Unmanned aerial vehicle filling device
By designing the transmission unit and push unit of the drone loading device, the problem of complex and inability to launch quickly is solved, and the rapid and reliable loading and launch of the drone is achieved.
Patent Information
- Application Number
- CN202311453185.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2023-11-03
- Publication Date
- 2025-05-06
- Estimated Expiration
- 2043-11-03
AI Technical Summary
The existing drone loading mechanism has complex workflows and cannot adapt to the needs of rapid launches.
A drone loading device is designed, including a fixed bracket, a conveying unit and a pushing unit. The conveying unit realizes the transmission of the drone to the barrel position through the conveyor belt and the tensioning wheel, and the pushing unit realizes the pushing of the drone to the launch position through the slide and the push drive module.
It realizes reliable transmission and rapid loading and launch of drones, simplifies the loading process, and adapts to the needs of rapid launch.
Smart Images

Figure CN119929220A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV) launching structures, and in particular to a UAV loading device. Background Art
[0002] During the launch of a UAV, a launching device loading mechanism is usually used to transfer the UAV to the launch position. The existing method is to grab the UAV to the launch position through a crank connecting rod grabbing mechanism, or to load the UAV to a designated position by transferring a rotating actuating structure to launch the UAV. However, the existing loading mechanism workflow is relatively complicated and cannot meet the needs of rapid launch. Summary of the invention
[0003] The present invention provides a drone loading device, which can solve the technical problems in the prior art.
[0004] The present invention provides a UAV loading device, wherein the device comprises a fixed bracket, a transmission unit and a pushing unit, wherein the transmission unit is arranged on the fixed bracket and is used to transmit the UAV to the barrel position, and the pushing unit is used to push the UAV to the launching position, the transmission unit comprises a transmission drive module, a tensioning wheel and a conveyor belt, and the conveyor belt cooperates with the tensioning wheel to realize transmission under the action of the driving force of the transmission drive module to transmit the UAV to the barrel position, and the pushing unit comprises a slideway, a pushing drive module, a driving module bracket, a pushing support and a gear rack, the gear rack is arranged between the slideway and the pushing support, the pushing drive module and the driving module bracket are arranged on the pushing support, and the driving module bracket moves along the slideway under the action of the driving force of the pushing drive module to push the UAV to the launching position.
[0005] Preferably, the fixed support may be a multi-layer structure, and the conveying unit and the pushing unit are arranged correspondingly on each layer.
[0006] Preferably, an adapter is provided on the conveyor belt, and the adapter cooperates with a slider on the surface of the drone to fix the drone.
[0007] Preferably, limiting units are provided at both ends of the slideway.
[0008] Preferably, mounting edges are reserved on both sides of the slideway for fixing to the fixing bracket or the transport vehicle by punching or mechanical clamping.
[0009] Preferably, a plurality of mounting seats are arranged at the bottom and around the fixing bracket for mounting the fixing bracket on a launching vehicle or on the ground.
[0010] Preferably, the transmission drive module comprises a drive body, a transmission shaft and a bearing seat.
[0011] Preferably, the driving body is a stepping motor.
[0012] Preferably, the conveyor belt is a chain.
[0013] Preferably, the pushing drive module is a stepping motor.
[0014] Through the above technical solution, the UAV can be first transported to the barrel position by a transmission unit in a transmission movement direction, and then pushed to the launch position (i.e., inside the barrel) by a pushing unit in another pushing movement direction, thereby achieving reliable transmission of the UAV and rapid loading and launching. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] The included drawings are used to provide a further understanding of the embodiments of the present invention, which constitute a part of the specification, are used to illustrate the embodiments of the present invention, and together with the text description, explain the principles of the present invention. Obviously, the drawings in the following description are only some embodiments of the present invention, and for ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.
[0016] Figure 1 A schematic diagram of a drone loading device according to an embodiment of the present invention is shown;
[0017] Figure 2 A schematic diagram of a transmission unit according to an embodiment of the present invention is shown;
[0018] Figure 3 A schematic diagram of a transmission driving module according to an embodiment of the present invention is shown;
[0019] Figure 4 A schematic diagram of an adapter according to an embodiment of the present invention is shown;
[0020] Figure 5 A schematic diagram of a pushing unit according to an embodiment of the present invention is shown. DETAILED DESCRIPTION
[0021] It should be noted that, in the absence of conflict, the embodiments in this application and the features in the embodiments can be combined with each other. The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. The following description of at least one exemplary embodiment is actually only illustrative and is by no means intended to limit the present invention and its application or use. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0022] It should be noted that the terms used herein are only for describing specific embodiments and are not intended to limit the exemplary embodiments according to the present application. As used herein, unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "comprise" and / or "include" are used in this specification, it indicates the presence of features, steps, operations, devices, components and / or combinations thereof.
