Диссертация (785882), страница 70
Текст из файла (страница 70)
J. Three-dimensional CFD rotordynamic analysis of gaslabyrinth seals // Journal of Vibration and Acoustics. — 2003. —Vol. 125. — Pp. 427–433.436Список литературы259. Moore J. J., Ransom D. L., Viana F. Rotordynamic force predictionof centrifugal compressor impellers using computational fluiddynamics // Journal of Engineering for Gas Turbines and Power. —2011. — Vol. 133. — P. 042504.260. Morton P.
G. Unstable shaft vibrations arising from thermal effectsdue to oil shearing between stationary and rotating elements //IMechE Ninth International Conference on Vibrations in RotatingMachinery. — University of Exeter, UK, 2008. — Pp. 383–392.261. Moser R. D., Kim J., Mansour N.
N. Direct numerical simulation ofturbulent channel flow up to Re = 590 // Physics of Fluids. —1999. — Vol. 11, no. 4. — Pp. 943–945.262. MTU Aero Engines GmbH Press Release. Brush seals. — 2014. —URL: http://www.mtu.de/news-media/press/presskits/press-kit-ila-2014/ (visited on 09/21/2015).263. Multiple row brush seal testing for steam turbine applications withhigh temperature and high pressure conditions and long serviceintervals / T.
Osterhage [et al.] // 6th European Conference onTurbomachinery. — Lille, France, 2005. — 096 05/57.264. Murphy B. T., Lorenz J. A. Simplified Morton effect analysis forsynchronous spiral vibrations // Journal of Vibration andAcoustics. — 2010. — Vol. 132. — Pp. 051008–7.265. Muszynska A. Rotordynamics. — Boca Raton : Taylor & Francis,2005. — 1075 pp.266.
NASA 2007 NASA Seal/Secondary Air System Workshop:tech. rep. / NASA. — 2008. — NASA/CP-2008-215263/VOL1.267. Negative stiffness in gas turbine leaf seals / I. H. J. Jahn [et al.] //ASME Turbo Expo. — Vancouver, Canada, 2011. — GT2011-46483.268. Nelson H. D., McVaugh J. M. The dynamics of rotor-bearingsystems using finite elements // Journal of Engineering forIndustry.
— 1976. — Vol. 98. — Pp. 593–600.437Список литературы269. Neural network and CFD-based optimization of square cavity andcurved cavity static labyrinth seals / S. P. Asok [et al.] // TribologyInternational. — 2007. — Vol. 40. — Pp. 1204–1216.270. Niu M. C.-Y. Airframe Structural Design. Practical DesignInformation and Data on Aircraft Structures. — 2nd ed. — ADAdaso/Adastra Engineering LLC, 1999.271. Nonlinear transient finite element analysis of rotor-bearing-statorsystems / J. Padovan [et al.] // Journal of Computers andStructures. — 1984. — Vol. 18. — Pp. 629–639.272. Non-metallic brush seals for gas turbine bearings / N. Bhate[et al.] // ASME Turbo Expo.
— Vienna, Austria, 2004. —GT2004-54296.273. Nordmann R., Dietzen F., Weiser H. Calculation of rotordynamiccoefficients and leakage for annular gas seals by means of finitedifference techniques // Journal of Tribology. — 1989. —Vol. 111. — Pp. 545–552.274. Nordmann R., Massmann H. Identification of dynamic coefficients ofannular turbulent seals // Rotordynamic Instability Problems inHigh-Performance Turbomachinery. — Texas A&M University,USA, 1984. — Pp.
295–311.275. Numerical investigation of leakage and power loss for different sealtypes in turbine stage environment / R. Yang [et al.] // ASMETurbo Expo. — Glasgow, UK, 2010. — GT2010-22743.276. Nunez D., Ransom D., Prueger G. Brush seal arrangement for theRS-68 turbopump set // Seals/Secondary Fluid Flows Workshop. —Cleveland, OH, USA, 1997.
— NASA/CP—2006-214320/VOL1.277. OpenFOAM User Guide / OpenFOAM Foundation. — Release2.2.2, 2013.438Список литературы278. Pai S., Riha D. Model verification and validation concepts for aprobabilistic fracture assessment model to predict cracking of knifeedge seals in the Space Shuttle Main Engine high pressureoxidizer // ASME Turbo Expo. — Copenhagen, Denmark, 2012. —GT2012-70132.279.
