An open structure integrated support for unmanned aerial platform

Abstract

The utility model relates to an open structure integrated support for unmanned flight platform belongs to unmanned plane technical field, the utility model discloses: core bearing structure (1), transition structure (2) and shock attenuation module (3), wherein, core bearing structure (1) is designed as the'dustpan'special-shaped structure, provides 7 equipment installation surfaces, shock attenuation module (3) is full position shock absorber, realizes integrated support in unmanned platform bottom, sidewall, top full position installation, transition structure (2) is used for with unmanned platform connection. The utility model can satisfy unmanned flight platform use environment.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) technology and relates to an open-structure integrated support for unmanned flight platforms. Background Technology

[0002] Unmanned aerial platforms are increasingly widely used in numerous fields due to their flexibility, economy, and deployability. However, with the continuous expansion of application scenarios and the increasing complexity and variability of missions, single-function unmanned aerial platforms can no longer meet practical application needs. Therefore, the ability to integrate onboard equipment based on mission diversity has become a core challenge in the design of unmanned aerial platforms.

[0003] In unmanned aerial platforms, the diversity of missions requires the platform to flexibly accommodate equipment with different functions, such as positioning modules, communication modules, information processing modules, and mission payloads. The integration of equipment is not a simple stacking process; this is even more crucial in the operating environment of unmanned aerial platforms. Achieving efficient integration of different types of equipment, improving the platform's scalability, ensuring the usability and versatility of integrated structural components, and enhancing the practicality and lifespan of the unmanned aerial platform are all of paramount importance. Research has revealed that currently common solutions involve integrated layered or frame-type structures.

[0004] Existing solutions have the following characteristics:

[0005] Shelf-type structures consist of multiple layers of parallel-arranged panels secured with screws or other fasteners, and are commonly used in server chassis and similar applications. The modular, vertically stacked form facilitates layered maintenance, but in smaller spaces, height limitations restrict scalability; the panels rely on supporting structures for fixation, resulting in poor vibration or impact resistance; and to compensate for insufficient rigidity, panel thickness or reinforcing ribs may be added, leading to a heavier structure, making it more suitable for static, light-load applications.

[0006] A frame structure uses a three-dimensional frame as the main support, and equipment can be fixed to the frame via brackets to form an integral rigid structure, which is often used in scenarios such as large cabinets. Frame structures have strong resistance to vibration and deformation, and are suitable for heavy loads or dynamic loads, but they themselves require a certain volume and are not suitable for compact designs; moreover, the processing and assembly of customized frames are relatively complex.

[0007] There is currently a gap in meeting the requirements for dynamic, lightweight, and compact design of unmanned aerial platforms.

[0008] This utility model features a core load-bearing structure, a transition structure, and a shock-absorbing module, allowing for multi-faceted equipment mounting and multi-directional wiring to meet the operational environment of unmanned aerial platforms. Its purpose is to achieve lightweight dynamic loads suitable for maneuvering flight. Summary of the Invention

[0009] The purpose of this invention is to provide an open-structure integrated support for unmanned aerial platforms to solve the problems of the heavy weight of layered structures, which are more suitable for static, light loads, and have high complexity in customized frame processing and assembly.

[0010] To solve the above-mentioned technical problems, this utility model provides an open-structure integrated support for unmanned aerial platforms. The integrated support includes a core load-bearing structure (1), a transition structure (2), and a shock-absorbing module (3). The core load-bearing structure (1) is designed as a "basket" irregular structure, providing seven equipment mounting surfaces. The shock-absorbing module (3) is an all-position shock absorber, enabling the integrated support to be installed in all positions on the bottom, side walls, and top of the unmanned platform. The transition structure (2) is used to connect with the unmanned platform.

[0011] This utility model provides an open-structure integrated support for unmanned aerial platforms. The key points and protection points of this utility model are fourfold: First, the open-structure integrated support for unmanned aerial platforms consists of a core load-bearing structure, a transition structure, and a shock-absorbing module; second, the core load-bearing structure has an open, irregular shape, namely a "basket-shaped" form, which can be widened, heightened, lengthened, and other deformable expansions; third, the core load-bearing structure has multi-faceted loading and multi-directional wiring capabilities; and fourth, it features a handle extension for reducing weight. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the overall open-structure integrated bracket of this utility model;

[0013] Figure 2 This is an exploded view of the open-structure integrated support structure of this utility model;

[0014] Figure 3 This is a schematic diagram of the use of the open-structure integrated bracket of this utility model;

[0015] Figure 4 This is a diagram for structural simulation analysis. Detailed Implementation

[0016] To make the objectives, contents, and advantages of this utility model clearer, the specific embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples.

[0017] This utility model discloses an open-structure integrated support for unmanned aerial platforms, including a core load-bearing structure (1), a transition structure (2), and a shock-absorbing module (3). The core load-bearing structure (1) is designed as a "basket" shaped structure, providing seven mounting surfaces for equipment. The shock-absorbing module (3) is an all-position shock absorber, enabling the integrated support to be installed at all positions on the bottom, side walls, and top of the unmanned platform. The transition structure (2) is used for connection with the unmanned platform. This design meets the usage environment requirements of unmanned aerial platforms.

[0018] To achieve the above objectives and improve the carrying capacity of unmanned aerial platforms, this utility model provides the following technical solution: an open-structure integrated support for unmanned aerial platforms, belonging to the field of unmanned aerial vehicle (UAV) supporting mechanical structures. The solution comprehensively considers weight reduction design, vibration reduction design, heat dissipation, and maintenance capabilities. The technical solution of this utility model will be clearly and completely described below with reference to the accompanying drawings.