[0023] Unless otherwise specifically stated, the relative arrangement of the parts and steps described in these embodiments, numerical expressions and numerical values do not limit the scope of the present invention. At the same time, it should be understood that, for ease of description, the sizes of the various parts shown in the accompanying drawings are not drawn according to the actual proportional relationship. The technology, method and equipment known to ordinary technicians in the relevant field may not be discussed in detail, but in appropriate cases, the technology, method and equipment should be regarded as a part of the authorization specification. In all examples shown and discussed here, any specific value should be interpreted as being merely exemplary, rather than as a limitation. Therefore, other examples of exemplary embodiments may have different values. It should be noted that similar reference numerals and letters represent similar items in the following drawings, so once a certain item is defined in an accompanying drawing, it does not need to be further discussed in subsequent drawings.
[0024] Figure 1 A schematic diagram of a drone loading device according to an embodiment of the present invention is shown.
[0025] like Figure 1 , 2As shown in Figure 5, an embodiment of the present invention provides a UAV loading device, wherein the device includes a fixed bracket 1, a transmission unit 2 and a pushing unit 3, wherein the transmission unit 2 is arranged on the fixed bracket 1, and is used to transmit the UAV 4 to the barrel position, and the pushing unit 3 is used to push the UAV 4 to the launching position, and the transmission unit 2 includes a transmission drive module 21, a tension wheel 22 and a conveyor belt 23, and the conveyor belt 23 cooperates with the tension wheel 22 under the driving force of the transmission drive module 21 to realize transmission, so as to transmit the UAV 4 to the barrel position, and the pushing unit 3 is used to push the UAV 4 to the launching position. The delivery unit 3 includes a slide 31, a pushing drive module 32, a drive module bracket 33, a pushing support 34 and a gear rack. The gear rack is arranged between the slide 31 and the pushing support 34, the pushing drive module 32 and the drive module bracket 33 are arranged on the pushing support 34, and the drive module bracket 33 moves along the slide 31 under the action of the driving force of the pushing drive module 32 (the relative movement between the drive module bracket and the slide is realized by the driving force) to push the drone 4 to the launch position (the pushing support pushes the drone to move to the launch position).
[0026] That is, after receiving the transmission instruction, the transmission drive module can drive the conveyor belt to transmit the drone to the front of the barrel. After receiving the transmission instruction, the push drive module can push the drone into the barrel, thereby moving the drone from the storage position to the launch position and completing the launch preparation.
[0027] Through the above technical solution, the UAV can be first transported to the barrel position by a transmission unit in a transmission movement direction, and then pushed to the launch position, i.e., the barrel, by a pushing unit in another pushing movement direction, thereby achieving reliable transmission of the UAV and rapid loading and launching.
[0028] According to an embodiment of the present invention, the fixing bracket 1 may be a multi-layer structure, and the conveying unit 2 and the pushing unit 3 are arranged correspondingly on each layer.
[0029] For example, a conveying unit and a pushing unit are arranged on a layer structure.
[0030] According to an embodiment of the present invention, Figure 4 As shown, an adapter 24 is provided on the conveyor belt 23 , and the adapter 24 cooperates with a slider 41 on the surface of the drone 4 to fix the drone 4 .
[0031] For example, a slide groove may be provided on the adapter, and the UAV may be fixed by cooperating with the slide groove and the slider.
[0032] In this way, the drone can be fixed during the transmission process to ensure stability during transportation.
[0033] According to an embodiment of the present invention, limiting units (eg, mechanical limiting mechanisms) are provided at both ends of the slideway 31 .
[0034] By setting the limit unit, the drone position can be accurately pushed.
[0035] According to an embodiment of the present invention, installation edges are reserved on both sides of the slideway 31 for fixing to the fixing bracket 1 or the transport vehicle by punching or mechanical clamping.
[0036] Thereby, the installation and fixation of the pushing unit 3 can be facilitated.
[0037] According to an embodiment of the present invention, a plurality of mounting seats are arranged at the bottom and around the fixing bracket 1 for mounting the fixing bracket 1 on a launching vehicle or on the ground.
[0038] The specific installation location can be determined according to actual needs, and the present invention is not limited to this.
[0039] According to an embodiment of the present invention, Figure 3 As shown, the transmission driving module 21 includes a driving body 211 , a transmission shaft 212 and a bearing seat 213 .
[0040] Specifically, the driving body is arranged on a transmission shaft, and the transmission shaft passes through a bearing seat.
