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| Content Provider | The American Society of Mechanical Engineers (ASME) Digital Collection |
|---|---|
| Author | Peter, P. Galimutti Jerzy, T. Sawicki David, P. Fleming |
| Copyright Year | 2009 |
| Abstract | Analyses were performed on finger seal pads having a pressure drop across the pad at right angles to the direction of runner velocity. The film was tapered; the clearance could decrease in both the pressure flow and velocity directions. A substantial load could be carried solely due to the pressure flow; however, the bearing exhibited negative stiffness without film convergence in the velocity flow direction. This is in marked contrast to a full circular bearing or ring seal, where pressure flow alone produces a significant stiffness as long as the clearance converges in the flow direction. The performance of three different pad configurations has been evaluated: aspect ratios L/B of 0.5, 1 (square pad), and 2. Design examples pertaining to each aspect ratio were studied for a gas turbine seal. Results show that lowest leakage, highest load carrying capacity, and highest stiffness are attained for the wide-pad configuration, L/B = 0.5. This paper presents a detailed study of the pad; additional analysis needs to be done for the inclusion of the finger and many other considerations for designing a complete seal. |
| Sponsorship | International Gas Turbine Institute |
| Starting Page | 941 |
| Ending Page | 950 |
| Page Count | 10 |
| File Format | |
| ISBN | 9780791848876 |
| DOI | 10.1115/GT2009-59842 |
| e-ISBN | 9780791838495 |
| Volume Number | Volume 6: Structures and Dynamics, Parts A and B |
| Conference Proceedings | ASME Turbo Expo 2009: Power for Land, Sea, and Air |
| Language | English |
| Publisher Date | 2009-06-08 |
| Publisher Place | Orlando, Florida, USA |
| Access Restriction | Subscribed |
| Subject Keyword | Design Leakage Load bearing capacity Gas turbines Bearings Pressure drop Clearances (engineering) Stiffness Flow (dynamics) Pressure Stress |
| Content Type | Text |
| Resource Type | Article |
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