CN212172558U - Unmanned aerial vehicle task equipment mounting structure - Google Patents
Unmanned aerial vehicle task equipment mounting structure Download PDFInfo
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- CN212172558U CN212172558U CN202020439398.XU CN202020439398U CN212172558U CN 212172558 U CN212172558 U CN 212172558U CN 202020439398 U CN202020439398 U CN 202020439398U CN 212172558 U CN212172558 U CN 212172558U
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Abstract
The utility model belongs to an unmanned aerial vehicle mounting structure, which provides an unmanned aerial vehicle task equipment mounting structure for solving the technical problems of single task execution and low economy of the existing unmanned aerial vehicle equipment, and comprises an equipment switching frame and a protective cover; the equipment switching frame is arranged at the top of the task equipment, and a balancing weight and an equipment mounting frame are arranged on the equipment switching frame; a fuselage mounting seat is arranged below the unmanned aerial vehicle body; when the task equipment is installed on the unmanned aerial vehicle body, the equipment installation frame is detachably connected with the machine body installation seat; task equipment is located to the protective cover outside, and the protective cover can be dismantled and connect on the unmanned aerial vehicle body. Through the unified connection structure interface of task equipment and unmanned aerial vehicle body design, the uniformity problem of mounting structure and focus trim in the installation of multiple different task equipment has been solved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle mounting structure, concretely relates to unmanned aerial vehicle task equipment mounting structure.
Background
Currently, unmanned aerial vehicles are widely used in monitoring, target positioning, target damage assessment, electronic countermeasure, communication relay and other fields. Because unmanned aerial vehicle cost is lower, the security is good and the performance is outstanding in practice, consequently the market demand is urgent, and the user especially needs one kind can carry on multitask equipment, and the unmanned aerial vehicle that the reloading is convenient and the performance is good. What needs to be considered then is the safety, reliability, convenience and economy requirements of the structural design of the drone.
The existing unmanned aerial vehicle task equipment is not allowed to be reloaded due to the fact that safety problems related to gravity center balancing are considered, one unmanned aerial vehicle is fixedly loaded with one or more types of task equipment. However, users often need to execute diversified tasks, and the task equipment needs to be replaced in the using process in consideration of compatibility and economical efficiency of different task equipment. Based on above-mentioned contradiction, the mounting means of current unmanned aerial vehicle and task equipment mainly has the task singleness that unmanned aerial vehicle can carry out, can't adapt to the problem of diversified task demand, simultaneously, when having multiple task equipment to load the requirement, foretell loading means can increase unmanned aerial vehicle demand quantity, and then increases purchasing cost, reduces economic nature.
Disclosure of Invention
The utility model discloses a main objective is to solve the mounting means of current unmanned aerial vehicle task equipment, has the task singleness that unmanned aerial vehicle can carry out, can't adapt to diversified task demand to and the increase purchasing cost that leads to, technical problem that economic nature is low provides an unmanned aerial vehicle task equipment mounting structure.
In order to achieve the purpose, the invention provides the following technical scheme:
an unmanned aerial vehicle task equipment mounting structure is characterized by comprising an unmanned aerial vehicle body, an equipment switching frame and a protective cover;
the equipment switching frame is arranged at the top of the task equipment, and a balancing weight and an equipment mounting frame are arranged on the equipment switching frame;
a fuselage mounting seat is arranged below the unmanned aerial vehicle body;
the equipment mounting frame is detachably connected with the machine body mounting seat; task equipment is located to the protective cover outside, and the protective cover can be dismantled and connect on the unmanned aerial vehicle body.
Further, the equipment mounting rack comprises two equipment mounting rods which are arranged in parallel; the machine body mounting seat comprises two machine body mounting rods which are arranged in parallel; when task equipment installs on the unmanned aerial vehicle body, two equipment fixing pole can dismantle with the fuselage installation pole of next-door neighbour respectively and be connected.
Further, when task equipment installs on the unmanned aerial vehicle body, two fuselage installation poles are located the outside of two equipment fixing poles respectively, and closely adjacent fuselage installation pole and equipment fixing pole are respectively through at least one pin or screw connection.
Further, the front of the protective cover is streamlined.
Further, the fuselage installation pole passes through the screw or splices and installs in the below of unmanned aerial vehicle body.
Furthermore, the equipment switching frame is connected with the task equipment through screws, and the equipment mounting rod and the balancing weight are mounted on the equipment switching frame through screws.
