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载人航天空间环境模拟器与某大型风洞制造的若干关键技术——记王仲仁总师的创新
引用本文:王若维,董小瑛.载人航天空间环境模拟器与某大型风洞制造的若干关键技术——记王仲仁总师的创新[J].塑性工程学报,2004,11(2):35-40.
作者姓名:王若维  董小瑛
作者单位:哈尔滨工业大学,哈尔滨,150001
摘    要:王仲仁教授为载人航天工程空间环境模拟器与某大型风洞制造项目的总师,这两个容器的最大直径均超过12m,均有大型法兰,对于风洞还有大尺寸的收缩形体,截面变化激烈。本文介绍了王仲仁教授在这两个项目制造过程中,在技术方案和成形技术方面的创新。

关 键 词:载人航天工程  空间环境  模拟器  大型法兰  柔性  多点成形
文章编号:1007-2012(2004)02-0035-06
修稿时间:2004年1月19日

Some key technologies used in manufacturing the space environmental simulator and a large wind tunnel--Innovations of Prof.Z.R.Wang
WANG Ruo-wei DONG Xiao-ying.Some key technologies used in manufacturing the space environmental simulator and a large wind tunnel--Innovations of Prof.Z.R.Wang[J].Journal of Plasticity Engineering,2004,11(2):35-40.
Authors:WANG Ruo-wei DONG Xiao-ying
Abstract:Prof. Z. R. Wang was the general engineer of the manufacturing project of the space environmental simulator and a large wind tunnel. The largest diameter in these two vessels is all larger than 12m and there are large size flanges in these two vessels. In the large wind tunnel, there is a large size double-curve panel structure with a complicated shape. In this paper, some innovations of Prof. Wang used in the manufacturing of these two projects are introduced
Keywords:KM-6  large size flange  flexible  reconfigurable forming
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