CN212423516U - Triaxial self-stabilizing optical pod holder device of multi-rotor unmanned aerial vehicle - Google Patents
Triaxial self-stabilizing optical pod holder device of multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN212423516U CN212423516U CN202021214344.XU CN202021214344U CN212423516U CN 212423516 U CN212423516 U CN 212423516U CN 202021214344 U CN202021214344 U CN 202021214344U CN 212423516 U CN212423516 U CN 212423516U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle, specifically be a many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device, including bottom plate, triaxial cloud platform, fixed plate, mounting panel, shock-resistant structure and shock-absorbing structure, the triaxial cloud platform is installed in the bottom plate bottom, be equipped with shock-resistant structure between bottom plate and the fixed plate, be equipped with shock-absorbing structure between fixed plate and the mounting panel, set up the regulation hole that is used for the screw installation on the mounting panel, shock-resistant structure includes fixing base, roating seat, articulated seat, fixed axle, connecting seat and spring, the fixing base sets up the middle part in the fixed plate bottom, the roating seat passes through bearing movable assembly and is in the fixing base, articulated seat welding is in the bottom. This many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device through setting up the structure of shocking resistance, receives forward or when backward impact at the triaxial cloud platform, can cushion it to reduce the impaired probability of triaxial cloud platform.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle has the characteristics of small volume, light weight, low cost, flexible operation and high safety, and is widely applied to the fields of aerial photography, detection, search and rescue, resource exploration and the like. And unmanned aerial vehicle itself has the big, the strong problem of vibrations of shake in the flight, for guaranteeing the quality of taking photo by plane and protecting the equipment of taking photo by plane, need use to increase steady cloud platform and come the equipment of taking photo by plane cooperation.
Because current unmanned aerial vehicle has the foot rest usually for the cloud platform that unmanned aerial vehicle carried is difficult for receiving the object impact of side direction, nevertheless, the front and the back of current unmanned aerial vehicle cloud platform do not possess corresponding protection machanism, can't cushion when the cloud platform receives the object and openly or the back is strikeed, appears the damage easily.
In order to solve the problem, the application provides a three-axis self-stabilizing optical nacelle holder device for a multi-rotor unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
Objects of the invention
For solving the technical problem who exists among the background art, the utility model provides a many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device has shock resistance's characteristics.
(II) technical scheme
In order to solve the technical problem, the utility model provides a multi-rotor unmanned aerial vehicle three-axis self-stabilizing optical pod holder device, which comprises a bottom plate, a three-axis holder, a fixed plate, a mounting plate, an impact-resistant structure and a damping structure;
the three-axis tripod head is installed in the bottom plate, be equipped with shock-resistant structure between bottom plate and the fixed plate, be equipped with shock-absorbing structure between fixed plate and the mounting panel.
Preferably, the mounting plate is provided with an adjusting hole for mounting a screw.
Preferably, shock-resistant structure includes fixing base, roating seat, articulated seat, fixed axle, connecting seat and spring, the fixing base sets up the middle part in the fixed plate bottom, the roating seat passes through bearing movable assembly and is in the fixing base, articulated seat welding is in the bottom of roating seat, the connecting seat welding is at the middle part on bottom plate top, and the connecting seat passes through fixed axle activity hinge joint on articulated seat, spring fixed connection is between bottom plate and fixed plate.
Preferably, the shock-absorbing structure comprises an air spring and a connecting bolt, and the air spring is connected between the mounting plate and the fixing plate through the connecting bolt.
Preferably, the rotating seat is I-shaped.
Preferably, the number of the springs is four, and the four springs are respectively arranged between the bottom plate and four corners of the fixing plate.
The above technical scheme of the utility model has following profitable technological effect:
1. this many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device through setting up the structure of shocking resistance, receives forward or when backward impact at the triaxial cloud platform, can cushion it to reduce the impaired probability of triaxial cloud platform.
2. This many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device through setting up shock-absorbing structure, can cushion the shock attenuation in the triaxial cloud platform use to improve the stability in the triaxial cloud platform use.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic view of the impact-resistant structure of the present invention.
Reference numerals:
1. a base plate; 2. a three-axis pan-tilt; 3. a fixing plate; 4. mounting a plate; 41. an adjustment hole; 5. an impact resistant structure; 51. a fixed seat; 52. a rotating base; 53. a hinged seat; 54. a fixed shaft; 55. a connecting seat; 56. a spring; 6. a shock-absorbing structure; 61. an air spring; 62. and connecting the bolts.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in detail with reference to the accompanying drawings. It should be understood that the description is intended to be illustrative only and is not intended to limit the scope of the present invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
Specific embodiments of the present invention will be described below with reference to the accompanying drawings.
Referring to fig. 1, the present invention provides a technical solution: the utility model provides a many rotor unmanned aerial vehicle triaxial is from steady optics nacelle cloud platform device, includes bottom plate 1, triaxial cloud platform 2, fixed plate 3, mounting panel 4, impact structure 5 and shock-absorbing structure 6.
Triaxial cloud platform 2 is installed in bottom plate 1 bottom, be equipped with impact structure 5 between bottom plate 1 and the fixed plate 3, be equipped with shock-absorbing structure 6 between fixed plate 3 and the mounting panel 4.
The mounting plate 4 is provided with an adjusting hole 41 for mounting a screw.
In this embodiment, utilize to set up the regulation hole 41 on mounting panel 4, this cloud platform device of being convenient for is whole with the installation of different model unmanned aerial vehicles, improves its adaptability.
The impact-resistant structure 5 includes a fixed seat 51, a rotating seat 52, a hinge seat 53, a fixed shaft 54, a connecting seat 55 and a spring 56.
