CN210416980U - A many rotor unmanned aerial vehicle for meteorological analysis - Google Patents
A many rotor unmanned aerial vehicle for meteorological analysis Download PDFInfo
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- CN210416980U CN210416980U CN201920951575.XU CN201920951575U CN210416980U CN 210416980 U CN210416980 U CN 210416980U CN 201920951575 U CN201920951575 U CN 201920951575U CN 210416980 U CN210416980 U CN 210416980U
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Abstract
The utility model discloses a many rotor unmanned aerial vehicle for meteorological analysis, including many rotor unmanned aerial vehicle and meteorological instrument body, the last fixed surface of meteorological instrument body installs the handle fixed mounting has quick detach mounting structure on the cargo platform of many rotor unmanned aerial vehicle's upper surface, the meteorological instrument body passes through quick detach mounting structure movable mounting on many rotor unmanned aerial vehicle's cargo platform. The utility model discloses an above-mentioned isotructure's cooperation has realized when stable based on mounting structure, conveniently installs fast and dismantles the effect.
Description
Technical Field
The utility model relates to a many rotor unmanned aerial vehicle technical field specifically is a many rotor unmanned aerial vehicle for meteorological analysis.
Background
A multi-rotor unmanned aerial vehicle is a special unmanned helicopter with three or more rotor shafts. It is rotated by a motor on each shaft, driving the rotor, thereby generating lift. The collective pitch of the rotors is fixed and not variable as in a typical helicopter. Through changing the relative speed between the different rotors, the size of unipolar propulsive force can be changed to the orbit of control aircraft. It is strong with the nature controlled, but VTOL and hover, and the wide application in meteorological analysis field, wherein be used for meteorological analysis's many rotor unmanned aerial vehicle include meteorological instrument and many rotor unmanned aerial vehicle, and meteorological instrument is the professional equipment that is used for meteorological service fields such as weather forecast, meteorological monitoring. Can be classified into two categories, namely a ground meteorological observation instrument and a high-altitude meteorological detection instrument. Mainly have anemoscope, humiture record appearance, sensor, wind speed alarm appearance, wind energy anemoscope, meteorological center software, GPRS wireless transmission module etc. and traditional many rotor unmanned aerial vehicle that is used for meteorological analysis, meteorological instrument are difficult to quick dismouting of carrying on, when detecting and maintaining its inside data, need relapse the loaded down with trivial details mounting structure of dismouting, and it is not convenient enough to use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a many rotor unmanned aerial vehicle for meteorological analysis possesses when stable based on mounting structure, conveniently carries out the advantage of quick installation and dismantlement, has solved the problem that meteorological instrument body in traditional meteorological analysis's many rotor unmanned aerial vehicle is difficult to carry out the dismouting.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a many rotor unmanned aerial vehicle for meteorological analysis, includes many rotor unmanned aerial vehicle and meteorological instrument body, the last fixed surface of meteorological instrument body installs the handle fixed mounting has quick detach mounting structure on the cargo platform of many rotor unmanned aerial vehicle's upper surface, the meteorological instrument body passes through quick detach mounting structure movable mounting on many rotor unmanned aerial vehicle's cargo platform.
The quick-release mounting structure comprises a connecting base, the connecting base is detachably connected on a carrying platform of the multi-rotor unmanned aerial vehicle through a bolt, the connecting base is internally provided with an installation groove, the groove of the installation groove is internally connected with a sliding clamping plate in a sliding way, one ends of two return springs are fixedly connected with the back surface of the sliding clamping plate, the other ends of the two return springs are fixedly connected with the wall of the mounting groove, the front surface of the sliding clamping plate is fixedly connected with a connecting rod, the connecting rod penetrates through the connecting base to be fixedly connected with a button, the bottom of the mounting groove is provided with four slots, the surface of the sliding clamping plate is provided with four rectangular through holes corresponding to the four slots, the lower fixed surface of meteorological instrument body is connected with four trips, the meteorological instrument body is placed in the inslot of mounting groove and passes four rectangle through-holes through four trips and penetrate four slots in with the slip cardboard joint.
Preferably, the four slots are distributed symmetrically in front, back, left and right directions along a symmetry axis of the connecting base.
Preferably, the meteorological instrument body is matched with the mounting groove.
Preferably, the bottom of the mounting groove is fixedly connected with a compression spring.
Preferably, a spring groove is formed in the plate of the sliding clamping plate, and the compression spring penetrates through the spring groove to be mutually extruded with the lower surface of the meteorological instrument body.
