Диссертация (785882), страница 69
Текст из файла (страница 69)
A. Brush seal leakagecorrelations based on effecitve thickness // 4th InternationalSymposium on Transport Phenomena and Dynamics of RotatingMachinery, ISROMAC-4. A. — Honolulu, HI, USA, 1992. —Pp. 296–304.208. Hybrid multistage brush seal : WO 2010/076636 / X. Zheng,J. J. Duquette. — 08.07.2010.209. Hydrodynamic brush seal : WO 2005/001316 / J. F. Justak. —06.01.2005.210. Hysteresis and bristle stiffening effects in brush seals / P. Basu[et al.] // Journal of Propulsion and Power.
— 1994. — Vol. 10,no. 4. — Pp. 569–575.211. Impact of frequency dependence of gas labyrinth seal rotordynamiccoefficients on centrifugal compressor stability / G. Vannini [et al.] //ASME Turbo Expo. — Glasgow, UK, 2010. — GT2010-22039.212. Improved steam turbine leakage control with a brush seal design /R. M.
Pastrana [et al.] // 30th Turbomachinery Symposium. —Texas A&M University, USA, 2001. — Pp. 33–38.213. Improved understanding of negative stiffness in filament seals /G. Franceschini [et al.] // ASME Turbo Expo. — Copenhagen,Denmark, 2012. — GT2012-68899.431Список литературы214. Improvement of conventional seals for rotor-stator cavities ofheavy-duty gas turbines by application of interstage brush-seals /M. Mantero [et al.] // ASME Turbo Expo. — San Antonio, TX,USA, 2013. — GT2013-95601.215. Innovative rotating intershaft brush seal for sealing between rotatingshafts.
Part I—Mechanical design of the rotating brush seal /G. Holloway [et al.] // 42nd AIAA/ASME/SAE/ASEE JointPropulsion Conference & Exhibit. — Sacramento, California, USA,2006. — AIAA 2006-4751.216. Instability of a high pressure compressor equipped with honeycombseals / M. Camatti [et al.] // 32nd Turbomachinery Symposium. —Texas A&M University, USA, 2003. — Pp. 39–48.217. Integrity testing of brush seal in shroud ring of T-700 engine /R. C. Hendricks [et al.] // NASA Seals Workshop. — 1992. — NASATM 105863.218. Investigation on the dynamic coefficients of impeller eye labyrinthseals / N.
G. Wagner [et al.] // 38th Turbomachinery Symposium. —Texas A&M University, USA, 2009. — Pp. 53–69.219. Iwatsubo T., Fukumoto K., Mochida H. An experimental study ofdynamic characteristics of labyrinth seals // RotordynamicInstability Problems in High-Performance Turbomachinery. —Texas A&M University, USA, 1993. — Pp. 219–237.220. Jahn I. H. J. Maximizing contacting filament seal performanceretention // ASME Turbo Expo. — San Antonio, TX, USA,2013. — GT2013-94261.221. Jahn I. H. J., Gillespie D., Cooper P. Hydrodynamic air-riding inleaf seals // ASME Turbo Expo. — San Antonio, TX, USA, 2013.
—GT2013-95585.222. Johnson K. L. Contact mechanics. — Cambridge : CambridgeUniversity Press, 2004. — P. 452.432Список литературы223. Jongh F. de The synchronous rotor instability phenomenon—Mortoneffect // 37th Turbomachinery Symposium. — Texas A&MUniversity, USA, 2008. — Pp. 159–167.224. Kaviany M. Principles of heat transfer in porous media. —2nd ed. — New York : Springer, 1995. — 708 pp.225. Kellenberger W. Spiral vibrations due to the seal rings inturbogenerators thermally induced interaction between rotor andstator // Journal of Mechanical Design. — 1980. — Vol. 102. —Pp.
177–184.226. Kim N., Rhode D. L. Refined turbulence modeling for swirl velocityin turbomachinery seals // International Journal of RotatingMachinery. — 2003. — Vol. 9. — Pp. 451–459.227. Kim T. S., Cha K. S. Comparative analysis of the influence oflabyrinth seal configuration on leakage behavior // Journal ofMechanical Science and Technology. — 2009. — Vol. 23. —Pp. 2830–2838.228. Klotz H., Brandt C. Alstom’s largest and most advanced steamturbine generator set for E.ON’s power plant DATTELN 4 //PowerGen Europe. — Milan, Italy, 2008.229.
Kordonski W. I., Gorodkin S. R. Magnetorheological fluid-basedseal // Journal of Intelligent Material Systems and Structures. —1996. — Vol. 7, no. 5. — Pp. 569–572.230. Krämer E. Dynamics of rotors and foundations. — Berlin : Springer,1993. — 383 pp.231. Kudriavtsev V. V., Braun M. J. Model developments for the brushseal numerical simulation // Journal of Propulsion and Power. —1996.
— Vol. 12. — Pp. 193–201.232. Kwanka K. Rotordynamic coefficients of short labyrinth gasseals—General dependency on geometric and physical parameters //Tribology Transactions. — 2007. — Vol. 50, no. 4. — Pp. 558–563.433Список литературы233. Kwanka K., Mair R. Identification of gas seal dynamic coefficientsbased on the stability behavior of a rotor // 1st European Conferenceon Turbomachinery. — Erlangen, Germany, 1995. — Pp.
