发明名称 Tapered, frequency-tuned rotor for turbine flow meter
摘要 A frequency-tuned turbine flow meter rotor comprises a rotor hub and a plurality of tapered rotor blades. Each of the plurality of rotor blades has a stagger angle that varies as a function of a radius measured from the hub, and a cross-sectional profile that is tapered according to a NACA airfoil design. A method for designing a frequency-tuned flow meter rotor comprises defining a cross-sectional profile, calibrating a rotor blade stagger angle, tapering the cross-sectional profile such that it characterizes an airfoil with a decreasing chord length and a decreasing relative thickness as a function of radius, and analyzing a natural oscillation frequency spectrum of the rotor with respect to a range of operationally-induced excitation frequencies.
申请公布号 US2009320608(A1) 申请公布日期 2009.12.31
申请号 US20070704038 申请日期 2007.02.08
申请人 PRATT & WHITNEY ROCKETDYNE, INC. 发明人 MARCU BOGDAN;UBOWSKI JOHN
分类号 G01F1/06 主分类号 G01F1/06
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