| contributor author | Takahashi, Naohiko | |
| contributor author | Miura, Haruo | |
| contributor author | Narita, Mitsuhiro | |
| contributor author | Nishijima, Noriyo | |
| contributor author | Magara, Yohei | |
| date accessioned | 2017-05-09T01:17:39Z | |
| date available | 2017-05-09T01:17:39Z | |
| date issued | 2015 | |
| identifier issn | 1528-8919 | |
| identifier other | gtp_137_03_032509.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/157896 | |
| description abstract | This paper deals with a new type of damper seal developed for a highpressure centrifugal compressor. Honeycomb seals and hole pattern seals are popularly used as damper seals and provide superior rotordynamic damping characteristics. Honeycomb seals are expensive because the manufacturing process is complex. Hole pattern seals are easier to manufacture, but they are still expensive. Use of a scallop pattern is one way to reduce manufacturing cost and time. A new seal that has a scallop pattern and small teeth on the stator surface is proposed. This pattern is cut on the stator surface using a disk type tool. To estimate the rotordynamic coefficients of this new seal, a bulk flow model code that is based on a twocontrolvolume model developed by Matsuda for labyrinth seals was newly developed. This model uses the Hirs model for the viscous shear stresses. The friction factor coefficients for the rotor surface, the stator surface, and the surface between the twocontrolvolumes were determined by computational fluid dynamics (CFD) steady analysis. The rotordynamic coefficients can also be obtained by using CFD perturbation analysis. The high accuracy of the bulk flow model was demonstrated by comparing its results with CFD perturbation analysis results. In the perturbation analysis, the whirling motion was treated as a steadystate problem by using a rotating frame of reference. For the damper seal, the rotor surface and its neighboring region were treated with a rotating frame of reference and the neighboring region of the stator was treated with a stationary frame of reference. The damping property of the new seal was evaluated by conducting rotor stability tests using a highpressure compressor with an electromagnetic exciter. The new seal equipped with swirl brakes was used for the balance piston of the compressor. Stability was evaluated by exciting the rotor during operation and identifying the eigenvalues of the rotor. The experimental results showed that the new seal increases damping. Comparison of the damping effect with calculations based on the bulk flow analysis showed good agreement. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Development of Scallop Cut Type Damper Seal for Centrifugal Compressors | |
| type | Journal Paper | |
| journal volume | 137 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4028448 | |
| journal fristpage | 32509 | |
| journal lastpage | 32509 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 003 | |
| contenttype | Fulltext | |