Auxiliary vertical take-off and landing method and device for fixed-wing aircraft

• Main Authors: HUANG RUI, ZHANG CHEN, ZHANG JIE, LIU TONG, ZHAO YAN, LI ZEFAN, SHENG HANLIN, LU YIN, GONG DONGSHENG, WANG ZHE, LI JIACHENG
• Format: Patent
• Language: Chinese; English
• Published: 30.04.2021
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention discloses an auxiliary vertical take-off and landing method for a fixed-wing aircraft, and the method comprises the steps: carrying the fixed-wing aircraft to vertically take off at a take-off stage through a rotor aircraft, and enabling the rotor aircraft to be separated from the fixed-wing aircraft after the rotor aircraft takes off to a preset height; and/or in the landing stage, firstly, the rotor craft is used for being in butt joint with the fixed wing craft in the air, and then the rotor craft is used for carrying the fixed wing craft to vertically land. The invention further discloses an auxiliary vertical take-off and landing device for the fixed-wing aircraft. Compared with the prior art, on the premise that the load and flight performance of the fixed-wing aircraft are not reduced and the aerodynamic layout of the fixed-wing aircraft is not changed, the fixed-wing aircraft can take off and land under the condition of no taxiing runway through proper tiny modification. 本发明公开了一种固定翼飞行器辅助