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Unmanned aerial vehicle hydraulic catapult launching system

A kind of unmanned aerial vehicle and hydraulic technology, which is applied in the direction of launch/drag transmission device, etc., can solve the problems of difficult processing, easy wear and tear of traction rope, and large volume, so as to reduce the pulley speed increaser with large speed ratio and improve quick response ability, and the effect of shortening the response time

Inactive Publication Date: 2015-04-01
SICHUAN AVIATION IND CHUANXI MACHINE
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, it is necessary to design or improve the flow path in the cylinder according to the flow rate flowing into the cylinder, which has disadvantages such as complicated process and difficult processing;
[0008] 2) The speed increaser mostly adopts a pulley speed increaser, which has disadvantages such as complex structure and easy wear of the traction rope;
[0009] 3) Water turbine energy absorbing devices or oil-gas buffer energy absorbing devices are mostly used as buffer energy absorbing devices, which have disadvantages such as difficult design and calculation and large volume

Method used

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  • Unmanned aerial vehicle hydraulic catapult launching system
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  • Unmanned aerial vehicle hydraulic catapult launching system

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Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0024] refer to figure 1 . In the embodiment described below, the UAV hydraulic ejection take-off system includes a hydraulic energy system 29, a launch frame 30, a sliding car 31, a lock release mechanism 32, an electrical control system 33, a carrier platform 34 and a buffer energy-absorbing system, Among them, the hydraulic energy system 29 uses the combination of the accumulator 9 and the hydraulic motor 15 to convert the hydraulic energy into the ejection power of the UAV, and the electrical control system 33 controls the pitching device 26 and the lock release mechanism 32 through the hydraulic energy system 29. The piston rod of the hydraulic cylinder performs telescopic movement, respectively realizing the adjustment of the launching angle of the launching frame 30 and the locking and releasing of the sliding trolley. The ca...

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Abstract

The invention aims to provide an unmanned aerial vehicle hydraulic catapult launching system which is compact in structure and short in response time. A buffer energy-absorption system is integrated in a hydraulic energy system. The technical scheme includes that in the hydraulic energy system, high-pressure hydraulic oil pumped out by a tandem pump group is divided into two paths, one path is connected with an energy accumulator through a hydraulic pipeline, the other path is connected with an oil tank through an electromagnetic overflow valve, the energy accumulator is connected with an oil inlet of a hydraulic motor through the hydraulic pipeline and an inserting valve with an electromagnetic directional valve, a sliding trolley slides in an accelerated manner under the action of power outputted by the hydraulic energy system, an electromagnet 2DT and an electromagnet 3DT are simultaneously powered off after the launching speed of an unmanned aerial vehicle is reached, the inserting valve is closed, the sliding trolley continues to move forwards under the inertia action of the sliding trolley, a traction belt drives the hydraulic motor to rotate reversely, the hydraulic oil is charged to the energy accumulator, kinetic energy of the sliding trolley is consumed, the sliding trolley decelerates to stop, and a buffer energy-absorption function is achieved.

Description

technical field [0001] The invention relates to a hydraulic catapult take-off system for an unmanned aerial vehicle, in particular to a hydraulic energy system integrated with a buffer energy-absorbing system. Background technique [0002] In recent years, with the development of science and technology and military equipment technology, unmanned aerial vehicles are becoming an indispensable weapon in modern high-tech warfare in the military field, and are increasingly equipped with land, sea, and air forces for attack , reconnaissance and other combat missions and target drone training missions. In the civilian field, the application of drones is also increasing, such as: land and resources survey, emergency relief, deep forest fire monitoring, environmental monitoring, etc. [0003] The launch and recovery system is an important functional system of UAVs, and it is a necessary technical guarantee to meet the various needs of UAVs such as flexibility, reusability, and high ...

Claims

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Application Information

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IPC IPC(8): B64F1/06
Inventor 高洪友叶和军严海杨程镭
Owner SICHUAN AVIATION IND CHUANXI MACHINE
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