Honeycomb annular seals are an attractive design alternative due to their superior static and dynamic performance. However, their implementation in industrial practice has been delayed by the following characteristics: a) manufacturing time can be appreciable, and b) they can seriously damage the shaft if rubbing occurs. To minimize these problems, “hole-pattern” gas damper seals, which are formed by simply drilling holes into an annular smooth seal, were manufactured and tested. The hole-pattern damper seal stator can be made of high-strength plastic materials which are less likely to damage a shaft during rubbing. The experimental results presented demonstrate that, compared to a honeycomb seal, a hole-pattern damper seal with 3.18 mm hole diameters and a high percentage of hole surface has achieved: (a) an average of 12 percent reduction in leakage rate, and(b) considerably higher effective damping, especially under high speeds and low inlet pressure ratio conditions.
Skip Nav Destination
Article navigation
October 1998
Research Papers
A Comparison of Experimental Rotordynamic Coefficients and Leakage Characteristics Between Hole-Pattern Gas Damper Seals and a Honeycomb Seal
Z. Yu,
Z. Yu
Turbomachinery Laboratory, Texas A&M University, College Station, TX 77843-3254
Search for other works by this author on:
D. W. Childs
D. W. Childs
Turbomachinery Laboratory, Texas A&M University, College Station, TX 77843-3254
Search for other works by this author on:
Z. Yu
Turbomachinery Laboratory, Texas A&M University, College Station, TX 77843-3254
D. W. Childs
Turbomachinery Laboratory, Texas A&M University, College Station, TX 77843-3254
J. Eng. Gas Turbines Power. Oct 1998, 120(4): 778-783 (6 pages)
Published Online: October 1, 1998
Article history
Received:
February 3, 1997
Online:
November 19, 2007
Citation
Yu, Z., and Childs, D. W. (October 1, 1998). "A Comparison of Experimental Rotordynamic Coefficients and Leakage Characteristics Between Hole-Pattern Gas Damper Seals and a Honeycomb Seal." ASME. J. Eng. Gas Turbines Power. October 1998; 120(4): 778–783. https://doi.org/10.1115/1.2818467
Download citation file:
Get Email Alerts
Cited By
Gas Turbine Combustion Optimization Using Neural Network Model and Wavelet Analysis
J. Eng. Gas Turbines Power
Experimental and Numerical Investigations into the Blade Tip Phantom Cooling Performance
J. Eng. Gas Turbines Power
Related Articles
Theory Versus Experiment for the Rotordynamic Characteristics of a High Pressure Honeycomb Annular Gas Seal at Eccentric Positions
J. Tribol (April,2003)
Experimental Study on Static and Dynamic Characteristics of Liquid Annular Convergent-Tapered Damper Seals With Honeycomb Roughness Pattern
J. Tribol (July,2003)
Dynamic Characteristics of the Diverging Taper Honeycomb-Stator Seal
J. Turbomach (October,2006)
Related Proceedings Papers
Related Chapters
Nonmetallic Pressure Piping System Components Part A: Experience With Nonmetallic Materials in Structural/Pressure Boundary Applications
Online Companion Guide to the ASME Boiler and Pressure Vessel Codes
Nonmetallic Pressure Piping System Components 1 Part A: Experience With Nonmetallic Materials in Structural/Pressure Boundary Applications
Companion Guide to the ASME Boiler and Pressure Vessel Codes, Volume 1, Fifth Edition
Classification of Part Shaping Methods
Introduction to Plastics Engineering