Compared with the prior art, the beneficial effects of the utility model are as follows:
firstly, the utility model arranges the meteorological instrument body in the mounting groove by arranging the quick-release mounting structure, the meteorological instrument body is fixed in the mounting groove through the clamping fit of the sliding clamping plate, the two return springs and the four clamping hooks, when the meteorological instrument body is required to be taken down from the multi-rotor unmanned aerial vehicle and used independently to analyze internal data and the like, the sliding clamping plate is driven by the pressing button through the connecting rod, the two reset springs are extruded along the bottom of the mounting groove to slide, so that the clamping hook and the sliding clamping plate are released from clamping, the meteorological instrument body can be taken out of the mounting groove, when in mounting, the four clamping hooks penetrate through the four rectangular through holes and penetrate into the four slots, and are clamped with the sliding clamping plate under the elastic action of the two reset springs, can install, realize based on mounting structure stable while, conveniently install fast and the effect of dismantling.
Two, the utility model discloses a set up compression spring and spring groove, after releasing the joint with trip and slip cardboard through pressing the button, under compression spring's elastic action, can make the trip extract the rectangle through-hole with meteorological instrument body rebound to realize that the one-hand can carry out the effect of dismantling the operation fast.
Drawings
FIG. 1 is a front view of the present invention;
FIG. 2 is a front sectional view of the quick release mounting structure of the present invention;
FIG. 3 is a front sectional view of the quick release mounting structure of the present invention;
fig. 4 is a top sectional view of the quick release mounting structure of the present invention.
In the figure: the system comprises a 1-multi-rotor unmanned aerial vehicle, a 2-meteorological instrument body, a 3-handle, a 4-quick-release mounting structure, a 5-connecting base, a 6-mounting groove, a 7-sliding clamping plate, an 8-reset spring, a 9-connecting rod, a 10-button, an 11-slot, a 12-rectangular through hole, a 13-clamping hook, a 14-compression spring and a 15-spring groove.
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 to 4, the present invention provides a technical solution: the utility model provides a many rotor unmanned aerial vehicle for meteorological analysis, includes many rotor unmanned aerial vehicle 1 and meteorological instrument body 2, the utility model discloses well meteorological instrument body 2 is meteorological instrument, is the professional equipment that is used for meteorological service fields such as meteorological forecast, meteorological monitoring. Can be classified into two categories, namely a ground meteorological observation instrument and a high-altitude meteorological detection instrument. Mainly there are anemoscope, humiture record appearance, a sensor, wind speed alarm appearance, wind energy anemoscope, meteorological center software, GPRS wireless transmission module etc. its model is L99-FSFX meteorological scientific research instrument, fixed surface installs fixed mounting has quick detach mounting structure 4 on the objective platform of the upper surface of 3 many rotor unmanned aerial vehicle 1 of handle on meteorological instrument body 2's the last surface, meteorological instrument body 2 is on many rotor unmanned aerial vehicle 1's objective platform through 4 movable mounting of quick detach mounting structure.
The quick-release mounting structure 4 comprises a connecting base 5, the connecting base 5 is detachably connected on a carrying platform of the multi-rotor unmanned aerial vehicle 1 through bolts, a mounting groove 6 is arranged in the connecting base 5, a sliding clamping plate 7 is connected in the groove of the mounting groove 6 in a sliding manner, one end of two reset springs 8 is fixedly connected to the back surface of the sliding clamping plate 7, the other end of each reset spring 8 is fixedly connected to the groove wall of the mounting groove 6, a connecting rod 9 is fixedly connected to the front surface of the sliding clamping plate 7, the connecting rod 9 penetrates through a button 10 fixedly connected to the connecting base 5, four slots 11 are arranged at the bottom of the mounting groove 6, the four slots 11 are symmetrically distributed along the symmetrical axis of the connecting base 5 in the front-back and left-right directions, so that the stress of the connecting structure is more uniform, the stability of the clamping, the lower surface of the meteorological instrument body 2 is fixedly connected with four clamping hooks 13, the meteorological instrument body 2 is placed in a groove of the mounting groove 6 and passes through four rectangular through holes 12 through the four clamping hooks 13 to penetrate into four slots 11 to be clamped with the sliding clamping plate 7, the meteorological instrument body 2 is placed in the mounting groove 6 by arranging the quick-release mounting structure 4, the meteorological instrument body 2 is matched with the four clamping hooks 7 through the clamping of the sliding clamping plate 7, the meteorological instrument body 2 is fixed in the mounting groove 6, the meteorological instrument body 2 is taken down from the multi-rotor unmanned aerial vehicle 1 when needed, the meteorological instrument is used independently, internal data and the like are analyzed, the sliding clamping plate 7 is driven by the pressing button 10 through the connecting rod 9, the two resetting springs 8 are extruded to slide along the bottom of the mounting groove 6, so that the clamping hooks 13 and the sliding clamping plate 7 are released, namely the meteorological instrument body 2 can be, during installation, the four clamping hooks 13 penetrate through the four rectangular through holes 12 into the four slots 11 and are clamped with the sliding clamping plate 7 under the elastic action of the two reset springs 8, so that installation can be carried out, the effect of convenient and rapid installation and disassembly based on stable installation structure is realized, the meteorological instrument body 2 is matched with the installation groove 6, the structure is more tightly matched, relative shaking caused by overlarge connection gap is prevented, the normal service life of the device is influenced, the stability of the structure is effectively improved, the compression spring 14 is fixedly connected to the bottom of the installation groove 6, the spring groove 15 is formed in the plate of the sliding clamping plate 7, the compression spring 14 penetrates through the spring groove 15 to be mutually extruded with the lower surface of the meteorological instrument body 2, after the clamping hooks 13 and the sliding clamping plate 7 are released through the press button 10, the meteorological instrument body 2 can be upwards sprung under the elastic action of the compression spring 14, the hook 13 is pulled out of the rectangular through hole 12, so that the effect of rapid disassembly operation by one hand is achieved.