[0019] like Figure 1 The open-structure integrated support for unmanned aerial platforms includes a core load-bearing structure (1), a transition structure (2), and a shock-absorbing module (3). The core load-bearing structure (1) is connected to the shock-absorbing module (3) below via countersunk screws (4), and the shock-absorbing module (3) is connected to the transition structure (2) below via flat-head screws (5), thus forming an open-structure integrated support.

[0020] like Figure 2 The core load-bearing structure (1) is a "basket-shaped" bracket that can be integrally formed and processed; it has 7 mounting surfaces and can be installed in all directions, including front, back, left and right; the core load-bearing structure (1) is provided with through holes or threaded holes to adapt to various equipment installation methods such as through holes and threaded holes; it can be widened, heightened, lengthened and other expansion deformations.

[0021] Lightening grooves are provided on the left and right sides and bottom surface of the core load-bearing structure (1). The lightening grooves on the left and right sides can be used as handles. Combining the functions of the lightening grooves and handles can achieve multiple effects in one structure and improve the ease of operation.

[0022] The transition structure (2) is a transition plate used to connect with the unmanned platform. A "protruding ear" structure is provided at the front end of the transition structure (2), which is designed to facilitate installation and operation. Multiple bracket mounting holes are provided on the transition structure (2) to facilitate connection with the unmanned platform.

[0023] The shock absorption module (3) is a group of all-position shock absorbers, connecting the core load-bearing structure (1) and the transition structure (2), realizing the function of installing the integrated bracket in all positions on the bottom, side wall, and top of the unmanned platform. Figure 2 As shown, the core load-bearing structure (1) and the transition structure (2) are connected by 6 damping modules (3).

[0024] Figure 3 The diagram shows a specific embodiment of this utility model. The core support structure (1) has four sides on which equipment is fixed, including communication equipment and information processing equipment, which can provide communication channels and information processing capabilities for the unmanned platform, meeting system integration requirements. The equipment fixed on the side of the bracket is a bidirectional aviation plug outlet, and the bracket structure can still be flexibly adapted.

[0025] Figure 4 The diagram shows a structural simulation analysis of an embodiment of this utility model. Multiple sets of symmetrical light-reducing grooves were designed on the basis of an open-structure integrated bracket. Although a large number of new light-reducing grooves were designed, the strength requirements were still met, and the overall design cycle was greatly shortened.

[0026] This utility model belongs to the field of mechanical structures. It designs an open-structure integrated support for unmanned aerial platforms, including a core load-bearing structure (1), a transition structure (2), and a shock-absorbing module (3). The core load-bearing structure (1) is designed as a "basket" shaped structure, which can provide seven equipment mounting surfaces. The shock-absorbing module (3) is an all-position shock absorber, which can realize the integrated support for installation at all positions on the bottom, side walls, and top of the unmanned platform. The transition structure (2) is used to connect with the unmanned platform. It meets the usage environment of the unmanned aerial platform.

[0027] The key points and protection points of this utility model are four: First, it is an open-structure integrated support for unmanned aerial platforms, including a core load-bearing structure, a transition structure and a shock-absorbing module; second, the core load-bearing structure is an open-shaped irregular structure, namely a "basket-shaped" form, which can be widened, heightened and lengthened; third, the core load-bearing structure has the functions of multi-faceted loading and multi-directional wiring; and fourth, it has the function of extending the handle of the light-reducing groove.

[0028] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.

Claims

1. An open-structure integrated support for unmanned aerial platforms, characterized in that, The integrated support includes: a core load-bearing structure (1), a transition structure (2), and a shock-absorbing module (3); wherein, the core load-bearing structure (1) is designed as a "basket" irregular structure, providing 7 equipment mounting surfaces; the shock-absorbing module (3) is an all-position shock absorber, enabling the integrated support to be installed in all positions at the bottom, side walls, and top of the unmanned platform; the transition structure (2) is used to connect with the unmanned platform.

2. The open-structure integrated support for unmanned aerial platforms as described in claim 1, characterized in that, The core load-bearing structure (1) is connected to the damping module (3) below through countersunk screw assembly (4), and the damping module (3) is connected to the transition structure (2) below through flat screw assembly (5), forming an integrated bracket with an open structure.

3. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, The core load-bearing structure (1) is a "basket-shaped" bracket, which is integrally molded and processed; it has 7 mounting surfaces, enabling installation in all directions: forward, backward, left, and right.

4. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, The core load-bearing structure (1) is provided with through holes or threaded holes to adapt to various installation methods.

5. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, Lightening grooves are provided on the left and right sides and the bottom surface of the core load-bearing structure (1), with the lightening grooves on the left and right sides serving as handles.

6. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, The transition structure (2) is a transition plate for connecting with the unmanned platform. A "protruding ear" structure is provided at the front end of the transition structure (2). The design of the "protruding ear" structure facilitates installation and operation.

7. The open-structure integrated support for unmanned aerial platforms as described in claim 6, characterized in that, The transition structure (2) is provided with multiple bracket mounting holes for easy connection with unmanned platforms.

8. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, The shock absorption module (3) is a group of all-position shock absorbers, which connect the core load-bearing structure (1) and the transition structure (2) to realize the function of installing the integrated bracket at all positions on the bottom, side wall and top of the unmanned platform.

9. The open-structure integrated support for unmanned aerial platforms as described in claim 8, characterized in that, The core load-bearing structure (1) and the transition structure (2) are connected by six damping modules (3).

10. The open-structure integrated support for unmanned aerial platforms as described in claim 2, characterized in that, The core support structure (1) has four sides with equipment fixed on them, including communication equipment and information processing equipment, which provide communication channels and information processing capabilities for the unmanned platform and meet the system integration requirements; the equipment fixed on the side of the support is a two-way aviation plug outlet.

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