The fixed seat 51 is arranged in the middle of the bottom end of the fixed plate 3, the rotating seat 52 is in an I shape, and the rotating seat 52 is movably assembled in the fixed seat 51 through a bearing.
In the present embodiment, the rotating seat 52 and the fixed seat 51 enable the bottom plate 1 and the fixed plate 3 to be rotatably installed, so that when the three-axis pan/tilt head 2 is impacted laterally, the bottom plate 1 can be matched with the torsion of the spring 56 to buffer the impact force, thereby reducing the probability of damage to the three-axis pan/tilt head 2.
The hinged seat 53 is welded at the bottom of the rotating seat 52, the connecting seat 55 is welded at the middle of the top end of the bottom plate 1, the connecting seat 55 is movably hinged on the hinged seat 53 through a fixing shaft 54, and the spring 56 is fixedly connected between the bottom plate 1 and the fixing plate 3.
It should be noted that the number of the springs 56 is four, and four springs 56 are respectively disposed between the bottom plate 1 and the four corners of the fixing plate 3.
Because the both sides of unmanned aerial vehicle's bottom have the foot rest, the probability that triaxial cloud platform 2 receives two side impact is less, and receives the impact at front or the back great, for this reason, in this embodiment, through connecting seat 55 and articulated seat 53 make between bottom plate 1 and the fixed plate 3 can be preceding, the rotation of back, cooperation spring 56 receives the impact at front or the back at the triaxial cloud platform, through the compression and the extension of spring 56, make connecting seat 55 and articulated seat 53 elastic rotation cushion to reduce the impact force that triaxial cloud platform 2 received.
Referring to fig. 1-2, the shock absorbing structure 6 includes an air spring 61 and a connecting bolt 62, and the air spring 61 is connected between the mounting plate 4 and the fixing plate 3 through the connecting bolt 62.
In this embodiment, the vibration of the three-axis pan/tilt head 2 can be buffered and damped by the air spring 61 disposed between the mounting plate 4 and the fixing plate 3, so as to reduce the vibration of the three-axis pan/tilt head 2 and improve the stability of the three-axis pan/tilt head 2 during use.
It is to be understood that the above-described embodiments of the present invention are merely illustrative of or explaining the principles of the invention and are not to be construed as limiting the invention. Therefore, any modification, equivalent replacement, improvement and the like made without departing from the spirit and scope of the present invention should be included in the protection scope of the present invention. Further, it is intended that the appended claims cover all such variations and modifications as fall within the scope and boundaries of the appended claims or the equivalents of such scope and boundaries.
Claims (6)
1. A multi-rotor unmanned aerial vehicle three-axis self-stabilization optical pod holder device is characterized by comprising a bottom plate (1), a three-axis cradle head (2), a fixing plate (3), a mounting plate (4), an impact-resistant structure (5) and a damping structure (6);
the three-axis tripod head (2) is installed in bottom plate (1) bottom, be equipped with between bottom plate (1) and fixed plate (3) shock-resistant structure (5), be equipped with shock-absorbing structure (6) between fixed plate (3) and mounting panel (4).
2. The device of claim 1, wherein the mounting plate (4) is provided with adjusting holes (41) for mounting screws.
3. The device of claim 1, wherein the impact-resistant structure (5) comprises a fixed seat (51), a rotating seat (52), a hinged seat (53), a fixed shaft (54), a connecting seat (55) and a spring (56), the fixed seat (51) is arranged in the middle of the bottom end of the fixed plate (3), the rotating seat (52) is movably assembled in the fixed seat (51) through a bearing, the hinged seat (53) is welded at the bottom of the rotating seat (52), the connecting seat (55) is welded in the middle of the top end of the bottom plate (1), the connecting seat (55) is movably hinged on the hinged seat (53) through the fixed shaft (54), and the spring (56) is fixedly connected between the bottom plate (1) and the fixed plate (3).
4. The device according to claim 1, wherein the shock absorbing structure (6) comprises an air spring (61) and a connecting bolt (62), and the air spring (61) is connected between the mounting plate (4) and the fixing plate (3) through the connecting bolt (62).
5. The triple-axis self-stabilizing optical pod-holder apparatus of claim 3, wherein the swivel (52) is "i" shaped.
6. The device according to claim 3, wherein said springs (56) are four in number, and four springs (56) are respectively disposed between four corners of the base plate (1) and the fixed plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021214344.XU CN212423516U (en) | 2020-06-28 | 2020-06-28 | Triaxial self-stabilizing optical pod holder device of multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021214344.XU CN212423516U (en) | 2020-06-28 | 2020-06-28 | Triaxial self-stabilizing optical pod holder device of multi-rotor unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN212423516U true CN212423516U (en) | 2021-01-29 |
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| CN202021214344.XU Active CN212423516U (en) | 2020-06-28 | 2020-06-28 | Triaxial self-stabilizing optical pod holder device of multi-rotor unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114183494A (en) * | 2021-12-06 | 2022-03-15 | 中国科学院长春光学精密机械与物理研究所 | Passive self-stabilizing vibration reduction platform for aerial downward-looking camera |
-
2020
- 2020-06-28 CN CN202021214344.XU patent/CN212423516U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114183494A (en) * | 2021-12-06 | 2022-03-15 | 中国科学院长春光学精密机械与物理研究所 | Passive self-stabilizing vibration reduction platform for aerial downward-looking camera |
| CN114183494B (en) * | 2021-12-06 | 2024-01-26 | 中国科学院长春光学精密机械与物理研究所 | Passive self-stabilizing vibration reduction platform for aviation downward-looking camera |
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