Patankar S. V. Numerical heat transfer and fluid flow. —Washington : Hemisphere Publishing Corporation, 1980. — 197 pp.280. Pekris M. J., Franceschini G., Gillespie D. R. H. An investigation offlow, mechanical and thermal performance of conventional andpressure-balanced brush seals // ASME Turbo Expo. —Copenhagen, Denmark, 2012. — GT2012-68901.281. Pekris M. J., Franceschini G., Gillespie D. R. H. Effect of geometricchanges in an idealised contacting brush seal bristle pack on typicalkey performance measures // ASME Turbo Expo.
— Vancouver,Canada, 2011. — GT2011-46492.282. Pfefferle D., Dullenkopf K., Bauer H.-J. Design and validation of anew test rig for brush seal testing under engine relevant conditions //ASME Turbo Expo. — Vancouver, Canada, 2011. — GT2011-45107.283. Picardo A.
M. High Pressure Testing of Labyrinth Seals: MSThesis / Picardo A. M. — College Station, TX, USA : Texas A&MUniversity, 2003.284. Picardo A., Childs D. W. Rotordynamic coefficients for atooth-on-stator labyrinth seal at 70 bar supply pressures:measurements versus theory and comparisons to a hole-patternstator seal // Journal of Engineering for Gas Turbines and Power. —2005. — Vol. 127. — Pp. 843–855.285. Povinelli V. P. Current seal designs and future requirements forturbine engine seals and bearings // Journal of Aircraft. — 1975. —Vol. 12, no.
4. — Pp. 266–273.439Список литературы286. Prediction of stiffness coefficients for foil air bearings to performrotordynamic analysis of turbomachinery / Y. A. Ravikovich[et al.] // 9th IFToMM International Conference on RotorDynamics. — 2015. — Pp. 1277–1288. — DOI:10.1007/978-3-319-06590-8\_104.287. Preliminary experimental results for a cryogenic brush sealconfiguration / J. A. Carlile [et al.] // 29thAIAA/SAE/ASME/ASEE Joint Propulsion Conference andExhibit.
— Monterey, CA, USA, 1993. — AIAA-93-2535.288. Pressure activated leaf seal technology readiness testing /A. Bowsher [et al.] // ASME Turbo Expo. — Düsseldorf, Germany,2014. — GT2014-27046.289. Prior R., Short J., Basu P. Brush seal wear model // 34thAIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit.
— Cleveland, OH, USA, 1998. — AIAA 98-3170.290. Proctor M. P., Delgado I. R. Leakage and power loss test results forcompeting turbine engine seals // ASME Turbo Expo. — Vienna,Austria, 2004. — GT2004-53935.291. Proctor M. P., Delgado I. R. Preliminary test results of anon-contacting finger seal on a herringbone-grooved rotor // 44thAIAA/ASME/SAE/ ASEE Joint Propulsion Conference &Exhibit. — Hartford, CT, USA, 2008. — AIAA2008-4506.292. Proctor M.
P., Kumar A., Delgado I. R. High-speed,high-temperature finger seal test results // 38thAIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit. — Indianapolis, IN, USA. 2002. — AIAA2002-3793.293. Pugachev A. O. Aggregation of experimental and theoretical data forbrush seal leakage evaluation // 50th AIAA/ASME/SAE/ASEEJoint Propulsion Conference. — Cleveland, OH, USA, 2014. — DOI:10.2514/6.2014-3598. — AIAA 2014-3598.440Список литературы294. Pugachev A. O. Application of gradient-based optimization methodsfor a rotor system with static stress, natural frequency, and harmonicresponse constraints // Structural and MultidisciplinaryOptimization.
— 2013. — Vol. 47, no. 6. — Pp. 951–962. — DOI:10.1007/s00158-012-0867-4.295. Pugachev A. O. CFD optimization of liquid annular seals for leakageand rotordynamics improvement // ASME Turbo Expo. — Orlando,FL, USA, 2009. — DOI: 10.1115/GT2009-59173. — GT2009-59173.296. Pugachev A. O. Predicted performance of brush seals: porousmedium versus resolved bristle matrix and comparison withexperimental data // 10th European Conference onTurbomachinery. — Lappeenranta, Finland, 2013. —Pp. 160–170. — Paper 054.297. Pugachev A. O., Deckner M.
