发明名称 INTERNAL BALANCE CALIBRATION SYSTEM AND METHOD
摘要 A system for calibrating an internal balance used in the testing of scale models in wind tunnels including a base; apparatus for rigidly connecting a first portion of an internal balance to the base; force adaptor apparatus for rigidly engaging a second portion of the internal balance; apparatus for securing the force adaptor apparatus to the base, including apparatus for applying selected loads to the force adaptor apparatus so as to cause a corresponding loading on the internal balance; and low friction apparatus for coupling the force adaptor apparatus to the apparatus for securing, including apparatus for transmitting a direct force from the apparatus for applying selected loads to the force adaptor apparatus via a load point whose position relative to the force adaptor apparatus is substantially constant.
申请公布号 IL97982(D0) 申请公布日期 1992.06.21
申请号 IL19910097982 申请日期 1991.04.28
申请人 ISRAEL AIRCRAFT INDUSTRIES LTD. 发明人
分类号 G01G23/01;G01M9/06;(IPC1-7):G01G/ 主分类号 G01G23/01
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