CN217778989U - Cluster unmanned aerial vehicle transportation emitter - Google Patents
Cluster unmanned aerial vehicle transportation emitter Download PDFInfo
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- CN217778989U CN217778989U CN202122137321.4U CN202122137321U CN217778989U CN 217778989 U CN217778989 U CN 217778989U CN 202122137321 U CN202122137321 U CN 202122137321U CN 217778989 U CN217778989 U CN 217778989U
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses a cluster unmanned aerial vehicle transportation emitter belongs to unmanned air vehicle technical field. The method comprises the following steps: the top of the base is provided with an angle adjusting piece; the mounting part is hinged to the angle adjusting part; at least two groups of emission parts fixed on one side of the installation part in parallel; the angle adjusting piece is used for adjusting the inclination angle of the transmitting part and positioning. The utility model discloses well launching site bears multiunit unmanned aerial vehicle to transport unmanned aerial vehicle to the launching point, unmanned aerial vehicle takes off from the direct transmission of launching site, has realized cluster unmanned aerial vehicle transportation, has arranged and takes off the integration, has the advantage such as arrange fast, take off rapidly, has solved transportation security, take off the place restriction scheduling problem betterly simultaneously.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to cluster unmanned aerial vehicle transports emitter.
Background
With the technological progress, the national defense requirements and other user requirements are higher and higher, and hundreds of times of application and related launching technologies of the cluster type unmanned aerial vehicle need to be researched urgently. The cluster unmanned aerial vehicle application and the related launching technology can be applied to large-scale propaganda and performance, cluster industrial application operation and even a combat armed system.
When many unmanned aerial vehicle take off among the prior art, generally earlier on spacious place, arrange full unmanned aerial vehicle, restart unmanned aerial vehicle. This mode is limited to the spacious condition in place, just can satisfy the transmission demand of cluster type unmanned aerial vehicle, but when narrow place, this mode just is not suitable for.
SUMMERY OF THE UTILITY MODEL
Utility model purpose: in order to solve the problem, the utility model provides a cluster unmanned aerial vehicle transports emitter.
The technical scheme is as follows: a cluster unmanned aerial vehicle transports emitter for arranging and transporting or launching a plurality of unmanned aerial vehicles in the form of a cluster, includes: the top of the base is provided with an angle adjusting piece; an installation part hinged to the angle adjusting part; at least two groups of emission parts fixed on one side of the installation part in parallel; the angle adjusting piece is used for adjusting the inclination angle of the transmitting part and positioning.
In a further embodiment, each unmanned aerial vehicle is provided with a sleeve joint part matched with the launching part, and the sleeve joint parts are used for stably arranging the unmanned aerial vehicles on the launching parts according to a preset sequence.
Through adopting above-mentioned technical scheme, realize that unmanned aerial vehicle can stably arrange on the transmission portion according to predetermined order when the transportation or before the transmission, remain stable.
In a further embodiment, the emitting portion is a slide rail of a predetermined length.
Through adopting above-mentioned technical scheme, increase unmanned aerial vehicle's bearing capacity.
In a further embodiment, the socket joint portion is two sets of linear bearings which are pre-installed on the unmanned aerial vehicle body, and the linear bearings are matched with the transmitting portion.
Through adopting above-mentioned technical scheme, realize that unmanned aerial vehicle keeps balance on the transmission portion steadily.
In a further embodiment, the slide rail is a stainless steel guide rail, and a reinforcing strip is arranged on the outer side of the slide rail.
By adopting the technical scheme, the slide rail has high rigidity and good parallelism and straightness, and the reinforcing strips further increase the rigidity of the slide rail; the slide rail is under the gravity condition that bears multiunit unmanned aerial vehicle, and non-deformable is favorable to unmanned aerial vehicle smooth and easy slip to take off.
In a further embodiment, the mounting portion is a solid structure and the mounting portion is a nylon material.
Through adopting above-mentioned technical scheme, installation department insulating nature and toughness are good, avoid human static to influence the unmanned aerial vehicle on the slide rail to take off, and the installation department adopts solid construction simultaneously for balanced multiunit unmanned aerial vehicle's gravity is convenient for control unmanned aerial vehicle's transmission position on the slide rail.
In a further embodiment, the mounting portion is further provided with a holding portion.
Through adopting above-mentioned technical scheme, supplementary installation department angle regulation.
Has the advantages that: the launching part bears multiple groups of unmanned aerial vehicles, the unmanned aerial vehicles are transported to a launching point, the unmanned aerial vehicles take off from the launching part through direct launching, the integrated transportation, deployment and take-off of the cluster unmanned aerial vehicles are realized, and the unmanned aerial vehicles have the advantages of being rapid in deployment, taking off rapidly and the like, and simultaneously solve the problems of transportation safety, take-off site limitation and the like well.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a plan view of the present invention.