Compared with the prior art, the invention has the beneficial effects that:
1. the utility model discloses an unmanned aerial vehicle task equipment mounting structure, with the base of unmanned aerial vehicle body as task equipment installation, at unmanned aerial vehicle body lower part erection equipment mounting bracket, task equipment passes through the equipment fixing frame on the equipment switching frame and installs task equipment in the lower part of unmanned aerial vehicle body, and the protective cover is established outside task equipment as an independent part cover, has the guard action to task equipment. Through foretell mounting structure, different task equipment are equipped with the same equipment fixing frame, the unmanned aerial vehicle body is equipped with the same fuselage mount pad, when task equipment dispatches from the factory, only need through design balancing weight and equipment switching frame, for the corresponding equipment switching frame of different task equipment configurations, and accomplish the counter weight through the balancing weight in advance, can realize that every kind of task equipment reloads back unmanned aerial vehicle body focus all in focus within range, and reloads process easy operation, can accomplish task equipment fast and reloads. Through the unified connection structure interface of task equipment and unmanned aerial vehicle body design, the uniformity problem of mounting structure and focus trim in the installation of multiple different task equipment has been solved.
2. The utility model discloses in the connection structure for task equipment and unmanned aerial vehicle body design, can dismantle the fuselage installation pole and the equipment fixing pole of connection and accomplish through two, when the installation, specific outside that can make two fuselage installation poles be located two equipment fixing poles is through at least one pin or screwed connection. Aforementioned connection structure is simple workable, also can accomplish fast when the dismouting and dismantle and install the back firm.
3. The utility model discloses well equipment switching frame, equipment fixing pole, balancing weight and the connected mode of fuselage mounting pole are simple and convenient, are convenient for maintain, install and change, do benefit to production and use site management and control.
Drawings
Fig. 1 is an exploded view of an embodiment of the present invention;
fig. 2 is a schematic structural diagram of the embodiment of the present invention after the task equipment is installed;
FIG. 3 is a schematic view of the FIG. 2 with the protective cover removed;
fig. 4 is a sectional view a-a of fig. 3.
The unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, task equipment 2, equipment switching frames 3, balancing weights 4, equipment mounting frames 5, equipment mounting rods 501, a machine body mounting seat 6, a machine body mounting rod 601, a protective cover 7 and pins 8.
Detailed Description
The technical solution of the present invention will be clearly and completely described below with reference to the embodiments of the present invention and the accompanying drawings, and it is obvious that the described embodiments do not limit the present invention.
The utility model discloses a solve the uniformity problem of mounting structure and focus trim in the 2 installation processes of multiple different task equipment, through for task equipment 2 and the unified connection structure of unmanned aerial vehicle body 1 design, match corresponding equipment switching frame 3 for task equipment 2 in advance to install corresponding balancing weight 4, realized that different task equipment 2 changes the outfit fast, solved the problem that current unmanned aerial vehicle body 1 can't adapt to diversified task demand, effectively reduced purchasing cost, the economic nature has been improved.
Referring to fig. 1 and 2, an unmanned aerial vehicle task equipment mounting structure includes an unmanned aerial vehicle body 1, an equipment switching frame 3 and a protective cover 7. The equipment switching frame 3 is installed at the top of the task equipment 2, the balancing weight 4 and the equipment installation frame 5 are installed on the equipment switching frame 3, the balancing weight 4 and the equipment switching frame 3 are designed in advance when the task equipment 2 leaves a factory, the balance weight design is completed in advance for different task equipment 2, and when the equipment switching frame is installed on the unmanned aerial vehicle body 1, the balance weight adjustment is not needed again; furthermore, according to the difference of the task devices 2, appropriate device adapter racks 3 are configured for the task devices 2, and the device adapter racks 3 need to be designed or adjusted according to the structures, installation surface forms, weights and the like of the corresponding task devices 2, so that the assembly safety of the task devices 2, the installation performance of the balancing weights 4 and the device installation frames 5 on the task devices 2 and the like can be guaranteed. The equipment adapter rack 3 is a switching platform for installing different task equipment 2.
Correspondingly, fuselage mount pad 6 is installed to the below of unmanned aerial vehicle body 1 for be connected with equipment fixing frame 5 on the equipment switching frame 3, the connection of here is for dismantling the connection, when installing task equipment 2 on unmanned aerial vehicle body 1, equipment fixing frame 5 links to each other through the mode that can dismantle the connection with fuselage mount pad 6, protective cover 7 cover is established in task equipment 2's outside, has the guard action to task equipment 2, and protective cover 7 can be dismantled and connect on unmanned aerial vehicle body 1. The appearance of protective cover 7 can design according to task equipment 2's shape, and as an optimal selection scheme, its front portion can be designed for streamlined for reduce protective cover 7's air resistance, avoid increasing extra resistance for unmanned aerial vehicle body 1's flight. Protective cover 7 can be dismantled with unmanned aerial vehicle body 1 and be connected, accessible screwed connection, also can dismantle the mode of connection through other.