The working principle is as follows: when the multi-rotor unmanned aerial vehicle for meteorological analysis is used, the meteorological instrument body 2 is placed in the mounting groove 6, the meteorological instrument body 2 is fixed in the mounting groove 6 through the clamping fit of the sliding clamping plate 7, the two return springs 8 and the four clamping hooks 13, when the meteorological instrument body 2 needs to be taken down from the multi-rotor unmanned aerial vehicle 1 and used independently to analyze internal data and the like, the sliding clamping plate 7 is carried by pressing the button 10, the two return springs 8 are extruded to slide, so that the clamping hook 13 is released from clamping with the sliding clamping plate 7, the meteorological instrument body 2 can be taken out of the mounting groove 6, when in mounting, the four clamping hooks 13 penetrate through the four rectangular through holes 12 and penetrate into the four slots 11, and are clamped with the sliding clamping plate 7 under the elastic action of the two return springs 8, can install, realize based on mounting structure stable while, conveniently install fast and the effect of dismantling.
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 (5)
1. A many rotor unmanned aerial vehicle for meteorological analysis, includes many rotor unmanned aerial vehicle (1) and meteorological instrument body (2), its characterized in that: a handle (3) is fixedly arranged on the upper surface of the meteorological instrument body (2), a quick-release mounting structure (4) is fixedly arranged on a carrying platform on the upper surface of the multi-rotor unmanned aerial vehicle (1), and the meteorological instrument body (2) is movably arranged on the carrying platform of the multi-rotor unmanned aerial vehicle (1) through the quick-release mounting structure (4);
the quick-release mounting structure (4) comprises a connecting base (5), the connecting base (5) is detachably connected to a carrying platform of the multi-rotor unmanned aerial vehicle (1) through bolts, a mounting groove (6) is formed in the connecting base (5), a sliding clamping plate (7) is slidably connected in a groove of the mounting groove (6), one end of two reset springs (8) is fixedly connected to the back surface of the sliding clamping plate (7), the other end of each reset spring (8) is fixedly connected to the groove wall of the mounting groove (6), a connecting rod (9) is fixedly connected to the front surface of the sliding clamping plate (7), the connecting rod (9) penetrates through the connecting base (5) and is fixedly connected with a button (10), four slots (11) are formed in the bottom of the mounting groove (6), four rectangular through holes (12) are formed in positions, corresponding to the four slots (11), on the surface of the sliding clamping plate (7, the lower surface fixedly connected with four trip (13) of meteorological instrument body (2), meteorological instrument body (2) are placed in the inslot of mounting groove (6) and are passed four rectangle through-holes (12) through four trip (13) and penetrate four slots (11) in with slip cardboard (7) joint.
2. A multi-rotor drone for meteorological analysis according to claim 1, characterized in that: the four slots (11) are symmetrically distributed along the symmetrical axis of the connecting base (5).
3. A multi-rotor drone for meteorological analysis according to claim 1, characterized in that: the meteorological instrument body (2) is matched with the mounting groove (6).
4. A multi-rotor drone for meteorological analysis according to claim 1, characterized in that: the bottom of the mounting groove (6) is fixedly connected with a compression spring (14).
5. A multi-rotor drone for meteorological analysis according to claim 4, characterized in that: a spring groove (15) is formed in the plate of the sliding clamping plate (7), and the compression spring (14) penetrates through the spring groove (15) to be mutually extruded with the lower surface of the meteorological instrument body (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920951575.XU CN210416980U (en) | 2019-06-24 | 2019-06-24 | A many rotor unmanned aerial vehicle for meteorological analysis |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920951575.XU CN210416980U (en) | 2019-06-24 | 2019-06-24 | A many rotor unmanned aerial vehicle for meteorological analysis |
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| Publication Number | Publication Date |
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| CN210416980U true CN210416980U (en) | 2020-04-28 |
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| CN201920951575.XU Active CN210416980U (en) | 2019-06-24 | 2019-06-24 | A many rotor unmanned aerial vehicle for meteorological analysis |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112339980A (en) * | 2020-11-27 | 2021-02-09 | 中国科学院沈阳自动化研究所 | Torch transmission unmanned aerial vehicle |
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2019
- 2019-06-24 CN CN201920951575.XU patent/CN210416980U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112339980A (en) * | 2020-11-27 | 2021-02-09 | 中国科学院沈阳自动化研究所 | Torch transmission unmanned aerial vehicle |
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