In fig. 1 to 2, each reference is: base 1, angle adjusting part 2, the portion of gripping 3, installation department 4, transmission portion 5, unmanned aerial vehicle 6.
Detailed Description
In order to solve the problems in the prior art, the applicant has conducted in-depth analysis on various existing schemes, which are specifically as follows:
when many unmanned aerial vehicles take off among the prior art, generally arrange unmanned aerial vehicle full in spacious place earlier, restart unmanned aerial vehicle. This mode is limited to the place spaciously, just can satisfy the unmanned aerial vehicle's of cluster type transmission demand, but when constrictive place, this mode is just not applicable. And this mode is when transportation and transmission at cluster unmanned aerial vehicle, and transportation and transmission are gone on respectively, transport many unmanned aerial vehicles to the place earlier promptly, arrange many unmanned aerial vehicles again in the specific position in place, prepare the transmission. This mode is to many unmanned aerial vehicle transmission demands, and is efficient slow, with high costs.
For this purpose, the applicant proposes a solution, as shown in fig. 1 to 2, which provides a cluster drone transport launcher comprising a base 1, an angle adjusting piece 2, a mounting portion 4 and at least two sets of launching portions 5. The angle adjusting piece 2 is arranged at the top end of the base 1, and the mounting part 4 is hinged with the angle adjusting piece 2. The emission parts 5 are arranged on one side surface of the mounting part 4 in parallel, and the emission parts 5 are detachably connected with the mounting part 4; emission portion 5 is predetermined length's slide rail, adopts two sets of emission portions in this embodiment, and emission portion 5 is used for bearing and transporting emission multiunit unmanned aerial vehicle 6.
Under some working conditions, the launching of the surrounding environment is not ideal, for example, the launching site is not on a flat open ground, the surrounding environment has rocks or plants with different heights, in order to launch smoothly, the original launching height of the unmanned aerial vehicle 6 is required to be higher than the height of obstacles in the environment, in order that the base 1 comprises a mounting seat and three groups of telescopic rods (or three groups of supporting legs), the upper ends of the three groups of telescopic rods are mounted on the bottom surface of the mounting seat through connecting pins or other common movable connection modes, the three groups of telescopic rods comprise two states, when the unmanned aerial vehicle is not used, the three groups of telescopic rods are stored together, and when the unmanned aerial vehicle is used, the three groups of telescopic rods are unfolded; the one end that the telescopic link contacted ground has scalability for realize base 1's altitude mixture control, and connect through telescopic link between three telescopic links of group, base 1 adopts triangle independent structure, be convenient for can steadily support installation department 4 under various terrain conditions, unmanned aerial vehicle 6 on launching part 5 and the launching part 5, base 1 has high multistage linear adjustable mode, each support leg length of adjustment according to on-the-spot site conditions is used for guaranteeing that whole transmitting system is stable, especially guarantee the balance of installation department 4. Angle adjusting part 2 includes spacing seat, spacing seat has hollow structure, spacing seat demountable installation is on the top surface of mount pad, be provided with the universal joint ball in the spacing seat, the embedding of universal joint ball is in the hollow structure of spacing seat, the size of universal joint ball slightly littleer and hollow structure's size, guarantee that the universal joint ball can be at spacing internal rotation of seat, angle regulation, install spacing bolt in spacing outside the seat, rotate when the universal joint ball and adjust to predetermined angle, screw up spacing bolt, fixed universal joint ball, angle adjusting part 2 is used for realizing adjusting 5 inclinations of launching part and realizing the location. The base 1 and the angle adjusting member 2 may also be constructed as described in the prior art as model WF/Weifeng WT-3520 for achieving the corresponding effects, and the detailed construction thereof is not repeated herein.
In further embodiment, all be provided with the portion of cup jointing with launching part adaptation on every unmanned aerial vehicle, cup joint the portion and be used for steadily arranging unmanned aerial vehicle on launching part according to predetermined order. The portion of cup jointing is two sets of linear bearing of preinstallation at the unmanned aerial vehicle fuselage, and linear bearing is with launching looks adaptation.
Before taking off, a plurality of groups of unmanned aerial vehicles 6 are sleeved on the launching part 5, and the plurality of groups of unmanned aerial vehicles 6 are transported to the launching point at the same time; during takeoff, the installation part 4 and the emission part 5 form a preset angle with the horizontal plane, and takeoff of the multiple groups of unmanned aerial vehicles 6 in a preset direction is realized.