As shown in fig. 3 and 4, in an embodiment of the present invention, the specific structure of the above-mentioned fuselage mounting seat 6 and the equipment mounting frame 5 is that, the equipment mounting frame 5 includes two equipment mounting rods 501 arranged in parallel, the fuselage mounting seat 6 includes two fuselage mounting rods 601 arranged in parallel, when installing the task equipment 2 on the unmanned aerial vehicle body 1, the two fuselage mounting rods 601 are respectively located at the outer sides of the two equipment mounting rods 501, and the next-to-adjacent fuselage mounting rods 601 and the equipment mounting rods 501 are respectively connected through two pins 8 located at both ends. When equipment reloads, demolish protective cover 7 from unmanned aerial vehicle body 1 earlier, lift four pins 8 off again, make unmanned aerial vehicle body 1 and task equipment 2 alternate segregation, then link to each other new task equipment 2's equipment fixing pole 501 with fuselage installation pole 601, establish protective cover 7 cover again and install in task equipment 2's outside, link to each other protective cover 7 with unmanned aerial vehicle body 1, accomplish task equipment's reloading promptly.
The utility model discloses an in other embodiments, can change pin 8 into screw or other convenient connecting pieces of dismantling, in addition, except the connection structure of above-mentioned fuselage installation pole 601 and equipment fixing pole 501, other current structures of being convenient for can dismantle the connection, as long as can be general in unmanned aerial vehicle body 1 and task equipment 2.
The fuselage of unmanned aerial vehicle body 1 can be as the mounting base of task equipment 2, and fuselage mount pad 6 can be for gluing with the fuselage casing of unmanned aerial vehicle body 1, also can be as an organic whole with the screw connection. The task equipment 2 is generally connected with the equipment adapter rack 3 through screws, the equipment adapter rack 3 is connected with the equipment mounting rack 5 through screws, and the balancing weight 4 is generally connected with the equipment adapter rack 3 through screws. Screws or pins 8 may be used as connectors to connect the equipment mounting 5 and the fuselage mounting 6, and the protective cover 7 as a separate component.
The utility model discloses convenient to use, when reloading task equipment 2 to unmanned aerial vehicle body 1, can quick assembly disassembly, avoid unnecessary operation. In addition, mounting structure's security is high, and the focus of unmanned aerial vehicle body 1 has been adjusted through the counter weight to with the counter weight with the form integration of balancing weight 4 on equipment switching frame 3, avoided the focus that later stage operation leads to change, endanger flight safety. Moreover, the holistic economic nature of mounting structure is higher, makes unmanned aerial vehicle body 1 possess the ability that a tractor serves several tasks loaded.
The above description is only an embodiment of the present invention, and is not intended to limit the scope of the present invention, and all equivalent structural changes made by using the contents of the present specification and the drawings, or applied directly or indirectly to other related technical fields, are included in the scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle task equipment mounting structure which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), an equipment switching frame (3) and a protective cover (7);
the equipment switching frame (3) is arranged at the top of the task equipment (2), and a balancing weight (4) and an equipment mounting frame (5) are arranged on the equipment switching frame (3);
a fuselage mounting seat (6) is arranged below the unmanned aerial vehicle body (1);
the equipment mounting frame (5) is detachably connected with the machine body mounting seat (6); task equipment (2) outside is located to protective cover (7) cover, and protective cover (7) can be dismantled and connect on unmanned aerial vehicle body (1).
2. The unmanned aerial vehicle mission equipment mounting structure of claim 1, wherein: the equipment mounting rack (5) comprises two parallel equipment mounting rods (501); the machine body mounting seat (6) comprises two machine body mounting rods (601) which are arranged in parallel; the two equipment mounting rods (501) are respectively detachably connected with the adjacent machine body mounting rods (601).
3. The unmanned aerial vehicle mission equipment mounting structure of claim 2, wherein: the two machine body mounting rods (601) are respectively positioned at the outer sides of the two equipment mounting rods (501), and the adjacent machine body mounting rods (601) and the equipment mounting rods (501) are respectively detachably connected through at least one pin (8) or screw.
4. An unmanned aerial vehicle mission equipment mounting structure as claimed in claim 2 or 3, wherein: the front part of the protective cover (7) is streamline.
5. The unmanned aerial vehicle mission equipment mounting structure of claim 4, wherein: fuselage installation pole (601) are installed in the below of unmanned aerial vehicle body (1) through screw or cementing.
6. The unmanned aerial vehicle mission equipment mounting structure of claim 5, wherein: the equipment switching frame (3) is connected with the task equipment (2) through screws, and the equipment mounting rod (501) and the balancing weight (4) are mounted on the equipment switching frame (3) through screws.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020439398.XU CN212172558U (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle task equipment mounting structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020439398.XU CN212172558U (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle task equipment mounting structure |
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| CN212172558U true CN212172558U (en) | 2020-12-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202020439398.XU Active CN212172558U (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle task equipment mounting structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022141474A1 (en) * | 2020-12-31 | 2022-07-07 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and sensing module |
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2020
- 2020-03-31 CN CN202020439398.XU patent/CN212172558U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022141474A1 (en) * | 2020-12-31 | 2022-07-07 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and sensing module |
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