Dual Clearance Squeeze Film Damper for High Load Conditions
| contributor author | David P. Fleming | |
| date accessioned | 2017-05-08T23:21:21Z | |
| date available | 2017-05-08T23:21:21Z | |
| date copyright | April, 1985 | |
| date issued | 1985 | |
| identifier issn | 0742-4787 | |
| identifier other | JOTRE9-28443#274_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/100496 | |
| description abstract | Squeeze film dampers are widely used to control vibrations in aircraft turbine engines and other rotating machinery. However, if shaft unbalance rises appreciably above the design value (e.g., due to a turbine blade loss), a conventional squeeze film will be overloaded, and will no longer be effective in controlling vibration amplitudes and bearing forces. This paper describes a new damper concept characterized by two oil films. Under normal conditions, only one low-clearance film is active, allowing precise location of the shaft centerline. Under high unbalance conditions, both films are active, controlling shaft vibration in a near-optimum manner, and allowing continued operation until a safe shutdown can be made. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Dual Clearance Squeeze Film Damper for High Load Conditions | |
| type | Journal Paper | |
| journal volume | 107 | |
| journal issue | 2 | |
| journal title | Journal of Tribology | |
| identifier doi | 10.1115/1.3261045 | |
| journal fristpage | 274 | |
| journal lastpage | 278 | |
| identifier eissn | 1528-8897 | |
| keywords | Stress | |
| keywords | Clearances (Engineering) | |
| keywords | Dampers | |
| keywords | Vibration | |
| keywords | Aircraft | |
| keywords | Design | |
| keywords | Gas turbines | |
| keywords | Bearings | |
| keywords | Turbine blades | |
| keywords | Force AND Machinery | |
| tree | Journal of Tribology:;1985:;volume( 107 ):;issue: 002 | |
| contenttype | Fulltext |