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Multi-mode bomb dropping device for aircraft

A bomb-dropping device and multi-mode technology, which is applied in the field of unmanned aerial vehicles, can solve the problems of inability to select and switch the throwing method, only a single throw, and the bomb-dropping device can only throw at the same time. Convenience and the effect of reducing the difficulty of processing and installation

Active Publication Date: 2021-08-13
天津天羿科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of this, the present invention proposes a multi-mode bomb-dropping device for aircraft to solve the problem that most of the existing bomb-dropping devices can only throw at the same time or only a single throw, and cannot select and switch the throwing mode

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  • Multi-mode bomb dropping device for aircraft

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Embodiment Construction

[0040] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0041]In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and thus should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be understood a...

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Abstract

The invention provides a multi-mode bomb dropping device for an aircraft, the multi-mode bomb dropping device for the aircraft comprises a plurality of bomb barrels, a support, opening assemblies and a shifting assembly, the plurality of bomb barrels are installed on the support, the bottom of each bomb barrel is provided with a chassis, the number of the opening assemblies corresponds to the number of the bomb barrels, the plurality of opening assemblies are installed on the support, and the shifting assembly is installed on the support. The shifting assembly of each bullet cylinder is connected with the chassis of the bullet cylinder in a matched mode, the multiple opening assemblies correspond to the shifting assemblies, and the shifting assemblies are installed on the support. According to the multi-mode bomb dropping device for the aircraft, the problems that most of existing bomb dropping devices can only be thrown at the same time or can only be thrown singly, and the throwing modes cannot be selected and switched are solved.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a multi-mode bombing device for an aircraft. Background technique [0002] With the development of UAV technology, the application fields of UAVs are increasingly extended to all walks of life, especially in the fields of military, police and fire multi-rotor UAVs. The current application scenarios of drones include: emergency response, reconnaissance and strike, event security, etc. At present, there are two throwing methods for throwing drones such as shock bombs or tear gas bombs in emergency response. One is to fire the projectile by thermal launch, and the other is to throw the projectile by free fall. The shortcomings of the mode of using pyrotechnics to launch are mainly manifested in the high requirements for operators, which may easily cause accidental injury. Therefore, the current mainstream throwing method is free fall throwing, but the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/06
CPCB64D1/06B64U2101/15
Inventor 王霖徐雷雷王显平贾意弦
Owner 天津天羿科技有限公司
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