Cluster type launching cabin circumferential bundling structure

Abstract

The utility model relates to a circumferential bundling structure of a cluster type launching cabin, and belongs to the field of unmanned aerial vehicle launching. Comprising a launching cabin base, a launching cabin top surrounding and fixing structure, a flexible body connecting part and an adjustable tensioning and fixing mechanism. Wherein the adjustable tensioning and fixing mechanism is installed on the launching cabin base, the flexible body connecting part is connected with the launching cabin base through the adjustable tensioning and fixing mechanism, and the launching cabin base is connected with the launching cabin top surrounding and fixing structure through at least one flexible body connecting part. The adjustable tensioning and fixing mechanism is mainly used for tensioning and fixing a flexible body connecting part between the launching cabin base and the launching cabin top surrounding and fixing structure. According to the utility model, through the flexible body connecting part and the adjustable tensioning and fixing mechanism, a circumferential binding and connecting structure which can be flexibly adjusted and stably fixed is realized, and a reliable circumferential binding mode is provided on the basis of simplifying the installation process of the cluster type launching box.

Description

Technical Field

[0001] The utility model belongs to the field of unmanned aerial vehicle launch, and in particular relates to a circumferential bundling structure of a clustered launch cabin. Background Art

[0002] Drone swarm technology is a technology that achieves "cooperative networking" by upgrading the control components of drone systems, and coordinates the control of multiple drone systems to form drone swarms. Single reconnaissance and attack units are upgraded to multi-unit collaborative reconnaissance and attack. The drones in the swarm share information and cooperate with each other to achieve collaborative work tasks. During the application process, saturated reconnaissance and attack situations can be formed for multiple types of targets, and huge work efficiency has emerged. Drone swarms can carry out combat tasks such as cluster reconnaissance, omnidirectional saturation attacks, and damage assessments on distributed high-value targets on the ground or at sea under confrontation conditions, achieving full-coverage carpet-style suppression and attacks, especially for clusters in limited areas, dispersed and key parts of large targets.

[0003] The deployment and launching technology of drones is an important part of drone swarm technology. The existing drone deployment technologies published at home and abroad mainly include ground cluster launch, ground autonomous takeoff, and transport or fighter deployment. Among them, in the delivery technology using transport or fighter aircraft, in order to improve the delivery efficiency and increase the number of drones that can be delivered in a single delivery, multiple drone launch cabins will be clustered into a cluster launch cabin, and cluster launch will be achieved by uniformly launching the cluster launch cabins. Among them, the key technology of the cluster launch cabin is to effectively connect and fix multiple launch cabins together in a clustered manner, especially the circumferential fixing technology of the cluster launch cabin. The existing circumferential fixing method of the cluster launch cabin is mainly to achieve circumferential fixation by circumferentially wrapping the skin and surrounding ribs during the manufacturing process of the launch cabin. This method has the problems of high cost, complex installation process, high manufacturing precision requirements for related parts, and difficulty in effectively adjusting the preload force of the bundling structure.

[0004] Therefore, there is an urgent need for a circumferential bundling structure or method for a clustered launch module to solve the above-mentioned problems. Utility Model Content

[0005] 1. Technical issues to be resolved

[0006] The technical problem to be solved by the utility model is to provide a circumferential bundling structure for a clustered launch module to solve the problems of high cost and complicated installation process of the existing fixing method, high manufacturing precision requirements for related parts, and difficulty in effectively adjusting the pre-tightening force of the bundling structure.

[0007] (II) Technical solution

[0008] In order to solve the above technical problems, the utility model provides a clustered launch module circumferential bundling structure, comprising: a launch module base 4, a surrounding fixing structure 1 on the top of the launch module, a flexible body connecting component 3 and an adjustable tightening fixing mechanism 5;

[0009] The adjustable tensioning and fixing mechanism 5 is fixed on the launch module base 4, the flexible body connecting component 3 is connected to the launch module base 4 through the adjustable tensioning and fixing mechanism 5, and the launch module base 4 and the surrounding fixed structure 1 on the top of the launch module are connected to each other through at least one flexible body connecting component 3, and the adjustable tensioning and fixing mechanism 5 is used to tighten and fix the flexible body connecting component 3 between the launch module base 4 and the surrounding fixed structure 1 on the top of the launch module.

[0010] The launch cabin top is provided with two surrounding fixed structures 1, two flexible body connecting components 3, and two adjustable fixing mechanisms 5;

[0011] The two flexible connecting parts 3 are connected to the two adjustable fixing mechanisms 5 respectively, and the two launch cabin top surrounding fixing structures 1 are fixedly connected to the launch cabin base through the flexible connecting parts 3 and the adjustable fixing mechanisms 5 respectively.