One of them effect of transmission portion 5 is used for bearing multiunit unmanned aerial vehicle 6, because multiunit unmanned aerial vehicle 6 has self gravity, if the structure of transmission portion 5 is not enough to support multiunit unmanned aerial vehicle 6's gravity, transmission portion 5 will warp, influences the smoothness nature of the 6 transmission takeoffs of unmanned aerial vehicle, and under some operating modes, unmanned aerial vehicle 6 can drop from transmission portion 5 because transmission portion 5 warp, leads to the 6 damages of unmanned aerial vehicle. In order to solve the problem, the following technical scheme is proposed:
in a further embodiment, the slide rail is a stainless steel guide rail, and a reinforcing strip is arranged on the outer side of the slide rail. The slide rail adopts the stainless steel guide rail, and the slide rail rigidity is high, and depth of parallelism and straightness accuracy are good, and the rigidity of slide rail is further increased to the enhancement strip. The slide rail is under the gravity condition that bears multiunit unmanned aerial vehicle 6, and non-deformable is favorable to unmanned aerial vehicle 6's smooth and easy slip to take off.
In a further embodiment, the mounting portion 4 is a solid structure and the mounting portion 4 is a nylon material. Installation department 4 adopts the nylon materials processing to make, and insulating nature and toughness are good, avoid human static to influence unmanned aerial vehicle 6 on the slide rail to take off, and installation department 4 adopts solid construction simultaneously for balanced multiunit unmanned aerial vehicle 6's gravity is convenient for control on the slide rail unmanned aerial vehicle 6's transmission position.
Still be equipped with the portion of gripping 3 on installation department 4 in further embodiment, the portion of gripping 3 is the handle of fixed mounting in installation department 4 both sides for realize the supplementary transmission position of adjusting unmanned aerial vehicle 6 on transmission portion 5.
The working principle is as follows:
during transportation, a plurality of groups of unmanned aerial vehicles 6 are sleeved on the launching part 5, and the installation part 4, the launching part 5 and the plurality of groups of unmanned aerial vehicles 6 are transported integrally; after reaching the launching site, unfolding the base 1 and connecting the base with the installation part 4 through the angle adjusting part 2; the angle of installation department 4 is adjusted to angle adjustment spare 2, realizes that unmanned aerial vehicle 6 prepares to take off with predetermined angle, controls 6 launches of unmanned aerial vehicle through the control cabinet and takes off, realizes that unmanned aerial vehicle 6 gets into the airline fast or directly attacks short distance target.
The preferred embodiments of the present invention have been described in detail with reference to the accompanying drawings, however, the present invention is not limited to the details of the above embodiments, and the technical idea of the present invention is that the technical solution of the present invention is subjected to various equivalent transformations, which all belong to the protection scope of the present invention.
Claims (7)
1. A cluster unmanned aerial vehicle transports emitter for arrange and transport or launch a plurality of unmanned aerial vehicle in the form of cluster, include:
the top of the base is provided with an angle adjusting piece;
an installation part hinged to the angle adjusting part;
at least two groups of emission parts fixed on one side of the installation part in parallel; the angle adjusting piece is used for adjusting the inclination angle of the transmitting part and positioning.
2. A cluster unmanned aerial vehicle transports emitter of claim 1, characterized in that:
each unmanned aerial vehicle is provided with a sleeve joint part matched with the launching part, and the sleeve joint parts are used for stably arranging the unmanned aerial vehicles on the launching parts according to a preset sequence.
3. The cluster unmanned aerial vehicle transportation launcher of claim 1, wherein:
the transmitting part is a slide rail with a preset length.
4. The cluster unmanned aerial vehicle transportation launcher of claim 2, wherein:
the socket joint portion is two sets of linear bearings installed in advance on the unmanned aerial vehicle fuselage, linear bearing with emission portion looks adaptation.
5. The cluster unmanned aerial vehicle transportation launcher of claim 3, wherein:
the slide rail is a stainless steel guide rail, and a reinforcing strip is installed on the outer side of the slide rail.
6. The cluster unmanned aerial vehicle transportation launcher of claim 1, wherein:
the installation department is solid construction just the installation department is the nylon materials.
7. The cluster unmanned aerial vehicle transportation launcher of claim 1, wherein:
the installation part is also provided with a holding part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122137321.4U CN217778989U (en) | 2021-09-06 | 2021-09-06 | Cluster unmanned aerial vehicle transportation emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122137321.4U CN217778989U (en) | 2021-09-06 | 2021-09-06 | Cluster unmanned aerial vehicle transportation emitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217778989U true CN217778989U (en) | 2022-11-11 |
Family
ID=83903811
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122137321.4U Active CN217778989U (en) | 2021-09-06 | 2021-09-06 | Cluster unmanned aerial vehicle transportation emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217778989U (en) |
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2021
- 2021-09-06 CN CN202122137321.4U patent/CN217778989U/en active Active
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