发明名称 Airfoil-shaped fluid flow tool for use in making differential measurements
摘要 A fluid flow tool includes an airfoil structure and a support arm. The airfoil structure's high-pressure side and low-pressure side are positioned in a conduit by the support arm coupled to the conduit. The high-pressure and low-pressure sides substantially face opposing walls of the conduit. At least one measurement port is formed in the airfoil structure at each of its high-pressure side and low-pressure side. A first manifold, formed in the airfoil structure and in fluid communication with each measurement port so-formed at the high-pressure side, extends through the airfoil structure and support arm to terminate and be accessible at the exterior wall of the conduit. A second manifold, formed in the airfoil structure and in fluid communication with each measurement port so-formed at the low-pressure side, extends through the airfoil structure and support arm to terminate and be accessible at the exterior wall of the conduit.
申请公布号 US8733180(B1) 申请公布日期 2014.05.27
申请号 US201113302845 申请日期 2011.11.22
申请人 ENGLAND JOHN DWIGHT;KELLEY ANTHONY R.;CRONISE RAYMOND J.;THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 ENGLAND JOHN DWIGHT;KELLEY ANTHONY R.;CRONISE RAYMOND J.
分类号 G01F1/34 主分类号 G01F1/34
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