FLIGHT VEHICLE

• Main Authors: HUH JAE SUNG, KANG SEUNG HWAN, LIM BYEUNG JUN, JUN SANG OOK, PARK POO MIN
• Format: Patent
• Language: English; Korean
• Published: 21.06.2023
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; BLASTING; COSMONAUTICS; DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HEAT EXCHANGE IN GENERAL; HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT; HEATING; LIGHTING; MECHANICAL ENGINEERING; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING; WEAPONS

According to one embodiment, an aircraft may comprise: an aircraft body; an air inlet provided on at least one side of the outer surface of the aircraft body; an internal flow path having a flow cross-section that forms an angle with the inflow surface of the air inlet; a water cooling tube disposed between the air inlet and the internal flow path; and a fin assembly vertically coupled to the water cooling tube. At least a portion of the fin assembly may be arranged parallel to the flow direction of the internal flow path. 일 실시예에 따른 비행체는, 비행체 본체; 상기 비행체 본체 외측의 적어도 일 면에 구비된 공기 유입구; 상기 공기 유입구의 유입면과 각도를 이루는 유동 단면을 가지는 내부 유로; 상기 공기 유입구와 상기 내부 유로 사이에 배치된 수냉 튜브; 및 상기 수냉 튜브에 수직하게 결합된 핀 조립체;를 포함할 수 있고, 상기 핀 조립체의 적어도 일부는 상기 내부 유로의 유동 방향에 평행하게 배치될 수 있다.