parachute for drone
An unmanned aerial vehicle and parachute technology, applied in the field of parachutes, can solve the problems of low firm performance, short service life, poor buffering effect, etc., and achieve the effects of high firm performance, long service life and increased service life.
Inactive Publication Date: 2018-12-11
绍兴市上虞宏兴伞业旅游用品有限公司
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Problems solved by technology
[0008] In order to overcome the shortcomings of short service life, poor cushioning effect and low firmness of existing parachutes for unmanned aircraft, the technical problem to be solved by the present invention is to provide a parachute with long service life, good cushioning effect and high firmness. parachutes for drones
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Embodiment 1
[0026] A parachute for unmanned aircraft, such as Figure 1-4 As shown, a parachute part 3 is included, and the left and right sides of the unmanned aircraft 1 are welded symmetrically to the organic wing 2, and the top of the wing 2 is provided with a parachute part 3, and the parachute part 3 includes a pole 4, an electric wheel 5, a first Spring 6, first stay cord 7, second stay cord 8, place plate 9, slide rail 10, second spring 11, slide block 12, support bar 13, umbrella wing 14, hinge part 15, electric reel 16, The third stay cord 17, the fourth stay cord 18 and the baffle plate 19; the left and right sides of the top of the wing 2 are symmetrically welded and connected with a pole 4, and the pole 4 is welded and connected with an electric wheel 5, the electric wheel 5 is rotatable, and the electric wheel 5 is wound with a first stay rope 7 and a second stay rope 8, and the left and right sides of the top of the wing 2 are connected with a first spring 6 by means of a h...
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The invention relates to a parachute and particularly relates to a parachute for an unmanned aerial vehicle. The invention aiming at providing the parachute for the unmanned aerial vehicle, which is long in service life, good in buffering effect and high in firm performance. In order to achieve the aim, the parachute for the unmanned aerial vehicle, provided by the invention, comprises a parachute part; wings are symmetrically welded and connected on left and right sides of the unmanned aerial vehicle; a parachute part is arranged at the top of each wing; the parachute parts comprise supporting rods and the like; the supporting rods are connected with electric wheels in a welding manner; the electric wheels can rotate; a first pull rope and a second pull rope are wound on the electric wheels; and first springs are connected with the left and right sides of the tops of the wings in a hook connection manner. The device provided by the invention has the effects of long service life, good buffering effect and high firm performance; the common parachute for the unmanned aerial vehicle is made of cloth and is easy to scratch; and the device provided by the invention takes a parachute wing as a main buffering mechanism.
Description
technical field [0001] The invention relates to a parachute, in particular to a parachute for an unmanned aircraft. Background technique [0002] Unmanned aerial vehicle, referred to as "unmanned aerial vehicle", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parachute or a block. ...
Claims
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IPC IPC(8): B64D17/80
CPCB64D17/80
Inventor 洪东科
Owner 绍兴市上虞宏兴伞业旅游用品有限公司