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contributor authorJ. M. Vance
contributor authorA. F. Storace
contributor authorB. P. Cardon
contributor authorL. A. San Andres
date accessioned2017-05-08T23:41:20Z
date available2017-05-08T23:41:20Z
date copyrightApril, 1993
date issued1993
identifier issn1528-8919
identifier otherJETPEZ-26715#383_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111944
description abstractA gas-operated bearing damper for turbomachinery has been designed, analyzed, and experimentally investigated in the laboratory. The damper utilizes air bled off from the compressor to power an actuator through orifices with area modulated by the vibratory displacement at the bearing support. The design objective for this passive device is to make the actuating dynamic gas pressure phase lead the vibratory displacement by 90 deg. Several variations of the basic concept have been tested. An analysis was performed to guide the experiments. All of the designs tested to date can produce positive damping, and one particular design has produced a damping coefficient of 8756 N-s/m (50 lb-sec/in.) with a power penalty of 5.2 kW (7 hp) at 310 KPa (45 psi). This design was installed on a laboratory rotor with flexibly supported ball bearings, and significant damping of the critical speed response was demonstrated. The experimental results to date suggest that further research can produce significant improvements in performance, and the device appears to be especially adaptable to high-temperature applications for aircraft engines.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Gas-Operated Bearing Damper for Turbomachinery
typeJournal Paper
journal volume115
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906720
journal fristpage383
journal lastpage389
identifier eissn0742-4795
keywordsBearings
keywordsDampers
keywordsTurbomachinery
keywordsDamping
keywordsDesign
keywordsDisplacement
keywordsOrifices
keywordsPressure
keywordsCompressors
keywordsActuators
keywordsRotors
keywordsBall bearings
keywordsAircraft engines AND High temperature
treeJournal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002
contenttypeFulltext


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