Show simple item record

contributor authorLuis San Andrés
contributor authorAdolfo Delgado
date accessioned2017-05-09T00:27:52Z
date available2017-05-09T00:27:52Z
date copyrightJuly, 2008
date issued2008
identifier issn1528-8919
identifier otherJETPEZ-27026#042505_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137906
description abstractThe paper presents parameter identification measurements conducted on a squeeze film damper (SFD) featuring a nonrotating mechanical seal that effectively eliminates lubricant side leakage. The SFD-seal arrangement generates dissipative forces due to viscous and dry-friction effects from the lubricant film and surfaces in contact, respectively. The test damper reproduces an aircraft application that must contain the lubricant for extended periods of time. The test damper journal is 2.54cm in length and 12.7cm in diameter, with a nominal clearance of 0.127mm. The damper feed end opens to a plenum filled with lubricant, and at its discharge grooved section, four orifice ports evacuate the lubricant. In earlier publications, single frequency force excitation tests were conducted, without and with lubricant in the squeeze film land, to determine the seal dry-friction force and viscous damping force coefficients. Presently, further measurements are conducted to identify the test system and SFD force coefficients using two sets of flow restrictor orifice sizes (2.8mm and 1.1mm in diameter). The flow restrictors regulate the discharge flow area and thus control the oil flow through the squeeze film. The experiments also include measurements of dynamic pressures at the squeeze film land and at the discharge groove. The magnitude of dynamic pressure in the squeeze film land is nearly identical for both sets of flow restrictors, and for small orbit radii, dynamic pressures in the discharge groove have peak values similar to those in the squeeze film land. The identified parameters include the test system damping and the individual contributions from the squeeze film, dry friction in the mechanical seal and structure remnant damping. The identified system damping coefficients are frequency and motion amplitude dependent due to the dry-friction interaction at the mechanical seal interface. Squeeze film force coefficients, damping and added mass, are in agreement with simple predictive formulas for an uncavitated lubricant condition and are similar for both flow restrictor sizes. The SFD-mechanical seal arrangement effectively prevents air ingestion and entrapment and generates predicable force coefficients for the range of frequencies tested.
publisherThe American Society of Mechanical Engineers (ASME)
titleSqueeze Film Damper With a Mechanical End Seal: Experimental Force Coefficients Derived From Circular Centered Orbits
typeJournal Paper
journal volume130
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2800345
journal fristpage42505
identifier eissn0742-4795
keywordsForce
keywordsFlow (Dynamics)
keywordsMotion
keywordsLubricants
keywordsDampers
keywordsDamping
keywordsInertia (Mechanics)
keywordsDry-friction whip and whirl
keywordsMeasurement
keywordsPressure
keywordsStress AND Gates (Closures)
treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record