Deformable-wing aircraft capable of being landed and recycled

By introducing a moving mechanism, an emergency landing buffer mechanism and an opening mechanism into the deformable flexible deformable wing aircraft, the problems of manual assistance and serious damage to failures in the prior art are solved, and the safe recycling and flexible application of the aircraft are realized.

CN119734836APending Publication Date: 2025-04-01SHANGHAI UNIV OF ENG SCI
1 Cites 0 Cited by

Patent Information

Application Number
CN202411810332.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-12-10
Publication Date
2025-04-01

AI Technical Summary

Technical Problem

The existing deformable flexible deformable wing aircraft require manual assistance during takeoff and landing, and the use scenario is single, and it will cause serious damage and poor protection when the fault lands.

Method used

A landing and recycling deformation wing aircraft is designed, including a base frame, steering mechanism, deformation wing, moving mechanism, impulse landing buffer mechanism and opening mechanism. The vehicle is driven to move through the mobile mechanism, the emergency landing buffer mechanism provides buffering force, and the opening mechanism controls the opening of the parachute, achieving soft landing and safe recycling.

Benefits of technology

It realizes safe landing of the aircraft in emergency situations, reduces damage, extends service life, and improves the flexibility and application scenarios of the aircraft.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

The invention discloses a landing and recycling deformation wing aircraft which comprises a base frame, steering mechanisms are arranged on the front side and the rear side of the base frame, the left side and the right side of the base frame are each provided with a deformation wing, a moving mechanism is arranged on the bottom face of the base frame, and a forced landing buffering mechanism is arranged in each deformation wing. An opening mechanism is further arranged on the rear side of the base frame, the opening mechanism is used for controlling opening of the forced landing parachute so as to provide main buffering force during forced landing, the forced landing buffering mechanism is used for providing auxiliary buffering force during forced landing, and the moving mechanism is used for driving the aircraft to move and buffering impact force generated by forced landing through movement. The opening mechanism is additionally arranged at the tail of the aircraft, the moving mechanism is additionally arranged at the bottom of the aircraft, and the forced landing buffering mechanism is additionally arranged in the deformation wing, so that the aircraft is buffered from the air to the ground to realize soft landing, and safe landing of the aircraft is guaranteed.
Need to check novelty before this filing date? Find Prior Art