分配设计的英文

• apportion design

• "分配"英文翻译    distribution; allocation; as ...
• "设计"英文翻译    devise; project; plan; desig ...
• "级配设计" 英文翻译 :    grade location
• "装配设计" 英文翻译 :    asd assembly design; design for assembly
• "红外分配设备" 英文翻译 :    infrared distribution equipment
• "空气分配设备" 英文翻译 :    air distribution equipment; air equipment
• "网络分配设备" 英文翻译 :    network distribution equipment
• "油品分配设备" 英文翻译 :    oil dispensing equipment
• "有线分配设备" 英文翻译 :    wired distribution equipment
• "巢式交配设计" 英文翻译 :    nested mating design
• "多系交配设计" 英文翻译 :    polycrossmating
• "间断极配设计" 英文翻译 :    gap-graded design
• "交互交配设计" 英文翻译 :    alternate mating design
• "实验交配设计" 英文翻译 :    experimental mating design
• "虚拟装配设计" 英文翻译 :    virtual assembly design
• "装配设计方案" 英文翻译 :    aslo; assembly layout
• "半双列交配设计" 英文翻译 :    half-diallelmating
• "部分双列交配设计" 英文翻译 :    partialdiallelmating
• "测交系交配设计" 英文翻译 :    testerstrainmating
• "单亲谱系交配设计" 英文翻译 :    incompletepedigreemating
• "全双列交配设计" 英文翻译 :    completediallelmating
• "双列杂交交配设计" 英文翻译 :    diallel mating design
• "双亲谱系交配设计" 英文翻译 :    completepedigreemating
• "自由授粉交配设计" 英文翻译 :    matingdesignofopen
• "电力用品和分配设备" 英文翻译 :    power supplies and distribution equipment

• The visual designer sets the expression for the associated control property , and then uses the evaluated expression result to assign control property values that are rendered on the design surface
  可视化设计器设置关联控件属性的表达式，然后再使用计算的表达式结果来分配设计图面上呈现的控件属性值。
• Abstract : a new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
  文摘:探讨了一种新的设计指标最优分配方法- -协同分配法,用于处理飞机顶层设计中的大规模设计指标最优分配问题.分析了飞机顶层设计中的设计指标最优分配特征,据此给出了协同法的原理并建立了数学模型.协同法按设计指标分配关系将最优分配问题分解为主系统优化和子系统优化,主优化对子系统设计指标进行最优分配,子优化以最小化分配设计指标值与期望设计指标值之间的差异为目标,进行子系统最优设计,或对底层元件(如飞机翼梁、翼肋和翼盒等)进行设计指标最优分配,并把最优解信息反馈给主优化.主优化通过子优化最优解信息构成的一致性约束协调分配量,提高系统整体性能,并重新给出分配方案.主系统与子系统反复协调,直到得到设计指标最优分配方案.两层可靠度指标分配算例初步验证了本文方法的正确性与可行性,三层可靠度指标分配算例证明了本文方法的有效性.最后,以重量指标分配为例,简要叙述了针对飞机顶层设计中设计指标协同分配的数学模型和求解思路
• A new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
  探讨了一种新的设计指标最优分配方法- -协同分配法,用于处理飞机顶层设计中的大规模设计指标最优分配问题.分析了飞机顶层设计中的设计指标最优分配特征,据此给出了协同法的原理并建立了数学模型.协同法按设计指标分配关系将最优分配问题分解为主系统优化和子系统优化,主优化对子系统设计指标进行最优分配,子优化以最小化分配设计指标值与期望设计指标值之间的差异为目标,进行子系统最优设计,或对底层元件(如飞机翼梁、翼肋和翼盒等)进行设计指标最优分配,并把最优解信息反馈给主优化.主优化通过子优化最优解信息构成的一致性约束协调分配量,提高系统整体性能,并重新给出分配方案.主系统与子系统反复协调,直到得到设计指标最优分配方案.两层可靠度指标分配算例初步验证了本文方法的正确性与可行性,三层可靠度指标分配算例证明了本文方法的有效性.最后,以重量指标分配为例,简要叙述了针对飞机顶层设计中设计指标协同分配的数学模型和求解思路
• Some problems occurred in the compensation management of cadi and the causes are discussed . according to the current situation of the human resource of cadi , the characteristics of engineers working in the cadi and the characteristics of the aircraft design , the distribution schemes focusing on job positions and performance are given , of which a linear programming model is built to resolve the performance compensation at the aim of max - motivation in order to form a suitable model of compensation management and to achieve " double - win " between the employee and the employer
  针对611所人力资源状况、工程技术人员特点及飞机设计专业工程工作特点，提出以岗位为核心的岗位薪点设计方案和以个人业绩为核心的绩效分配设计方案，建立了以激励强度最大化为目标的线性规划数模，用单纯形法求解绩效奖酬，以形成一种激励强度大、内部公平合理、对外具有竞争力的薪酬管理模式，即实现员工与组织在此问题上的“双赢” 。