发明名称 EJECTING PERFORMANCE ANALYSIS METHOD USING OBJECT EJECTION MECHANISM ADDED LOAD
摘要 A method for analyzing the ejection performance of a projectile ejection mechanism considering an additional load of the present invention comprises: dividing a launching tube (10) accommodating a projectile (1) into a first chamber (20) and a second chamber (30), physically defining conditions generated in the first and second chambers (20, 30) when ejecting the projectile (1) in consideration of an additional load, and mathematically modeling a projectile ejection mechanism by a physically defined equation to determine the design parameters of the projectile ejection mechanism based on the additional load; and applying the design parameters to the input conditions of a performance analysis program built in a gas generator missile launcher simulator (GGMLsim) program to allow a GGMLsim to analyze the performance of the projectile ejection mechanism with an empirical equation, instead of a flow analysis code, for which a large amount of computational complexity is required. In particular, analysis time can be reduced, and design parameters can be easily analyzed while obtaining the analysis result of the performance of a projectile ejection mechanism considering an additional load. [Reference numerals] (AA) Upgrade; (S10) analyze projectile ejection performance; (S100) Utilize actually data; (S20) Run a GGMLsim(Gas Generator Missile Launcher Simulator) program; (S20-1) mathematical modeling-based additional load performance analysis program code; (S20-2) Performance analysis program flow chart; (S20-3) Performance analysis execution file; (S30) Select a performance test type; (S40) Maximum acceleration and ejection speed conditions of a projectile by an ejection apparatus when an additional load exists; (S41) Run the GGMLsim program; (S42) Acquire internal ballistics design data of a gas generator; (S50) Ejection performance conditions with the additional load assumed using a thrust profile of the gas generator obtained in a ground combustion test; (S51) Run the GGMLsim program; (S52) Acquire ejection performance prediction data of the projectile; (S60) Additional load ejection comprehensive performance conditions before performing a comprehensive ejection test; (S61) Run the GGMLsim program; (S62) Acquire comprehensive ejection test prediction data; (S70) Determine whether to compare and correct the data
申请公布号 KR101378846(B1) 申请公布日期 2014.03.27
申请号 KR20130105363 申请日期 2013.09.03
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 PARK, CHUL HYUN;HA, JAE HOON;KIM, IL SOO
分类号 G06F19/00 主分类号 G06F19/00
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