Analysis of the experimental andCFD-based theoretical methods for studying rotordynamiccharacteristics of labyrinth gas seals // ASME Turbo Expo. —Glasgow, Scotland, UK, 2010. — DOI: 10.1115/GT2010-22058. —GT2010-22058.298. Pugachev A. O., Deckner M. CFD prediction and test results ofstiffness and damping coefficients for brush-labyrinth gas seals //ASME Turbo Expo. — Glasgow, Scotland, UK, 2010. — DOI:10.1115/GT2010-22667.299. Pugachev A.
O., Deckner M. Experimental and theoreticalrotordynamic stiffness coefficients for a three-stage brush seal //Mechanical Systems and Signal Processing. — 2012. — Vol. 31. —Pp. 143–154. — DOI: 10.1016/j.ymssp.2012.03.015.300. Pugachev A. O., Deckner M. Shape optimization of a labyrinth seal:leakage minimization and sensitivity of rotordynamic coefficients //IMechE Ninth International Conference on Vibrations in RotatingMachinery.
— University of Exeter, UK, 2008. — Pp. 849–859. —C663/029/08.441Список литературы301. Pugachev A. O., Degen H. CFD-predicted rotordynamic coefficientsfor a 20-teeth-on-stator labyrinth seal at high supply pressureconditions // ASME Turbo Expo. — Copenhagen, Denmark,2012. — DOI: 10.1115/GT2012-68381. — GT2012-68381.302. Pugachev A. O., Helm P. Calibration of porous medium models forbrush seals // Proceedings of the Institution of MechanicalEngineers, Part A: Journal of Power and Energy.
— 2009. —Vol. 223, no. 1. — Pp. 83–91. — DOI: 10.1243/09576509JPE641.303. Pugachev A. O., Kleinhans U., Gaszner M. Prediction ofrotordynamic coefficients for short labyrinth gas seals usingcomputational fluid dynamics // Journal of Engineering for GasTurbines and Power. — 2012. — Vol. 134, no. 6. —Pp. 062501–10. — DOI: 10.1115/1.4005971.304. Pugachev A. O., Ravikovich Y. A., Savin L. A. Flow structure in ashort chamber of a labyrinth seal with a backward-facing step //Computers & Fluids. — 2015. — Vol.
114. — Pp. 39–47. — DOI:http://dx.doi.org/10.1016/j.compfluid.2015.02.015.R305. PurePower○PW 1000G engine: tech. rep. / MTU Aero EnginesGmbH. — 2014. — 2 pp.306. Relative comparison between baseline labyrinth and dual-brushcompressor discharge seals in a T-700 engine test / R. C. Hendricks[et al.] // 39th International Gas Tubine and Aeroengine Congressand Exposition. — Hague, The Netherlands, 1994. — NASA TM106360, ARL-MR-232.307.
Rhode D. L., Hensel S. J., Guidry M. J. Labyrinth seal rotordynamicforces using a three-dimensional Navier-Stokes code // Journal ofTribology. — 1992. — Vol. 114. — Pp. 683–689.308. Rhode D. L., Ko S. H., Morrison G. L. Leakage optimization oflabyrinth seals using a Navier–Stokes code // TribologyTransactions. — 1994. — Vol.
37, no. 1. — Pp. 105–110.442Список литературы309. Rotordynamic coefficients and leakage flow of parallel grooved sealsand smooth seals / R. Nordmann [et al.] // Rotordynamic InstabilityProblems in High-Performance Turbomachinery. — Texas A & MUniversity, USA, 1986. — Pp. 129–153.310. Rotordynamic coefficients of labseals for turbines—comparing CFDresults with experimental data on a comb–grooved labyrinth /J. Schettel [et al.] // ASME Turbo Expo. — Reno-Tahoe, NV, USA,2005. — GT2005-68732.311. Roy B., Deo H.
V., Zheng X. Progressive clearance labyrinth seal forturbo-machinery applications // ASME 2011 InternationalMechanical Engineering Congress & Exposition. — Denver, CO,USA, 2011. — IMECE2011-64870.312. Ruggiero E. J. Experimental results from a sensor brush seal // 46thAIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit. — Nashville, TN, USA, 2010. — AIAA2010-6830.313. Ruggiero E.
![](https://s.studizba.com/z.php?f=/templates/si/i/noavatar.png&w=100&h=100&t=1"){kind=avatar}
