English translation for "weight requirement"
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- 重量规格
Related Translations:
- Example Sentences:
| 1. | Meet the minimum height and weight requirement male candidates : 163 cm tall and weigh 50kg
男性身高最少一百六十三厘米，体重最少五十千克。 | | 2. | Waive the minimum weight requirement for one - off posting of a maximum of 1 , 000 items upon presentation of the coupon
凭优惠券使用大量投寄空邮邮件服务投寄不多于1 , 000封邮件，可获豁免最低重量限制的要求。 | | 3. | Well , i have never participated in a blood donation . actually i am willing to donate blood . but i am not up to the standard of weight requirement . what a pity
我从来没参与过献血，事实上我很愿意献血，不过我的体重不够献血的标准。遗憾啊！ | | 4. | Putz admits that the ball is on the light side of fifa ' s 420 to 445 gram weight requirement , but says it is no bigger than previous balls . the controversy over the ball also has an off - pitch dimension
普策承认"飞火流星"的重量没有达到国际足联规定的420到445克之间的重量标准，但是在体积上却是有所增加。 | | 5. | 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 | | 6. | 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 | | 7. | These enhancements include the lowering of minimum quantity requirement for bulk local mail from 3 , 000 to 2 , 000 items per posting ; minimum weight requirement for bulk air mail from 20 kg to 5 kg per posting ; and minimum requirement for permit mail posting for both local and international mail from 500 to 100 items per posting
它们包括把大量投寄本地邮件的数量由每次最少三千件调低至二千件；把大量投寄空邮邮件的最低重量由二十千克减至五千克；而以特许邮递方式投寄的本地和国际邮件的最低要求则由每次五百件降至一百件。 |
- Similar Words：
- "weight reduction regimen" English translation, "weight reduction with drugs" English translation, "weight register" English translation, "weight relieving motion" English translation, "weight report" English translation, "weight response type car retarder" English translation, "weight restriction" English translation, "weight retainer" English translation, "weight ring" English translation, "weight rod" English translation
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