A mechanism for launching drones on airships
A technology for unmanned aerial vehicles and airships, which is applied in the direction of launching/dragging transmissions, rigid spacecraft, etc., which can solve the problems of unmanned aerial vehicles consumption, application scenarios that cannot meet the endurance requirements, etc., and achieve the effect of saving energy consumption
Active Publication Date: 2022-07-08
AEROSPACE SHENZHOU AIRCRAFT
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Problems solved by technology
At present, the launch of UAVs is generally carried out by self-starting flight or ground catapult take-off, but these methods require the UAV to consume its own energy to fly to the required flight altitude and cruising area, which cannot meet the requirements of high endurance requirements. Application Scenario
Method used
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[0017] The present invention will be further described below with reference to the accompanying drawings and specific embodiments. It should be noted that, on the premise of no conflict, the embodiments or technical features described below can be combined arbitrarily to form new embodiments. .
[0018] refer to figure 1 . An embodiment of the present invention provides a mechanism for launching an unmanned aerial vehicle on an airship, which includes a guide rail assembly and a transmission assembly for being installed on the airship, and a force bearing assembly 1 for installing on the unmanned aerial vehicle. The guide rail assembly includes a launcher assembly. The guide rail 2 and the pulley guide rails 3 arranged on both sides of the launching guide rail 2, the force bearing assembly 1 is arranged on the launching guide rail 2 and can move along the launching guide rail 2, and the pulley guide rail 3 is provided with a first movable pulley group 4 and a second movable p...
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The invention discloses a mechanism for launching an unmanned aerial vehicle on an airship. On the pulley guide rails on both sides of the launch guide rail, the force-bearing components are arranged on the launch guide rail and can move along the launch guide rail. The pulley guide rail is provided with a first movable pulley block and a second movable pulley block. The first drum, the first fixed pulley group, the second drum, the second fixed pulley group, the third drum and the third fixed pulley group, the first drum is wound with a front pull rope, and the front pull rope is connected after passing through the first fixed pulley group On the first movable pulley set, the second reel is wound with a rear pulley, which passes through the second fixed pulley and is connected to the second movable pulley. The pulley block, the second movable pulley block and the first movable pulley block are in contact with the force bearing component.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicle launching, in particular to a mechanism for launching an unmanned aerial vehicle on an airship. Background technique [0002] UAVs have developed rapidly both domestically and internationally. Due to their advantages of flexible maneuverability, high timeliness, low cost, strong detection and monitoring capabilities, and wide coverage, they are increasingly used in military and civilian applications. At present, the launch of drones is generally carried out by means of self-starting flight or ground ejection take-off, but these methods require the drone to consume its own energy to fly to the required flight altitude and cruising area, which cannot meet the requirements of high endurance. application scenarios. SUMMARY OF THE INVENTION [0003] In order to overcome the deficiencies of the prior art, the purpose of the present invention is to provide a mechanism for launching an ...
Claims
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IPC IPC(8): B64F1/04B64B1/06
CPCB64F1/04B64B1/06
Inventor 靳美娜李锦清周洪于林友关玉明
Owner AEROSPACE SHENZHOU AIRCRAFT