Affiliation:
1. Turbomachinery Laboratory, Texas A&M University, College Station, TX 77843
Abstract
Selected test results are presented for an annular gas seal using a smooth rotor and a hole-pattern-roughness stator for a supply pressure of 70 bar, three pressure ratios, three speeds up to 20,000 rpm, two clearances, and three preswirl ratios. Dynamic data include frequency-dependent direct and cross-coupled stiffness and damping coefficients. Static data include leakage and upstream and downstream pressures and temperatures. Very good agreements are found between measurements and predictions from a two-control-volume bulk-flow model.
Subject
Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials
Reference21 articles.
1. Childs, D., and Moyer, D., 1985, “Vibration Characteristics of the HPOTP (High Pressure Oxygen Turbopump) of the SSME (Space Shuttle Main Engine),” ASME J. Eng. Gas Turbines Power, 107, pp. 152–159.
2. Yu, Z., and Childs, D. W., 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, 120(4), pp. 778–783.
3. Moore, J., Walker, S., and Kuzdal, M., 2002, “Rotordynamic Stability Measurements During Full Load Testing of a 6000 psi Reinjection Centrifugal Compressor,” Proceedings, 31st Texas A&M University Turbomachinery Symposium, pp. 29–38.
4. Gelin, A., Pugnet, J.-M., Bolusset, D., and Friez, P., 1996, “Experience in Full Load Testing Natural Gas Compressors for Rotordynamic Improvements,” International Gas Turbine Conference, ASME Paper No. 96-GT-378.
5. Memmott, E., 1994, “Stability of a High Pressure Centrifugal Compressor Through Application of Shunt Holes and a Honeycomb Labyrinth,” 13th Machinery Dynamics Seminar, CMVA, September, 12–13.
Cited by
65 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献