According to a preferred embodiment of the present invention, a temperature control device for a launch tube comprises: a base part which is coupled to the launch tube and controls the temperature of a projectile accommodated in the launch tube; a temperature control part spaced apart at a predetermined distance from the base part, and configured so as to come in contact with the projectile to control the temperature of the projectile; and a connection part connecting the base part and the temperature control part.
본 발명의 바람직한 실시예에 따른 발사관용 온도 조절 장치는, 발사관의 내부에 수용되는 발사체의 온도를 조절하는 것으로서, 상기 발사관에 결합하는 베이스부, 상기 베이스부로부터 소정 간격 이격되게 구비되고, 상기 발사체에 접촉하도록 구성되어 상기 발사체의 온도를 조절하는 온도조절부, 및 상기 베이스부와 상기 온도조절부를 연결하는 연결부를 포함한다.
Temperature control apparatus for launching tube
발사관용 온도 조절 장치
30.01.2019
Patent
Elektronische Ressource
Koreanisch
IPC: | F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze / B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS |
Multi-tube unmanned aerial vehicle launching control system
Europäisches Patentamt | 2023
|HORIZONTAL LAUNCHING TUBE CONTROL APPARATUS USING DUPLICATED CONTROL AND SUBMARINE HAVING THE SAME
Europäisches Patentamt | 2016
|