CN219237364U

CN219237364U - Automatic control device that throws of sonde of unmanned aerial vehicle platform

Info

Publication number: CN219237364U
Application number: CN202223602215.XU
Authority: CN
Inventors: 李觐卿; 申军涛; 陈玉达; 崔满元; 徐浩书; 李泽; 金佳宁; 吴强
Original assignee: Beijing Huayun Shangtong Science & Technology Co ltd; Tianjin Huayun Tianyi Special Meteorological Detection Technology Co ltd; Huayun Sounding Beijing Meteorological Technology Corp
Current assignee: Beijing Huayun Shangtong Science & Technology Co ltd; Tianjin Huayun Tianyi Special Meteorological Detection Technology Co ltd; Huayun Sounding Beijing Meteorological Technology Corp
Priority date: 2022-12-30
Filing date: 2022-12-30
Publication date: 2023-06-23
Anticipated expiration: 2032-12-30

Abstract

The utility model provides an automatic throwing control device of a sonde of an unmanned aerial vehicle platform, which comprises a shell, a quick-release module, mounting bins, hoops and a fixed lock, wherein a dismounting assembly is fixedly arranged at the upper end of the shell, the periphery of the dismounting assembly is detachably connected to the unmanned aerial vehicle platform, a plurality of mounting bins are fixedly arranged on the first side of the shell, the mounting bins are mutually parallel, a carrier is arranged in each mounting bin, the periphery of the carrier is fixedly sleeved with the hoops, the periphery of each hoops is detachably connected to one end of one fixed lock, and the other end of the fixed lock is fixedly connected to the first side of the shell. According to the automatic throwing control device for the sonde of the unmanned aerial vehicle platform, after the novel throwing controller is mounted on the unmanned aerial vehicle platform, the novel throwing controller is provided with a multi-path mounting channel, can mount the sonde or other carriers, accurately throws the carriers by responding to a remote control command, and efficiently collects and transmits carrier data in real time.

Description

Automatic control device that throws of sonde of unmanned aerial vehicle platform

Technical Field

The utility model belongs to the field of unmanned aerial vehicles, and particularly relates to an automatic throwing control device of a sonde of an unmanned aerial vehicle platform.

Background

The unmanned aerial vehicle platform can carry specific equipment to realize specific functions. Besides carrying a meteorological sensor for carrying out real-time observation of airborne meteorological elements, the method can also be used for carrying a throwing meteorological detector for realizing the observation of the vertical atmosphere and the ground meteorological environment of special disaster points, and the throwing device carrier throwing switch is started in response to a remote control command for realizing the throwing treatment of a specific place.

Disclosure of Invention

In view of the above, the utility model aims to provide an automatic throwing control device of a sonde of an unmanned aerial vehicle platform, so as to realize throwing operation in a special scene and solve the problem of high energy consumption of a throwing carrier in the prior art when the throwing carrier is fixed.

In order to achieve the above purpose, the technical scheme of the utility model is realized as follows:

the utility model provides a control device is thrown automatically to sonde of unmanned aerial vehicle platform, which comprises an outer shell, quick detach module, the installation storehouse, clamp and fixed lock, shell upper end fixed mounting dismantles the subassembly, dismantle the periphery of subassembly and can dismantle and be connected to unmanned aerial vehicle platform on, a plurality of installation warehouses of first side fixed mounting of shell, and a plurality of installation warehouses each other parallel arrangement, set up a carrier in every installation warehouses, and the periphery of carrier is fixed cup joints a clamp, the periphery of every clamp can be dismantled and be connected to the one end of a fixed lock, the other end fixed connection of fixed lock is to the first side of shell.

Furthermore, a throwing control module and a receiver are respectively arranged in the shell, signals of the receiver and the fixed lock are respectively connected to the throwing control module, a radio frequency antenna is arranged at one end of the receiver, and the radio frequency antenna is located outside the shell.

Further, the fixed lock is an electromagnetic lock of a non-energy type, and the periphery of the clamp is connected to one end of the fixed lock through magnetism.

Further, the installation bin is of an inverted barrel-shaped structure, the inner diameter of the installation bin is larger than the outer diameter of the carrier, and the upper end of the carrier is located in the installation bin.

Further, quick detach subassembly includes the connecting plate that casing and lower extreme set up, the upper end of lower extreme fixed connection to the shell of connecting plate, and one side of casing sets up electric connection contact, and throws control module and pass through electric connection contact signal connection to unmanned aerial vehicle's controller, and the opposite side of casing sets up the buckle, and the casing periphery can be dismantled through the buckle and be connected to unmanned aerial vehicle platform on.

Further, the shell and the buckle are of an injection molding integrated structure.