[0041] According to an embodiment of the present invention, the driving body is a stepping motor.
[0042] According to one embodiment of the present invention, the conveyor belt 23 is a chain.
[0043] For example, the adapter 24 may be provided at a link of a chain.
[0044] According to an embodiment of the present invention, the pushing drive module 32 is a stepping motor.
[0045] In the description of the present invention, it is necessary to understand that the directions or positional relationships indicated by directional words such as "front, back, up, down, left, right", "lateral, vertical, perpendicular, horizontal" and "top, bottom" are usually based on the directions or positional relationships shown in the drawings. They are only for the convenience of describing the present invention and simplifying the description. Unless otherwise specified, these directional words do not indicate or imply that the devices or elements referred to must have a specific direction or be constructed and operated in a specific direction. Therefore, they cannot be understood as limiting the scope of protection of the present invention. The directional words "inside and outside" refer to the inside and outside relative to the contours of each component itself.
[0046] For ease of description, spatially relative terms such as "above", "above", "on the upper surface of", "above", etc. may be used here to describe the spatial positional relationship between a device or feature and other devices or features as shown in the figure. It should be understood that spatially relative terms are intended to include different orientations of the device in use or operation in addition to the orientation described in the figure. For example, if the device in the accompanying drawings is inverted, the device described as "above other devices or structures" or "above other devices or structures" will be positioned as "below other devices or structures" or "below other devices or structures". Thus, the exemplary term "above" can include both "above" and "below". The device can also be positioned in other different ways (rotated 90 degrees or in other orientations), and the spatially relative descriptions used here are interpreted accordingly.
[0047] In addition, it should be noted that the use of terms such as "first" and "second" to limit components is only for the convenience of distinguishing the corresponding components. If not otherwise stated, the above terms have no special meaning and therefore cannot be understood as limiting the scope of protection of the present invention.
[0048] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.
Claims
1. A drone loading device, characterized in that: The device comprises a fixed support (1), a transmission unit (2) and a pushing unit (3); the transmission unit (2) is arranged on the fixed support (1) and is used to transmit a UAV (4) to a barrel position; the pushing unit (3) is used to push the UAV (4) to a launching position; the transmission unit (2) comprises a transmission drive module (21), a tension wheel (22) and a transmission belt (23); the transmission belt (23) cooperates with the tension wheel (22) to achieve transmission under the action of the driving force of the transmission drive module (21) so as to transmit the UAV (4) to the launch position; The pushing unit (3) comprises a slideway (31), a pushing drive module (32), a drive module bracket (33), a pushing support (34) and a gear rack, wherein the gear rack is arranged between the slideway (31) and the pushing support (34), the pushing drive module (32) and the drive module bracket (33) are arranged on the pushing support (34), and the drive module bracket (33) moves along the slideway (31) under the action of the driving force of the pushing drive module (32) to push the UAV (4) to the launching position.
2. The device according to claim 1, characterized in that The fixed support (1) may be a multi-layer structure, with the conveying unit (2) and the pushing unit (3) being arranged correspondingly on each layer.
3. The device according to claim 2, characterized in that An adapter (24) is provided on the conveyor belt (23), and the adapter (24) cooperates with a slider (41) on the surface of the drone (4) to achieve fixation of the drone (4).
4. The device according to claim 3, characterized in that Limiting units are arranged at both ends of the slideway (31).
5. The device according to claim 4, characterized in that The slideway (31) has reserved mounting edges on both sides for fixing to the fixing bracket (1) or the transport vehicle by punching or mechanical clamping.
6. The device according to claim 5, characterized in that A plurality of mounting seats are arranged at the bottom and around the fixing bracket (1) for mounting the fixing bracket (1) on a launching vehicle or on the ground.
7. The device according to any one of claims 1 to 6, characterized in that The transmission drive module (21) comprises a drive body (211), a transmission shaft (212) and a bearing seat (213).
8. The device according to claim 7, characterized in that The driving body is a stepping motor.
9. The device according to any one of claims 1 to 6, characterized in that: The conveyor belt (23) is a chain.
10. The device according to any one of claims 1 to 6, characterized in that The pushing drive module (32) is a stepping motor.
Citation Information
Patent Citations
Automatic circular launching and recovery device of unmanned aerial vehicle
CN108248886A
Device and method for continuous launching of drones
CN109436364A
Repeating unmanned aerial vehicle electromagnetic catapult system and unmanned aerial vehicle hangar
CN112173153A
Medium-sized unmanned aerial vehicle launcher based on energy storage flywheel
CN112937899A
Multimode unmanned aerial vehicle
EP2391863A1