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contributor authorKim, Baik Jin
contributor authorOh, Joseph
contributor authorPalazzolo, Alan
date accessioned2022-05-08T09:19:11Z
date available2022-05-08T09:19:11Z
date copyright2/21/2022 12:00:00 AM
date issued2022
identifier issn0742-4795
identifier othergtp_144_03_031027.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284983
description abstractHirth coupling transmits high torques in the rotating assemblies of compressors and turbines. Their mating surface contacts cause local changes in lateral shaft stiffness. This is affected by the teeth geometry, contact surface area, coupling preload, and surface finish at the contact faces. Industry practice ignores localized lateral flexibility from the Hirth coupling, or is guided by limited experience-based rules of thumb. The authors provide a novel modeling approach utilizing 3D solid finite elements which accounts for contact deformations, intricate interface teeth geometries, stress concentration, and surface finish. This provides an increased accuracy localized stiffness model for the Hirth coupling, to improve rotordynamic response predictions. Free–free natural frequencies of a test rotor including a Hirth coupling are experimentally measured. The rotor is instrumented with strain gauges for preload force measurements, and the Hirth coupling contacting surface profiles are measured with a stylus type surface profiler. A GW contact model is obtained from the measured surface profiles. An iterative computation algorithm is utilized to calculate Hirth coupling contact stiffness and contact pressure at the complex-shaped contact surfaces. Predicted and measured natural frequencies are compared versus preload.
publisherThe American Society of Mechanical Engineers (ASME)
titleTest and Theory for a Refined Structural Model of a Hirth Coupling
typeJournal Paper
journal volume144
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4052088
journal fristpage31027-1
journal lastpage31027-11
page11
treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 003
contenttypeFulltext


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