Further, both side walls of casing are equipped with the slide hole respectively, and a buckle is connected in every slide hole slip, and the one end of casing sets up the key hole, installs the button in the key hole, and every buckle middle part all is equipped with the slot hole, and sets up the slide in the slot hole, and one side of slide is equipped with domatic, and the one end fixed connection of slide is to the one end of button, and the one end installation spring of buckle, the one end fixed connection of spring is inboard to the casing.

Compared with the prior art, the automatic casting control device for the sonde of the unmanned aerial vehicle platform has the following beneficial effects: this novel throwing controller carries on behind unmanned aerial vehicle platform, possesses the multichannel and carries on the passageway, can carry on sonde or other carriers, and through responding to remote control command with the accurate input of carrier to gather transmission carrier data in real time high-efficiently.

Drawings

The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the utility model. In the drawings:

fig. 1 is a schematic structural diagram of an automatic casting control device of a sonde of an unmanned aerial vehicle platform according to an embodiment of the present utility model;

fig. 2 is a schematic front view of an automatic casting control device of a sonde of an unmanned plane platform according to an embodiment of the present utility model;

fig. 3 is a schematic test diagram of an automatic sonde throwing control device of an unmanned aerial vehicle platform according to an embodiment of the present utility model;

FIG. 4 is a schematic structural view of a quick release assembly according to an embodiment of the present utility model;

FIG. 5 is an internal schematic view of a quick release assembly according to an embodiment of the present utility model;

fig. 6 is a schematic structural diagram of a snap-fit and key-press fit according to an embodiment of the present utility model.

Reference numerals illustrate:

1-a radio frequency antenna; 2-a housing; 3-quick release assembly; 31-a housing; 32-connecting plates; 33-a buckle; 34-key; 35-long holes; 36-sliding plate; 4, a mounting bin; 5-clamping hoop; 6-carrier.

Detailed Description

It should be noted that, without conflict, the embodiments of the present utility model and features of the embodiments may be combined with each other.

In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first", "a second", etc. may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.

In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art in a specific case.

The utility model will be described in detail below with reference to the drawings in connection with embodiments.

As shown in fig. 1-6, an automatic control device that throws of sonde of unmanned aerial vehicle platform, including shell 2, quick detach module, installation storehouse 4, clamp 5 and fixed lock, shell 2 upper end fixed mounting dismantles the subassembly, dismantle the periphery of subassembly and dismantle on the unmanned aerial vehicle platform, the first side fixed mounting three installation storehouse 4 of shell 2, and the mutual parallel arrangement of three installation storehouse 4, set up a carrier 6 in every installation storehouse 4, and the periphery of carrier 6 is fixed cup joints a clamp 5, the periphery of every clamp 5 can dismantle the one end of being connected to a fixed lock, the other end fixed connection of fixed lock is to the first side of shell 2, this control device that throws is carried in unmanned aerial vehicle platform back, possess three routes and carry the passageway, can carry sonde or other carriers 6, through responding to the remote control command with carrier 6 accurate throwing, and the transmission carrier 6 data of real-time high-efficient collection.

The device comprises a shell 2, a casting control module, a sonde data receiving and processing module and a receiver, wherein the casting control module, the sonde data receiving and processing module, the receiver and a fixed lock are respectively connected to the casting control module through signals, a radio frequency antenna 1 is arranged at one end of the receiver, the radio frequency antenna 1 is located outside the shell 2, the fixed lock is an electromagnetic lock, the periphery of a clamp 5 is magnetically connected to one end of the fixed lock, the casting control module, the sonde data receiving and processing module and the receiver are in the prior art, the sonde data receiving and processing module can receive real-time data from a carrier 6 through the radio frequency antenna 1 and send the data to the casting control module, and the casting control module can process the sounding data from the sonde data receiving and processing module and process the sounding data into a fixed data format to be uploaded to an unmanned aerial vehicle collector through a communication line of a quick-dismantling assembly 3.

Through installing clamp 5 and throwing controlling means's fixed lock of electromagnetism carrier 6 on carrier 6 fixed part possesses the characteristics of nimble regulation size, consequently can use the sonde as carrier 6 but not limited to, and then can be equipped with different grade type carrier 6 and realize different functions, possess the wide characteristics of range of application, use the unable type electromagnetic lock as fixed lock of electromagnetism carrier 6, do not need the power supply just have stronger magnetic force, can load, throw the carrier 6 of general weight, the short time power on can when throwing is carried out, can adapt to unmanned aerial vehicle power supply capability not enough characteristics. The carrying of the carrier 6 is very simple and convenient, and the throwing control module controls the fixed lock to loosen the connection of the carrier 6 and the clamp 5 by responding to the throwing control command from the communication line of the quick-release assembly 3, so as to control the release of the carrier 6.

