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contributor authorJ. Tecza
contributor authorJ. Walton
date accessioned2017-05-08T23:41:20Z
date available2017-05-08T23:41:20Z
date copyrightApril, 1993
date issued1993
identifier issn1528-8919
identifier otherJETPEZ-26715#360_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111941
description abstractIn this paper a novel, high-load chambered porous damper design, supporting analysis, and experimental results are presented. It was demonstrated that significant damping can be generated from the viscous discharge losses of capillary tubes arranged in chambered segments with large radial clearances and that the resulting damping is predictable and fairly constant with speed and eccentricity ratio. This design avoids the nonlinearities associated with high-eccentricity operation of conventional squeeze film dampers. Controlled orbit tests with a porous chambered configuration were completed and favorably compared with theoretical predictions. The ability to accommodate high steady-state and transient imbalance conditions makes this damper well suited to a wide range of rotating machinery, including aircraft gas turbine engines.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Chambered Porous Damper for Rotor Vibration Control: Part I—Concept Development
typeJournal Paper
journal volume115
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906717
journal fristpage360
journal lastpage365
identifier eissn0742-4795
keywordsDampers
keywordsRotor vibration
keywordsDamping
keywordsDesign
keywordsGas turbines
keywordsAircraft
keywordsSteady state
keywordsMachinery AND Stress
treeJournal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002
contenttypeFulltext


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