首页> 外国专利> DYNAMIC AND STATIC LOAD SYNCHRONOUS SERVO CONTROL SYSTEM FOR THREE-AXIS SIX-DIRECTION HOPKINSON PRESSURE BAR

DYNAMIC AND STATIC LOAD SYNCHRONOUS SERVO CONTROL SYSTEM FOR THREE-AXIS SIX-DIRECTION HOPKINSON PRESSURE BAR

机译:三轴六向霍普金森压力杆的动态和静态负载同步伺服控制系统

摘要

Provided is a dynamic and static load synchronous servo control system for a three-axis six-direction Hopkinson pressure bar, wherein a square bar (10, 21, 34, 43, 53, 60) is fixed by a self-lubricating square bar and a support frame (11, 18, 33, 44, 52, 55), and the square bar (10, 21, 34, 43, 53, 60) is in centring connection with a central cube square box (63) in a square opening; a confining pressure loading hydraulic cylinder (2, 24, 45) and a confining pressure loading actuator (2, 27, 46) are combined with a confining pressure loading frame (7, 31, 47) in series; an electromagnetic pulse excitation chamber (6, 14, 29, 40, 49, 57) is placed in the confining pressure loading frame (7, 17, 31, 37, 47, 58) and is freely and tightly fitted with an incident end of the square bar (10, 21, 34, 43, 53, 60); and the confining pressure loading frame (7, 17, 31, 37, 47, 58) is connected to a boss (8, 20, 32, 42, 51, 61) in series, and the boss (8, 20, 32, 42, 51, 61) is disposed at the incident end of the square bar (10, 21, 34, 43, 53, 60). The arrangement of the boss (8, 20, 32, 42, 51, 61) can ensure that the incident end of the Hopkinson pressure bar is a free end after a test sample (64) is subjected to a static confining pressure, the problem of being unable to ensure the free state of the end of a Hopkinson incident bar after static pre-stress is applied in the traditional dynamic and static combination Hopkinson bar system is solved, and test conditions are provided for subsequent application of electromagnetic excitation stress pulses and an ultrasonic test under in-situ pressure maintenance conditions.
机译:提供了一种用于三轴六向霍普金森压力杆的动,静载荷同步伺服控制系统,其中,方杆(10、21、34、43、53、60)由自润滑方杆固定,并且支撑框架(11、18、33、44、52、55),而方杆(10、21、34、43、53、60)与一个方形的中央立方体方盒(63)居中连接开幕围压负荷液压缸(2、24、45)和围压负荷致动器(2、27、46)与围压负荷框架(7、31、47)串联组合。电磁脉冲激发室(6、14、29、40、49、57)放置在围压加载框架(7、17、31、37、47、58)中,并自由紧密地与方棒(10、21、34、43、53、60);围压负荷框架(7、17、31、37、47、58)与凸台(8、20、32、42、51、61)串联连接,凸台(8、20、32, 42、51、61)布置在方杆(10、21、34、43、53、60)的入射端。凸台(8、20、32、42、51、61)的布置可以确保霍普金森压力杆的入射端是在测试样品(64)承受静态围压后的自由端,这是问题所在。解决了传统的动态和静态组合霍普金森棒系统中施加静态预应力后无法确保霍普金森入射棒末端的自由状态的问题,并为随后施加电磁激励应力脉冲提供了测试条件,在原位压力维持条件下进行超声波测试。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号