例句與造句

1. The experimental results show that distortion of the monolithic component from odd - even of the three different sequences is the smallest
   結(jié)果表明，三種模擬結(jié)果中奇偶銑削加工得到的結(jié)構(gòu)件的變形最小。
2. The first stage of cbd is the era of monolithic components , a seeming oxymoron that describes the adolescent state of components today
   Cbd的第一階段是單片式組件的時代，是今天組件青春期表面矛盾的描述。
3. Three milling machining sequences consisting of ordinal , odd - even and even - odd were simulated based on the model for frame monolithic components
   利用該模型對整體框類結(jié)構(gòu)件進行了奇偶銑削、偶奇銑削和順序銑削三種加工順序的有限元模擬。
4. The agreement of simulation and experimental results proves the validity of the model for predicting distortion law of aerospace monolithic components due to milling process
   該模型對三種加工順序的模擬結(jié)果與試驗結(jié)果一致，可用于預(yù)測整體結(jié)構(gòu)件的加工變形。
5. In the next stage , monolithic components give way to distributed components as maturing component standards and new infrastructural components permit component interoperability and portability
   在下一階段，隨著成熟的組件標(biāo)準(zhǔn)和新的基礎(chǔ)設(shè)施組件允許實現(xiàn)組件的互操作性和可移植性，單獨式組件讓位于分布式組件。
6. It's difficult to find monolithic component in a sentence. 用monolithic component造句挺難的
7. To resolve the problem of distortion of large - complex aerospace monolithic components during milling process , a finite element model ( fem ) of milling process simulation in distortion field and temper - attire field was established
   摘要為了控制尺寸大、形狀復(fù)雜的航空框類整體在銑削加工時產(chǎn)生的變形，建立了銑削加工時的變形場和溫度場的有限元模型。
8. In chapter 1 , the background and significance of this research is introduced firstly . then , the state of the art in the research of machining distortion of the monolithic component is summarized . finally , the main contents and frame structure of this dissertation are shown
   第一章闡述了論文研究的背景和意義,總結(jié)了航空整體結(jié)構(gòu)件數(shù)控加工變形的國內(nèi)外研究現(xiàn)狀,提出了本論文的研究內(nèi)容和總體框架。
9. Machining deformation of aircraft monolithic component is simulated by finite element method ( fem ) and validated by experiment . the initial residual stress in pre - stretched plate is generated by simulating quenching and stretching processes . with a single tool - tooth milling process fem , the machining loads in monolithic component material removing is obtained . restart - calculation is put forward to complete the whole simulation of machining process . to verify the fem result , an experiment is carried out . the deformation distribution of the monolithic component resulting from fem shows a good agreement with the experiment result , which indicates that the key technologies presented in the paper are practicable and can be used to simulate the milling process of monolithic component to predict its deformation . lengthy and expensive trial and error experiment process can be avoided
   在模擬淬火、拉伸過程獲得含有初始殘余應(yīng)力的預(yù)拉伸板材以及模擬單齒切削過程獲得切削載荷的基礎(chǔ)上,提出并采用接力算法,對一航空整體結(jié)構(gòu)件的材料銑削過程進行有限元仿真,同時進行了試驗研究.結(jié)果表明,有限元模擬的整體結(jié)構(gòu)件的變形與試驗具有一致性,從而證明提出的整體結(jié)構(gòu)件加工仿真關(guān)鍵技術(shù)的可行性,避免了為研究加工變形而進行的繁瑣的試錯法