Landing system for unmanned aerial vehicle recovery

• Main Author: ZHU YINGUANG
• Format: Patent
• Language: Chinese; English
• Published: 07.12.2018
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention discloses a landing system for unmanned aerial vehicle recovery. The landing system includes an unmanned aerial vehicle and a recovery landing system, wherein the unmanned aerial vehicleincludes a rotor wing head, a main shaft and a machine body. Two landing gears are symmetrically arranged at the bottom of the machine body, and the landing gears are slidably inserted at the bottomof the machine body. Buffer rods are arranged on the portion, located in the machine body, of the landing gears, and buffer cavities are formed in the bottom of the machine body. The buffer rods are slidably inserted in the buffer cavities, buffer plates with through holes are arranged on the end portions of the buffer rods, and damping liquid is injected into the buffer cavities. The landing system for the unmanned aerial vehicle recovery includes a parachute bay, a connecting device and a recovery control device, and the parachute bay includes a cabin cover, a parachute pack, a catapult anda base plate. The recovery