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A device and method for unmanned aerial vehicle ejection locking release

A technology for releasing devices and UAVs, which is applied in the direction of launching/dragging transmissions, etc. It can solve the problems of non-reusable use, no buffer function of heavy hammers, and locking UAVs, etc., to achieve fast response, simple use, and adaptability Good results

Active Publication Date: 2021-05-25
AEROSPACE TIMES FEIHONG TECH CO LTD +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The shear pins are cut off after the ejection acceleration phase, losing kinetic energy of the aircraft and cannot be reused, nor can they lock the drone before ejection
The current inertia solution of the heavy hammer has a slow inertia release response, and the heavy hammer itself often has no buffer function during the deceleration section and is easily damaged
The support frame does not have the avoidance function of the ejection path, and has poor adaptability to UAVs with a double tail support structure

Method used

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  • A device and method for unmanned aerial vehicle ejection locking release
  • A device and method for unmanned aerial vehicle ejection locking release
  • A device and method for unmanned aerial vehicle ejection locking release

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Embodiment Construction

[0041] In order to better understand the technical solutions of the present invention, the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0042] It should be clear that the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0043] Terms used in the embodiments of the present invention are only for the purpose of describing specific embodiments, and are not intended to limit the present invention. As used in the embodiments of the present invention and the appended claims, the singular forms "a", "said" and "the" are also intended to include the plural forms unless the context clearly indicates otherwise.

[0044] The locking release device of the UAV inc...

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Abstract

The invention provides a UAV ejection locking release device and method, which relate to the technical field of UAV launch and recovery, and can realize the locking of the UAV on the ejection tackle before ejection and the automatic unlocking of the acceleration section after ejection, and has a support The avoidance function of the frame on the ejection path is reliable in structure and easy to use; the device includes a support frame for fixing the lock release mechanism, and is connected with the support frame tipping device to realize the tipping action of the UAV after ejection; the ejection hook, set In the belly of the UAV, it is used to connect the UAV with the lock release mechanism; the lock release mechanism is used to lock and unlock the UAV by locking and unlocking the ejection hook; the supporting frame down device is used for Install the support frame so that the support frame can realize the down action after the UAV is ejected. The technical scheme provided by the invention is applicable to the process of ejecting the drone.

Description

【Technical field】 [0001] The invention relates to the technical field of unmanned aerial vehicle launch and recovery, and in particular to an unmanned aerial vehicle ejection locking release device and method. 【Background technique】 [0002] Military drones are advanced combat equipment with high technological content. UAVs that use catapults to take off do not need a runway, and can be launched within a length of 10 meters that can be deployed by the catapult. The launch cost is low and the launch time is short. It is especially suitable for the rapid launch of small and medium-sized fixed-wing UAVs. [0003] At present, there are mainly several types of catapults for UAVs, such as pneumatic ejection, motor ejection, and electromagnetic ejection. They are essentially an energy conversion device, which converts the potential energy stored in the catapult or external electrical energy into the take-off of the UAV in a short time. kinetic energy. [0004] Commonly used catap...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 曾鹏陈建国王宣博刘腾达王子龙李博
Owner AEROSPACE TIMES FEIHONG TECH CO LTD
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