders 9 push the driving block 5 to move, under the support of the supporting frame 8, the driving block 5 drives the swing arm 6 to move, so that the swing arm 6 drives the claws 7 to move angularly, according to the principle, the other group of driving cylinders 9 drives the other group of claws 7 to move angularly to grab and clamp a cargo, the cargo is automatically unloaded after being conveyed to a specified destination, the stable conveying and unloading of the cargo by the unmanned aerial vehicle are realized, the stability during cargo transportation is improved, then, two groups of micro cylinders 1101 are opened through remote operation of a worker, the supporting legs 10 are driven to rotate angularly by the micro cylinders 1101, the supporting legs 10 are supported by the retainers 1105, under the elasticity of the auxiliary springs 1103 and under the hinging of the hinging pins 1102, the linkage rods 1104 are used for folding and supporting the supporting legs, therefore, the support legs 10 are driven by the two groups of micro cylinders 1101 to fold, the unfolding buffering of the support legs 10 when the unmanned aerial vehicle aircraft lands is realized, the impact force on the body of the unmanned aerial vehicle is reduced, the shock absorption effect of the unmanned aerial vehicle is improved, then the unmanned aerial vehicle body 1 encounters unstable airflow in the flying process or avoids strong vibration of the camera 3 when the unmanned aerial vehicle lands, the buffering and shock absorption are carried out on the camera 3 by the buffering mechanism 2, the four groups of support springs 201 support the pressing plate 205 and the support seat 4, when vibration is needed, the pressing plate 205 pushes the push rod 204 to move, the push rod 204 pushes the compression spring 203 to compress and slide on the surface of the limit shaft 202, the pressing plate 205 is elastically supported under the cooperation of the four groups of support springs 201, the buffering protection on the camera 3 when the unmanned aerial vehicle lands is realized, and the damage of electronic components caused by, to complete the use work of the unmanned aerial vehicle.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides a but unmanned aerial vehicle aircraft of delivery of goods, includes unmanned aerial vehicle body (1), buffer gear (2), camera (3), jack catch (7) and support frame (8), its characterized in that: two groups of supporting frames (8) are installed at the bottom end of the unmanned aerial vehicle body (1), the top ends of the supporting frames (8) are fixedly connected with the unmanned aerial vehicle body (1), swing arms (6) are arranged at the bottom ends of the supporting frames (8), the top ends of the swing arms (6) are hinged with the supporting frames (8), claws (7) are arranged at the bottom ends of the swing arms (6), the claws (7) are fixedly connected with the swing arms (6), driving blocks (5) are arranged at the top ends of the swing arms (6), the bottom ends of the driving blocks (5) are fixedly connected with the swing arms (6), two groups of driving cylinders (9) are installed at the bottom end of the unmanned aerial vehicle body (1) on one side of the driving blocks (5), one ends of the driving cylinders (9) are fixedly connected with the unmanned aerial vehicle body (1), the other ends of the driving cylinders (9) are hinged with the driving blocks (5), and supporting legs (10) are arranged at the bottom end of the, and unmanned aerial vehicle body (1) bottom of supporting leg (10) top is equipped with two sets of folding mechanism (11) to supporting seat (4) are installed on unmanned aerial vehicle body (1) top of folding mechanism (11) top, the top of supporting seat (4) is equipped with camera (3), and inside buffer gear (2) that is equipped with of supporting seat (4) of camera (3) below.
2. A deliverable unmanned aerial vehicle as claimed in claim 1, wherein: the inside of buffer gear (2) has set gradually supporting spring (201), spacing axle (202), compression spring (203), catch bar (204) and clamp plate (205), the inside of supporting seat (4) is equipped with spacing axle (202), and the both ends of spacing axle (202) all with supporting seat (4) inner wall fixed connection to the surface cover of spacing axle (202) is equipped with two sets of compression spring (203).
3. A deliverable unmanned aerial vehicle as claimed in claim 2, wherein: the top of the supporting seat (4) above the limiting shaft (202) is provided with a pressing plate (205), the bottom end of the pressing plate (205) is provided with two groups of push rods (204), the top ends of the push rods (204) are hinged with the pressing plate (205), and the bottom ends of the push rods (204) are hinged with the compression spring (203) through a sliding block.
4. A deliverable unmanned aerial vehicle as claimed in claim 3, wherein: four groups of supporting springs (201) are arranged at the top end of the supporting seat (4) on one side of the limiting shaft (202), the bottom ends of the supporting springs (201) are fixedly connected with the supporting seat (4), and the top ends of the supporting springs (201) are fixedly connected with the pressing plate (205).
5. A deliverable unmanned aerial vehicle as claimed in claim 1, wherein: the interior of folding mechanism (11) has set gradually miniature cylinder (1101), hinge pin (1102), auxiliary spring (1103), gangbar (1104) and holder (1105), the bottom mounting of unmanned aerial vehicle body (1) has two sets of holders (1105), and the bottom of holder (1105) all is equipped with gangbar (1104) to the top and the holder (1105) of gangbar (1104) are articulated mutually.
6. A deliverable unmanned aerial vehicle as claimed in claim 5, wherein: the bottom of gangbar (1104) is equipped with hinge pin (1102), and gangbar (1104) is articulated mutually with supporting leg (10) through hinge pin (1102) to the top of supporting leg (10) is equipped with miniature cylinder (1101), and the bottom of miniature cylinder (1101) is articulated mutually with supporting leg (10), and the top of miniature cylinder (1101) is articulated mutually with unmanned aerial vehicle body (1), be fixed with auxiliary spring (1103) on the outer wall of supporting leg (10) one side, and the top of auxiliary spring (1103) is articulated mutually with gangbar (1104).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021345250.6U CN212605839U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle aircraft capable of delivering goods |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021345250.6U CN212605839U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle aircraft capable of delivering goods |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212605839U true CN212605839U (en) | 2021-02-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021345250.6U Active CN212605839U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle aircraft capable of delivering goods |
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| Country | Link |
|---|---|
| CN (1) | CN212605839U (en) |
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2020
- 2020-07-10 CN CN202021345250.6U patent/CN212605839U/en active Active
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Legal Events
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| TR01 | Transfer of patent right |
Effective date of registration: 20231011 Address after: No. 107 Shahezi Village, Mengjiang Town, Shanhaiguan District, Qinhuangdao City, Hebei Province, 066000 Patentee after: Wang Shikuan Patentee after: Qiu Hao Patentee after: Zhang Zhongmou Address before: 226500 1003B, building 6, 999 Wanshou South Road, Chengnan street, Rugao City, Nantong City, Jiangsu Province Patentee before: Yunyi Zhichuang Aviation Technology (Nantong) Co.,Ltd. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20231127 Address after: No. 28, 1st Floor, Qinxin Electronic City, No. 138, Middle Section of Hebei Street, Jianshe Street, Haigang District, Qinhuangdao City, Hebei Province, 066000 Patentee after: Hebei Canzhou Decoration Engineering Co.,Ltd. Address before: No. 107 Shahezi Village, Mengjiang Town, Shanhaiguan District, Qinhuangdao City, Hebei Province, 066000 Patentee before: Wang Shikuan Patentee before: Qiu Hao Patentee before: Zhang Zhongmou |
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| TR01 | Transfer of patent right |