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 |
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分类号 |
G01G23/01;G01M9/06;(IPC1-7):G01G/ |
主分类号 |
G01G23/01 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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