[0012] The adjustable tightening and fixing mechanism 5 comprises: a flexible connecting component tightening pin 6 and a fixing block 7;

[0013] The tightening pin 6 of the flexible connecting component is used to tighten the flexible connecting component 3 between the launch cabin base 4 and the surrounding fixed structure 1 on the top of the launch cabin;

[0014] The fixing block 7 is fixed to the launch cabin base 4 by bolts, and the tightening pin 6 of the flexible body connecting component is fixed after being tightened.

[0015] The flexible connecting component 3 is connected and fixed to the surrounding fixed structure 1 on the top of the launch cabin through a set of bolts and nuts 2.

[0016] The flexible connecting component 3 and the flexible connecting component tightening pin 6 are connected and fixed by a screw 8 .

[0017] The launch module base 4 is fixedly connected to the cluster launch module by gluing.

[0018] The surrounding fixing structure 1 on the top of the launch module is provided with threaded fixing holes, and the surrounding fixing structure 1 on the top of the launch module is fixedly connected to the relevant structure on the top of the cluster launch module by screws.

[0019] The installation quantity of the launch cabin top surrounding fixed structure 1, the flexible body connecting component 3, the launch cabin base 4 and the adjustable fixing mechanism 5 is set to be adjustable according to the shape of the actual bundled cluster launch box.

[0020] (III) Beneficial effects

[0021] Compared with the prior art, the utility model has the following beneficial effects:

[0022] 1) The cluster launch module is circumferentially tied and fixed by a flexible connecting component and an adjustable tightening and fixing mechanism, which can effectively realize the circumferential bundling and fixing of a cluster launch module composed of multiple launch modules on the basis of ensuring a reasonable installation process of the cluster launch module;

[0023] 2) By arranging a fixed block on the adjustable tensioning and fixing mechanism, the effective bundling of the circumferential bundling structure of the cluster launch module is ensured on the basis of realizing flexible and adaptable circumferential fixed pre-tightening force;

[0024] 3) The installation process of the circumferential bundling structure is simplified through the modular design of the bundling structure, and an efficient and high-quality circumferential bundling method for the cluster launch cabin is obtained. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 This is a schematic diagram of the installation structure of the utility model;

[0026] Figure 2 This is a schematic diagram of the installation of the adjustable tensioning and fixing mechanism of the utility model;

[0027] Figure 3 It is a structural schematic diagram of the adjustable tensioning and fixing mechanism of the utility model. DETAILED DESCRIPTION

[0028] In order to make the purpose, content, and advantages of the utility model clearer, the specific implementation methods of the utility model are further described in detail below in conjunction with the drawings and embodiments.

[0029] This embodiment combines Figure 1-Figure 3 The utility model describes the circumferential bundling structure of the cluster launch module provided by the utility model.

[0030] like Figure 1 As shown, Figure 1The schematic diagram of the installation structure of the clustered launch module circumferential bundling structure of the utility model is shown. The clustered launch module circumferential bundling structure provided by the utility model comprises: a launch module base 4, a launch module top surrounding fixed structure 1, a flexible body connecting component 3 and an adjustable tightening and fixing mechanism 5; the adjustable tightening and fixing mechanism 5 is installed on the launch module base 4, the flexible body connecting component 3 is connected to the launch module base 4 through the adjustable tightening and fixing mechanism 5, and the launch module base 4 and the launch module top surrounding fixed structure 1 are connected to each other through at least one flexible body connecting component 3, and the adjustable tightening and fixing mechanism 5 is mainly used to tighten and fix the flexible body connecting component 3 between the launch module base 4 and the launch module top surrounding fixed structure 1. Specifically, in the present embodiment, two launch module top surrounding fixed structures 1, two flexible body connecting components 3, one launch module base 4 and two adjustable fixing mechanisms 5 are included, the two flexible body connecting components 3 are respectively connected to the two adjustable fixing mechanisms 5, and the two launch module top surrounding fixed structures 1 are respectively fixedly connected to the launch module base through the flexible body connecting components 3 and the adjustable fixing mechanisms 5. In some embodiments, the number of the fixed structure 1 surrounding the top of the launch cabin, the flexible connecting component 3, the launch cabin base 4 and the adjustable fixing mechanism 5 can be adjusted according to the actual shape of the bundled cluster launch box.

