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CN-121986054-A - Aircraft carrier convenient for taking off and landing of aircraft

CN121986054ACN 121986054 ACN121986054 ACN 121986054ACN-121986054-A

Abstract

The invention relates to an aircraft carrier convenient for taking off and landing of an aircraft, which comprises a main body and a buffer part, wherein a landing plate which is retracted and extended through elasticity is combined on the main body, so that the impact force is buffered through elasticity when the aircraft lands on the landing plate. Through this structure, combine the landing board through elasticity is withdrawed and is stretched out in the main part for effectively buffering the impact force when aircraft landed, not only can ensure steady landing, can also show the improvement organism durability.

Inventors

  • Li Xiangmo

Assignees

  • 李相默

Dates

Publication Date
20260505
Application Date
20241010
Priority Date
20231017

Claims (5)

  1. 1. An aircraft carrier for facilitating the landing of an aircraft, as an aircraft carrier, comprising: A main body, and And a buffer part coupled with a landing plate retracted and extended by elasticity on the upper surface of the main body, so that an impact force is buffered by elasticity when the aircraft lands on the landing plate.
  2. 2. An aircraft carrier for facilitating the landing of an aircraft according to claim 1, At the buffer portion, the lower end of the landing plate is coupled with a first elastic body, A double-layer plate is combined at the lower end of the first elastic body, A second elastomer is bonded to the lower end of the double-layer plate.
  3. 3. The aircraft carrier for facilitating aircraft landing of claim 1, further comprising: and a locking part which is arranged in the main body, fixes the position of the landing plate when the landing plate moves downwards, and enables the landing plate to lift upwards through elasticity when the landing plate is released from the locking part.
  4. 4. An aircraft carrier for facilitating the landing of an aircraft according to claim 1, A guide is retractably and retractably incorporated on the upper surface of the body so that when the guide is extended, it is used to guide an aircraft to be landed on the landing plate or when the guide is retracted, it is used to enable the aircraft to glide on a runway.
  5. 5. An aircraft carrier for facilitating the landing of an aircraft according to claim 4, The guide part includes: a support frame coupled to the upper surface of the main body in a retractable and extendable manner and disposed at a prescribed interval along the circumference of the landing plate, and The guide plate is rotatably combined with the upper end of the support frame and can be unfolded towards the inner side of the landing plate or stacked on the support frame.

Description

Aircraft carrier convenient for taking off and landing of aircraft Technical Field The present invention relates to an aircraft carrier facilitating the landing of an aircraft, and more particularly, to an aircraft carrier facilitating the landing of an aircraft capable of achieving the landing of an aircraft that is vertically landing as an unmanned plane at sea. Background The aircraft carrier is a ship capable of carrying and lifting an aircraft. In short, reference is made to a warship dedicated to the operation of an aircraft, unlike a conventional main force warship. If an aircraft carrier is owned, a conventional weapon can strike a large portion of the earth. This is because 70% of the earth is ocean, almost all sea areas are interconnected and can be co-located with each other, while civilization development requires a large amount of water resources, so most populated areas and industrial facilities are concentrated in areas within 300Km from the coastline. It follows that, since the modern sea warfare tactics is based on aircraft, the aircraft carrier is not only the core weapon of the modern sea warfare, but also the naval vessel used by the army of the 21 st century in the modern warfare. Korean aircraft carriers of korean naval forces must insert and place a wheel block on the wheels of the body when the carrier aircraft lands, moves or temporarily berths. In recent years, aircraft carriers have been equipped with unmanned aerial vehicles in addition to carrier-based aircraft. However, although an unmanned aerial vehicle mounted on an aircraft carrier has a vertical take-off and landing capability, the unmanned aerial vehicle is sensitive to sea wind, and is easily rolled up by the sea wind to collide with a carrier body in the take-off and landing process, so that the problem of frequent accidents is caused. The prior art documents in the technical field of the present invention include korean registered patent publication No. 10-2469043, korean registered patent publication No. 10-2523650, korean patent laid-open No. 10-2022-0161099, and the like. Disclosure of Invention Technical problem to be solved The present invention has been made in view of the above-described problems, and an object of the present invention is to provide a landing device that can smoothly land in a sea environment, and that can buffer impact at landing and realize fixed-point landing, by making a vertical landing aircraft such as an unmanned aerial vehicle landing from an aircraft carrier. Technical proposal In order to achieve the object, the aircraft carrier which facilitates the landing of the aircraft, provided by the invention, is used as the aircraft carrier, and comprises a main body and a buffer part, wherein a landing plate which is retracted and extended through elasticity is combined on the main body, so that the impact force is buffered through elasticity when the aircraft lands on the landing plate. In addition, in the buffer part, the lower end of the landing plate is coupled with a first elastic body, a double-layered plate is coupled to the lower end of the first elastic body, and a second elastic body is coupled to the lower end of the double-layered plate. Further, a locking part is provided inside the main body, fixes the position of the landing plate when the landing plate moves downward, and lifts the landing plate upward by elasticity when the landing plate is released. Furthermore, a guide is retractably and extendably incorporated on the upper side of the main body so that when the guide is extended, it is used to guide an aircraft to be landed on the landing plate, or when the guide is retracted, it is used to enable the aircraft to glide on a runway. The guide part includes a support frame coupled to the upper surface of the main body in a retracted and extended manner and disposed at a predetermined interval along the circumferential surface of the landing plate, and a guide plate rotatably coupled to an upper end of the support frame to be capable of being unfolded inward of the landing plate or being stacked on the support frame. Advantageous effects According to the aircraft carrier convenient for taking off and landing of the aircraft, the landing plate which is retracted and extended through elasticity is combined on the main body, so that the impact force of the aircraft during landing is effectively buffered, stable landing can be ensured, and the durability of the aircraft body can be obviously improved. In addition, the landing plate is fixed in a downward moving state, and is released when the aircraft takes off, and the aircraft is lifted up through elasticity, so that the aircraft can realize the instantaneous lift-off of the aircraft by means of the elastic action at the moment of taking off, and the effect of quick taking off is obtained. Drawings Fig. 1 is a perspective view of an aircraft carrier according to a preferred embodiment of the invention for facilitating the landi