297–309.234. Kwanka K., Ortinger W., Steckel J. Calculation and measurement ofthe influence of flow parameters on rotordynamic coefficients inlabyrinth seals // Rotordynamic Instability Problems inHigh-Performance Turbomachinery. — Texas A&M University,USA, 1993. — Pp. 209–218.235. Labyrinth seal and pocket damper seal high pressure rotordynamictest data / G. Vannini [et al.] // Journal of Engineering for GasTurbines and Power. — 2014.
— Vol. 136. — Pp. 022501–9.236. Labyrinth seal technology within the Dutch aero engine cluster /G. Kool [et al.] // ASME Turbo Expo. — Glasgow, UK, 2010. —GT2010-23469.237. Laos H. E., Vance J. M., Buchanan S. E. Hybrid brush pocketdamper seals for turbomachinery // Journal of Engineering for GasTurbines and Power. — 2000. — Vol. 122. — Pp. 330–336.238. Lattime S. B., Braun M. J., Choy F. K. Design considerationstowards the construction of hybrid floating brush seal // TribologyInternational. — 2004.
— Vol. 37. — Pp. 159–167.239. Leakage and rotordynamic coefficients of brush seals with zero coldclearance used in an arrangement with labyrinth fins / M. Gaszner[et al.] // Journal of Engineering for Gas Turbines and Power. —2013. — Vol. 135, no. 12. — Pp. 122506–11.
— DOI:10.1115/1.4025236.240. Lelli D., Chew J., Cooper P. Combined three-dimensional fluiddynamics and mechanical modeling of brush seals // Journal ofTurbomachinery. — 2006. — Vol. 128. — Pp. 188–195.241. Li J., De Choudhury P., Tacques R. Seal and bearing upgrade foreliminating rotor instability vibration in a high pressure natural gascompressor // ASME Turbo Expo. — Amsterdam, The Netherlands,2002. — GT2002-30635.434Список литературы242.
Li J., Obi S., Feng Z. The effects of clearance sizes on labyrinth brushseal leakage performance using a Reynolds-averaged Navier–Stokessolver and non-Darcian porous medium model // Proceedings of theInstitution of Mechanical Engineers, Part A: Journal of Power andEnergy. — 2009. — Vol. 223, no.
8. — Pp. 953–964.243. Li J., Qiu B., Feng Z. Experimental and numerical investigations onthe leakage flow characteristics of the labyrinth brush seal // Journalof Engineering for Gas Turbines and Power. — 2012. — Vol. 134,no. 10. — Pp. 102509–9.244. Li Z., Li J., Yan X. Multiple frequencies elliptical whirling orbitmodel and transient RANS solution approach to rotordynamiccoefficients of annual gas seals prediction // Journal of Vibration andAcoustics.
— 2013. — Vol. 135. — Pp. 031005–14.245. Lindsey W. T., Childs D. The effects of converging and divergingaxial taper on the rotordynamic coefficients of liquid annularpressure seals: theory versus experiment // Journal of Vibration andAcoustics. — 2000. — Vol. 122. — Pp. 126–131.246. Ludwig L. P. Gas path sealing in turbine engines: tech. rep. /NASA. — 1978. — NASA TM-73890.247. Lund J. W. Review of the concept of dynamic coefficients for fluidfilm journal bearings // Journal of Tribology. — 1987.
—Vol. 109. — Pp. 37–41.248. Mahler F., Boyes E. The application of brush seals in largecommercial jet engines // 31st AIAA/ASME/SAE/ASEE JointPropulsion Conference & Exhibit. — San Diego, CA, USA, 1995. —AIAA-95-2617.249. Malvano R., Vatta F., Vigliani A. Rotordynamic coefficients forlabyrinth gas seals: single control volume model // Meccanica. —2001. — Vol. 36.
— Pp. 731–744.435Список литературы250. Marie H. Dynamic simulation of finger seal-rotor interaction usingvariable dynamic coefficients // 42nd AIAA/ASME/SAE/ASEEJoint Propulsion Conference & Exhibit. — Sacramento, CA, USA,2006. — AIAA 2006-4931.251. Martin H. M. Labyrinth packings // Engineering. — 1908. —Vol.
85. — Pp. 33–36.252. Mason R. L., Gunst R. F., Hess J. L. Statistical Design and Analysisof Experiments. — 2nd ed. — Hoboken, NJ, USA : John Wiley &Sons, 2003.253. Mayhew E. R., Bill R. C., Voorhees W. J. Military engine sealdevelopment: potential for dual use // 30thAIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit.
— Indianapolis, IN, USA, 1994. — AIAA 94-2699.254. Menter F. Two-equation eddy-viscosity turbulence models forengineering applications // AIAA Journal. — 1994. — Vol. 32,no. 8. — Pp. 1598–1605.255. Millsaps K. T., Martinez-Sanchez M. Rotordynamic forces inlabyrinth seals: theory and experiment // Rotordynamic InstabilityProblems in High-Performance Turbomachinery. — Texas A&MUniversity, USA, 1993.
— Pp. 179–207.256. Modelling the labyrinth seal discharge coefficient using data miningmethods / T. Pychynski [et al.] // ASME Turbo Expo. — Glasgow,UK, 2010. — GT2010-22661.257. Modern reaction HP/IP turbine technology advances andexperiences / P. Hurd [et al.] // ASME Power Conference. —Chicago, Illinois, USA, 2005. — Pp. 425–435. — PWRC2005-50085.258. Moore J.