[0031] like Figure 2 and Figure 3 As shown, Figure 2 This is a schematic diagram of the installation of the adjustable tensioning and fixing mechanism of the circumferential bundling structure of the cluster launch module. Figure 3 The schematic diagram of the structure of the adjustable tensioning and fixing mechanism in the circumferential bundling structure of the cluster launch module is shown in FIG. The adjustable tensioning and fixing mechanism 5 includes a flexible body connection component tightening pin 6 and a fixed block 7, wherein the flexible body connection component tightening pin 6 is mainly used to tighten the flexible body connection component 3 between the launch module base 4 and the launch module top surrounding fixed structure 1, and the fixed block 7 is mainly used to fix the tightened flexible body connection component tightening pin 6. Specifically, in the application process, the launch module top surrounding fixed structure 1 and the launch module base 4 are respectively installed on the top and bottom of the cluster launch module, and then the flexible body connection component 3 is connected between the launch module top surrounding fixed structure 1 and the launch module base 4, and the flexible body connection component 3 is installed in the flexible body connection component tightening pin 6 in the adjustable tensioning and fixing mechanism 5, and the flexible body connection component tightening pin 6 is tightened to achieve reliable fixation between the flexible body connection component 3 and the launch module top surrounding fixed structure 1 and the launch module base 4. After tightening, the state is locked by installing the fixed block 7 on the flexible body connection component tightening pin 6 to ensure its connection performance.

[0032] Specifically, the flexible body connection component 3 is connected and fixed to the surrounding fixed structure 1 on the top of the launch cabin by at least one set of bolts and nuts 2.

[0033] Specifically, the flexible connecting component 3 and the adjustable tightening and fixing mechanism 5 are connected and fixed by at least one screw 8 .

[0034] Specifically, the fixing block 7 in the adjustable tensioning and fixing mechanism 5 is fixed to the launch cabin base 4 by bolts.

[0035] Specifically, the launch module base 4 and the cluster launch module are fixedly connected by gluing.

[0036] Specifically, threaded fixing holes are provided on the surrounding fixing structure 1 on the top of the launch module, and the surrounding fixing structure 1 on the top of the launch module is fixedly connected to the relevant structure on the top of the cluster launch module by screws.

[0037] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the technical principles of the present invention. These improvements and modifications should also be regarded as the protection scope of the present invention.

Claims

1. A circumferential bundling structure of a clustered launch module, characterized in that: include: A launch cabin base (4), a surrounding fixed structure (1) on the top of the launch cabin, a flexible body connecting component (3) and an adjustable tightening and fixing mechanism (5); The adjustable tensioning and fixing mechanism (5) is fixed on the launch cabin base (4), the flexible body connection component (3) is connected to the launch cabin base (4) via the adjustable tensioning and fixing mechanism (5), and the launch cabin base (4) and the surrounding fixed structure (1) on the top of the launch cabin are connected to each other via at least one flexible body connection component (3), and the adjustable tensioning and fixing mechanism (5) is used to tension and fix the flexible body connection component (3) between the launch cabin base (4) and the surrounding fixed structure (1) on the top of the launch cabin.

2. The circumferential bundling structure of the clustered launch module according to claim 1 is characterized in that: The launch cabin top surrounding fixed structures (1) are provided with two in total, the flexible body connecting components (3) are provided with two in total, and the adjustable tightening and fixing mechanisms (5) are provided with two in total; The two flexible body connection parts (3) are respectively connected to the two adjustable tensioning and fixing mechanisms (5), and the two launch cabin top surrounding fixed structures (1) are respectively fixedly connected to the launch cabin base via the flexible body connection parts (3) and the adjustable tensioning and fixing mechanisms (5).

3. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The adjustable tensioning and fixing mechanism (5) comprises: a flexible connecting component tightening pin (6) and a fixing block (7); The flexible body connecting component tightening pin (6) is used to tighten the flexible body connecting component (3) between the launch cabin base (4) and the surrounding fixed structure (1) on the top of the launch cabin; The fixed clamping block (7) is fixed to the launch cabin base (4) by bolts, and the tightening pin (6) of the flexible body connecting component is fixed after being tightened.

4. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The flexible body connection component (3) is connected and fixed to the surrounding fixed structure (1) on the top of the launch cabin via a set of bolts and nuts (2).

5. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The flexible body connecting component (3) and the flexible body connecting component tightening pin (6) are connected and fixed by means of a screw (8).

6. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The launch module base (4) is fixedly connected to the cluster launch module by gluing and bonding.

7. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The surrounding fixing structure (1) on the top of the launch cabin is provided with threaded fixing holes, and the surrounding fixing structure (1) on the top of the launch cabin is fixedly connected to the relevant structure on the top of the cluster launch cabin by means of screws.

8. The circumferential bundling structure of the clustered launch module according to claim 1, characterized in that: The installation quantity of the launch cabin top surrounding fixed structure (1), the flexible body connecting component (3), the launch cabin base (4) and the adjustable tensioning and fixing mechanism (5) is set to be adjustable according to the shape of the actual bundled cluster launch box.

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