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    • 43. 发明申请
    • CARBON HEATING ELEMENT, MANUFACTURING METHOD THEREOF, HEATING LAMP HAVING THE SAME AND HEATING LAMP WITH SUPPORTING PART AND FLEXIBLE PART
    • 碳加热元件及其制造方法,具有该加热元件的加热灯和具有支撑部件和柔性部件的加热灯
    • WO2012102457A1
    • 2012-08-02
    • PCT/KR2011/007721
    • 2011-10-18
    • LEE, Woo Yong
    • LEE, Woo Yong
    • H05B3/14
    • H05B3/0033H05B3/145H05B2203/017
    • Disclosed are a carbon heating element, etc. The carbon heating element according to the present invention comprises a carbon heating main body which comprises a carbon compound and is formed to generate heat by supplied power; a terminal part which is provided in both ends of the carbon heating main body and comprises a carbon compound and is formed to supply power to the carbon heating main body; and a coupling part which surface-contacts the carbon heating main body and the terminal part and coupled to the carbon heating main body and the terminal part by pressure before the carbon compound of the carbon heating main body and the carbon compound of the terminal part are formed and dried. Thus, the carbon heating element may improve a structure of a terminal part of the carbon heating element and improve product stability, reliability and economic efficiency.
    • 公开了碳加热元件等。根据本发明的碳加热元件包括碳加热主体,其包含碳化合物,并且通过供电而形成为产生热量; 端子部,其设置在碳加热主体的两端,并且包括碳化合物,并且形成为向碳加热主体供电; 以及与碳加热主体和端子部分表面接触并且在碳加热主体的碳化合物和端子部分的碳化合物之前通过压力耦合到碳加热主体和端子部分的耦合部分是 形成并干燥。 因此,碳加热元件可以提高碳加热元件的末端部分的结构,提高产品的稳定性,可靠性和经济性。
    • 44. 发明申请
    • DOOR CONTROL DEVICE COUPLED WITH WING DEPLOYMENT AND FLIGHT VEHICLE HAVING THE SAME
    • 与配置的车门控制装置和具有相同功能的飞行车辆
    • WO2011087189A1
    • 2011-07-21
    • PCT/KR2010/003756
    • 2010-06-11
    • AGENCY FOR DEFENSE DEVELOPMENTLEE, Woo YongSHIN, Sang HunHONG, Heon Suk
    • LEE, Woo YongSHIN, Sang HunHONG, Heon Suk
    • B64C3/56F42B10/14B64C1/14
    • F42B10/14
    • Disclosed are a door control device for a flight vehicle and a flight vehicle having the same, the door control device including, an opening formed at a main body of the flight vehicle and allowing a corresponding wing to be deployed from inside to outside of the main body, a door installed at the main body to be rotatable between a first state where the opening is open and a second state where the opening is closed, an elastic unit configured to apply an elastic force to the door such that the door rotates from the first state to the second state, and a door locking unit configured to lock the door in the first state, and, when the wing is deployed, unlock the door responsive to the deployment of the wing such that the door rotates to the second state, whereby the door can be closed without application of a separate driving device and an input of an additional operation signal, and the door control device having high operation reliability can be realized.
    • 公开了一种用于飞行器车辆的门控制装置和具有该门控制装置的机动车辆,门控制装置包括形成在飞行器主体上的开口,并允许对应的翼从内部到外部展开 主体,安装在主体上的门,以在开口打开的第一状态和开口关闭的第二状态之间旋转;弹性单元,其构造成向门施加弹力,使得门从 第一状态到第二状态,以及门锁单元,其构造成将门锁在第一状态,并且当机翼展开时,响应于机翼的展开来解锁门,使得门旋转到第二状态, 从而可以在不施加单独的驱动装置和附加操作信号的输入的情况下关闭门,并且可以实现具有高操作可靠性的门控制装置。