发明名称 STRENGTH CALCULATING SYSTEM OF THE HELICOPTER LANDING AREA AND CONTROLLING METHOD THEREFOR
摘要 The present invention provides a strength calculating system of a helicopter landing area and a control method thereof including a calculating terminal operating a landing strength calculating menu when a shipowner/classification strength bill is requested, then loading classification information and a 'D' value by a kind of a helicopter by inputting them, and then requesting the calculation of a landing strength value of the helicopter by inputting a deck and its detailed information and a management server outputting landing strength bill information to the calculating terminal after performing calculation by using specification information of the helicopter stored in a DB by receiving the 'D' value by kind of a helicopter, the classification information, the deck, and the detailed information. The present invention includes the calculating terminal and the management server storing basic information about the helicopter for ship building and performs the strength calculation of the helicopter landing area by inserting detail values of the deck after assorting standard information by inputting the 'D' value and the classification information suitable for a kind of the helicopter to a strength calculation input menu so that a worker immediately calculates a strength calculation value of the landing area according to the kind of the helicopter through the calculation system without manual strength calculation in order to maximize the efficiency of a landing strength calculation process.
申请公布号 KR20130134649(A) 申请公布日期 2013.12.10
申请号 KR20120058308 申请日期 2012.05.31
申请人 HYUNDAI HEAVY INDUSTRIES CO., LTD. 发明人 CHOI, MYUNG SOO
分类号 G06F19/00 主分类号 G06F19/00
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