Characteristics of a Spherical Seat TPJB With Four Methods of Directed Lubrication—Part II: Rotordynamic PerformanceSource: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 012::page 122503DOI: 10.1115/1.4036970Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Measured and predicted rotordynamic characteristics are presented for a four-pad, spherical-seat, tilting-pad journal bearing (TPJB) with 0.5 pivot offset, 0.6 L/D, 101.6 mm nominal diameter, and 0.3 preload in the load-between-pivots orientation. One bearing is tested four separate times in the following four different lubrication configurations: (1) flooded single-orifice (SO) at the bearing shell, (2) evacuated leading edge groove (LEG), (3) evacuated spray-bar blocker (SBB), and (4) evacuated spray-bar (SB). The same set of pads is used for every test to maintain clearance and preload; each method of lubrication is added as an assembly to the bearing. Test conditions include surface speeds and unit loads up to 85 m/s and 2.9 MPa, respectively. Dynamic data includes four sets (one set for each bearing configuration) of direct and cross-coupled rotordynamic coefficients derived from measurements and fit to a frequency-independent stiffness-damping-mass (KCM) matrix model. The pivot stiffness (pad and pivot in series) is measured and incorporated into predictions.
|
Show full item record
| contributor author | Coghlan, David M. | |
| contributor author | Childs, Dara W. | |
| date accessioned | 2017-11-25T07:16:10Z | |
| date available | 2017-11-25T07:16:10Z | |
| date copyright | 2017/23/8 | |
| date issued | 2017 | |
| identifier issn | 0742-4795 | |
| identifier other | gtp_139_12_122503.pdf | |
| identifier uri | http://138.201.223.254:8080/yetl1/handle/yetl/4233854 | |
| description abstract | Measured and predicted rotordynamic characteristics are presented for a four-pad, spherical-seat, tilting-pad journal bearing (TPJB) with 0.5 pivot offset, 0.6 L/D, 101.6 mm nominal diameter, and 0.3 preload in the load-between-pivots orientation. One bearing is tested four separate times in the following four different lubrication configurations: (1) flooded single-orifice (SO) at the bearing shell, (2) evacuated leading edge groove (LEG), (3) evacuated spray-bar blocker (SBB), and (4) evacuated spray-bar (SB). The same set of pads is used for every test to maintain clearance and preload; each method of lubrication is added as an assembly to the bearing. Test conditions include surface speeds and unit loads up to 85 m/s and 2.9 MPa, respectively. Dynamic data includes four sets (one set for each bearing configuration) of direct and cross-coupled rotordynamic coefficients derived from measurements and fit to a frequency-independent stiffness-damping-mass (KCM) matrix model. The pivot stiffness (pad and pivot in series) is measured and incorporated into predictions. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Characteristics of a Spherical Seat TPJB With Four Methods of Directed Lubrication—Part II: Rotordynamic Performance | |
| type | Journal Paper | |
| journal volume | 139 | |
| journal issue | 12 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4036970 | |
| journal fristpage | 122503 | |
| journal lastpage | 122503-13 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 012 | |
| contenttype | Fulltext |