发明名称 NOZZLE DEVICE EXPOSED IN HIGH TEMPERATURE AND HIGH VELOCITY GAS AND ROCKET HAVING THE SAME
摘要 PURPOSE: A nozzle device in high-temperature and high-velocity gas and a rocket having the same are provided to prevent a coating unit from becoming separated from a nozzle unit through a cover unit which covers the gap between the nozzle unit and the coating unit. CONSTITUTION: A nozzle device in high-temperature and high-velocity gas comprises a nozzle unit(141), a coating unit(142), and a cover unit(143). One end of the nozzle unit is connected to a combustion chamber of a propellant, and the other end is toward the outside. The nozzle unit is made of a titanium alloy. The coating unit is made of a ceramic material. The inner surface of the nozzle unit is coated with the coating unit. The cover unit covers a gap between the inner surface of the nozzle unit and the coating unit to prevent the coating unit from becoming separated from the nozzle unit.
申请公布号 KR20120027864(A) 申请公布日期 2012.03.22
申请号 KR20100089673 申请日期 2010.09.13
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 KIM, HONG KYU;SONG, YOUNG BEUM;HONG, SUNG SUK;SHIM, IN OK
分类号 F02K9/97;B64G1/40;C22C14/00 主分类号 F02K9/97
代理机构 代理人
主权项
地址