The installation bin 4 is of an inverted barrel-shaped structure, the inner diameter of the installation bin 4 is larger than the outer diameter of the carrier 6, the upper end of the carrier 6 is located in the installation bin 4, the design that the carrier 6 head parachute can be contained in the installation bin 4 is considered to be limited in carrying capacity of a general unmanned aerial vehicle platform, the casting control device is simple in structure, light and small, stability of the unmanned aerial vehicle platform flight process cannot be affected, a sonde is used as a typical application of the carrier 6, and environmental elements can be collected in the casting and falling process and uploaded to a sonde receiver in real time.

Through the installation of quick detach subassembly 3, throw controlling means can be simply convenient with unmanned aerial vehicle platform connection, quick detach subassembly 3 includes casing 31 and the connecting plate 32 that the lower extreme set up, the lower extreme fixed connection of connecting plate 32 is to the upper end of shell 2, one side of casing 31 sets up electric connection contact, and throw control module passes through electric connection contact signal connection to unmanned aerial vehicle's controller, the opposite side of casing 31 sets up buckle 33, casing 31 periphery can be dismantled through buckle 33 and be connected to unmanned aerial vehicle platform on.

The shell 31 has various embodiments, one of which is an injection molding integrated structure of the shell 31 and the buckle 33, the other is that, as shown in fig. 4-6, two side walls of the shell 31 are respectively provided with sliding holes, each sliding hole is slidably connected with one buckle 33, one end of the shell 31 is provided with a key hole, a key 34 is installed in the key hole, the middle part of each buckle 33 is provided with a long hole 35, a sliding plate 36 is arranged in the long hole 35, one side of the sliding plate 36 is provided with a slope, one end of the sliding plate 36 is fixedly connected with one end of the key 34, one end of the buckle 33 is provided with a spring, one end of the spring is fixedly connected with the inner side of the shell 31, and the quick-release assembly 3 can be connected with a quick-release base provided by the unmanned aerial vehicle platform in a plug-in manner so as to firmly fix the automatic throwing control device on the unmanned aerial vehicle platform. And after the installation is accomplished, the electric connection contact of quick detach subassembly 3 contacts with unmanned aerial vehicle platform quick detach base, can provide power and communication interface for sonde data reception processing mechanism through quick detach subassembly 3's lead-out wire.

The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the utility model.

Claims

1. Automatic control device that throws of sonde of unmanned aerial vehicle platform, its characterized in that: including shell (2), quick detach module, install bin (4), clamp (5) and fixed lock, the subassembly is dismantled in shell (2) upper end fixed mounting, dismantle the periphery of subassembly and can dismantle on being connected to unmanned aerial vehicle platform, a plurality of install bin (4) of first side fixed mounting of shell (2), and a plurality of install bin (4) are parallel to each other and set up in every install bin (4), and the periphery of carrier (6) is fixed cup joints a clamp (5), the periphery of every clamp (5) can dismantle the one end of being connected to a fixed lock, the other end fixed connection of fixed lock is to the first side of shell (2).

2. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 1, wherein: the inside of the shell (2) is respectively provided with a throwing control module and a receiver, the receiver and the fixed lock are respectively connected to the throwing control module through signals, one end of the receiver is provided with a radio frequency antenna (1), and the radio frequency antenna (1) is positioned outside the shell (2).

3. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 1, wherein: the fixed lock is an incapacitating electromagnetic lock, and the periphery of the clamping hoop (5) is connected to one end of the fixed lock through magnetism.

4. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 1, wherein: the installation bin (4) is of an inverted barrel-shaped structure, the inner diameter of the installation bin (4) is larger than the outer diameter of the carrier (6), and the upper end of the carrier (6) is positioned in the installation bin (4).

5. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 1, wherein: the quick detach subassembly (3) include casing (31) and connecting plate (32) that the lower extreme set up thereof, the lower extreme fixed connection of connecting plate (32) is to the upper end of shell (2), and one side of casing (31) sets up electric connection contact, and throws control module and pass through electric connection contact signal connection to unmanned aerial vehicle's controller, and the opposite side of casing (31) sets up buckle (33), and casing (31) periphery can be dismantled through buckle (33) and be connected to unmanned aerial vehicle platform.

6. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 5, wherein: the shell (31) and the buckle (33) are of an injection molding integrated structure.

7. The automatic sonde casting control device of the unmanned aerial vehicle platform according to claim 5, wherein: the both sides wall of casing (31) is equipped with the slide hole respectively, and a buckle (33) is connected in the slip in every slide hole, and the one end of casing (31) sets up the keyhole, installs button (34) in the keyhole, and every buckle (33) middle part all is equipped with slot hole (35), and sets up slide (36) in slot hole (35), and one side of slide (36) is equipped with the domatic, and the one end fixed connection of slide (36) is to the one end of button (34), and the one end installation spring of buckle (33), the one end fixed connection of spring is inboard to casing (31).