发明名称 AIRCRAFT DESIGNING METHOD, AIRCRAFT DESIGNING PROGRAM AND AIRCRAFT DESIGNING APPARATUS
摘要 An aircraft designing apparatus receives set values of design parameters related to the shape of an intake duct, creates analysis models for an aerodynamic characteristic analysis and a radar-cross-section analysis by using the values of the design parameters, calculates aerodynamic characteristics and radar-cross-section characteristics of the intake duct, and determines whether or not this analytical result satisfies a preset design condition. If it is determined that the analytical result does not satisfy the design condition, the values of the design parameters are updated. The updating of the design parameters, the analyses of the aerodynamic characteristics and the radar-cross-section characteristics, and the determining process are repeated until it is determined that the analytical result satisfies the design condition.
申请公布号 US2016092629(A1) 申请公布日期 2016.03.31
申请号 US201514864478 申请日期 2015.09.24
申请人 FUJI JUKOGYO KABUSHIKI KAISHA 发明人 SATO Kazushige;MURAKAMI Chikage;ISO Hideo
分类号 G06F17/50 主分类号 G06F17/50
代理机构 代理人
主权项 1. An aircraft designing method of designing a shape of a predetermined design object in an aircraft, the aircraft designing method comprising: a design-parameter setting step for setting a value of at least one design parameter related to the shape of the design object; an analyzing step for creating analysis models for an aerodynamic characteristic analysis and a radar-cross-section analysis by using the value of the at least one design parameter and calculating aerodynamic characteristics and radar-cross-section characteristics of the design object; a determining step for determining whether or not an analytical result obtained in the analyzing step satisfies a preset design condition; and a design-parameter updating step for updating the value of the at least one design parameter if a determination result obtained in the determining step indicates that the analytical result obtained in the analyzing step does not satisfy the design condition, wherein the analyzing step, the determining step, and the design-parameter updating step are repeated until the determination result obtained in the determining step indicates that the analytical result obtained in the analyzing step satisfies the design condition.
地址 Tokyo JP