Wednesday, October 19, 2011: 1:45 PM
Symphony I/II (Hilton Minneapolis)
It has been common practice to use classic pump curves when designing axial flow high-volume / low-head pumps. This presentation discusses axial pump design that is based on performance equations derived from an energy balance perspective. A specific real-world design case is presented for a pump with an output of 11,400 gallons per minute @ 6 foot head. Propeller 18.25 inch design OD was a required precondition. Primary design goal - maximize pumping efficiency. Leading edge prop geometry computed from incoming flow vector. Trailing edge prop geometry derived from energy-based performance equations with a slip-factor term borrowed from the world of marine prop design. Computational Fluid Dynamics (CFD) was used to predict the rotation-flow component of the fluid flow exiting the prop which was used to design the flow-straightener. A method for predicting a reasonable test RPM range will be discussed. A full-scale lab test was performed to pinpoint the final operating RPM within the predicted range and to verify the expected design performance. CAD models were made using 3-D parametric CAD from PTC (WildfireTM 4.0). Performance of pump was simulated using the mathematic computation software MathcadTM. Part design strength was verified by Finite Element Analysis (FEA, Pro/Mechanica). Fluid flow was predicted by CFD software from FluentTM. Pump test conformed to Hydraulics Institute HI 2.6 and US Army Corps of Engineers standard EM 1110-2-3105. Pump test evaluation included DigitalFlowTM ultrasonic flow meter, pressure transducers, and strain gauge based shaft power measurement using Microstrain Inc’s V-linkTM wireless RF telemetry.
See more of this Session: Novel Mixer and Mixed Reactor Design
See more of this Group/Topical: North American Mixing Forum
See more of this Group/Topical: North American Mixing Forum