본 발명은 비행체의 이착륙이 용이한 항공모함에 관한 것으로, 항공모함에 있어서, 본체; 및 상기 본체의 상면에 탄성에 의해 인입출 가능하도록 착륙판이 결합되고, 상기 착륙판에 비행체가 착륙 시 탄성을 통해 충격을 완화시키는 완충부;를 포함한다. 이러한 구성으로, 본체에 착륙판이 탄성에 의해 인입출 가능하도록 결합됨으로써, 비행체의 착륙 시 충격을 완화시킬 수 있어 안정적인 착륙은 물론, 기체의 내구성이 향상되는 효과를 얻을 수 있다.
The present invention relates to an aircraft carrier enabling easy takeoff and landing of an aircraft, the aircraft carrier comprising: a main body; and a buffer unit in which a landing plate is coupled to the top surface of the main body so as to be inserted and withdrawn by means of elasticity, and which mitigates impact by means of elasticity when an aircraft lands on the landing plate. Accordingly, the landing plate is coupled to the main body so as to be inserted and withdrawn by means of elasticity, thereby mitigating an impact during landing of an aircraft, thus enabling stable landing and improving airframe durability.
AIRCRAFT CARRIER
비행체의 이착륙이 용이한 항공모함
2024-07-30
Patent
Electronic Resource
Korean
IPC: | B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F16F SPRINGS , Federn |
Engineering Index Backfile | 1963
|Engineering Index Backfile | 1937
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