Диссертация (785882), страница 68
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— 1952. — Vol. 48. — Pp. 89–94.161. Ertas B. H., Vance J. M. Rotordynamic force coefficients for a newdamper seal design // Journal of Tribology. — 2007. — Vol. 129. —Pp. 365–374.162. Ertas B., Delgado A., Vannini G. Rotordynamic force coefficients forthree types of annular gas seals with inlet preswirl and highdifferential pressure ratio // Journal of Engineering for Gas Turbinesand Power. — 2012. — Vol. 134. — Pp.
042503–12.163. Eser D. Rotordynamic coefficients in stepped labyrinth seals //Computer Methods in Applied Mechanics and Engineering. —2002. — Vol. 191. — Pp. 3127–3135.164. Eser D., Kazakia J. Y. Air flow in cavities of labyrinth seals //International Journal of Engineering Science. — 1995. — Vol. 33(15).
— Pp. 2309–2326.165. Eshleman R. L., Eubanks R. A. On the critical speeds of acontinuous rotor // Journal of Engineering for Industry. — 1969. —Vol. 91. — Pp. 1180–1188.166. Evaluation of flow behaviour for clearance brush seals / Y. Dogu[et al.] // Journal of Engineering for Gas Turbines and Power. —2008.
— Vol. 130. — Pp. 012507–9.167. Experimental characterisation of the stiffness and leakage of aprototype leaf seal for turbine appplications / I. H. J. Jahn [et al.] //ASME Turbo Expo. — Berlin, Germany, 2008. — GT2008-51206.426Список литературы168. Experimental characterization of variable bristle diameter brush sealleakage, stiffness and wear / D. Trivedi [et al.] // ASME TurboExpo. — San Antonio, TX, USA, 2013. — GT2013-95086.169. Experimental investigation of a leaf seal prototype atengine-representative speeds and pressures / M. J. Pekris [et al.] //ASME Turbo Expo. — Montreal, Canada, 2015.
— GT2015-43231.170. Experimental results of an aramid fiber brush seal for high-powerdensity, liquid-cooled, rotating electric machines / W. D. Gerstler[et al.] // 48th AIAA/ASME/SAE/ASEE Joint PropulsionConference & Exhibit. — Atlanta, GA, USA, 2012. — AIAA2012-4005.171. Fellenstein J. A., DellaCorte C. Preliminary tuft testing of metallicbristles versus PS212, PS300, and HVOF300 // STLE AnnualMeeting. — Detroit, MI, USA, 1998.
— NASA TM-107522.172. Ferguson J. G. Brushes as high performance gas turbine seals //ASME Gas Turbine and Aeroengine Congress and Exposition. —Amsterdam, The Netherlands, 1988. — 88-GT-182.173. Finite element modeling and vibration analysis of a free powerturbine subjected to non-synchronous excitation / A. O. Pugachev[et al.] // 9th IFToMM International Conference on RotorDynamics. — 2015. — Pp.
1875–1886. — DOI:10.1007/978-3-319-06590-8\_155.174. Fleming D. P. Damping in tapered annular seals for anincompressible fluid: tech. rep. / NASA. — 1980.175. Fleming D. P. High stiffness seals for rotor critical speed control:tech. rep. / ASME. — 1977.176. Flitney R. K. Seals and sealing handbook. — 5th ed. —Amsterdam : Elsevier, 2007. — 620 pp.177. Flower R. Brush seal development system // 26thAIAA/SAE/ASME/ASEE Joint Propulsion Conference.
—Orlando, FL, USA, 1990. — AIAA-90-2143.427Список литературы178. Franceschini G., Jones T., Gillespie D. The development of a largeradial movement brush seal // ASME Turbo Expo. — Copenhagen,Denmark, 2012. — GT2012-68891.179. Franceschini G., Jones T. V., Gillespie D. R.
H. Improvedunderstanding of blow-down in filament seals // Journal ofTurbomachinery. — 2010. — Vol. 132. — Pp. 041004–10.180. Fundamental design issues of brush seals for industrial applications /S. Dinc [et al.] // Journal of Turbomachinery. — 2002. —Vol. 124. — Pp. 293–300.181.
Gail A., Beichl S. MTU brush seal—main features of an alternativedesign // 36th AIAA/ASME/SAE/ASEE Joint PropulsionConference & Exhibit. — Huntsville, AL, USA, 2000. — AIAA2000-3375.182. Gail A., Beichl S. The MTU brush seal design: tech.
rep. / MTU. —2006.183. Gamal A. J. M., Vance J. M. Labyrinth seal leakage tests: toothprofile, tooth thickness, and eccentricity effects // Journal ofEngineering for Gas Turbines and Power. — 2008. — Vol. 130. —Pp. 0125510–11.184. Gaszner M., Pugachev A. O. Experimental techniques fordetermining rotordynamic coefficients of gas seals: results for shortstaggered labyrinth seals and comparison with CFD // IMechETenth International Conference on Vibrations in RotatingMachinery. — London, UK, 2012. — Pp. 455–466. — C1326/019.185. Gradient-based optimization of a turboprop rotor system withconstraints on stresses and natural frequencies / A.
O. Pugachev[et al.] // 6th AIAA Multidisciplinary Design OptimizationSpecialist Conference. — Orlando, FL, USA, 2010. — DOI:10.2514/6.2010-3006. — AIAA 2010-3006.428Список литературы186. Grondahl C. Pressure actuated leaf seal feasibility study anddemonstration // 45th AIAA/ASME/SAE/ASEE Joint PropulsionConference & Exhibit. — Denver, CO, USA, 2009. — AIAA2009-5167.187. Grondahl C.
Pressure actuated leaf seals for improved turbine shaftsealing // 41st AIAA/ASME/SAE/ASEE Joint PropulsionConference & Exhibit. — Tucson, AZ, USA, 2005. — AIAA2005-3985.188. Grondahl C. M., Dudley J. C. Film riding leaf seals for improvedshaft sealing // ASME Turbo Expo. — Glasgow, UK, 2010. —GT2010-23629.189. Guardino C., Chew J. W. Numerical simulation of three-dimensionalbristle bending in brush seals // Journal of Engineering for GasTurbines and Power. — 2005. — Vol. 127. — Pp. 583–591.190. Gutierrez J. L., Davis C.
L., Hawkes T. M. First full-scale engineevaluation of an IHPTET exhaust nozzle technology demonstrator //31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit. — San Diego, CA, USA, 1995. — AIAA 95-2747.191. Halila E. E., Lenahan D. T., Thomas T. T. Energy Efficient EngineHigh Pressure Turbine Test Hardware Detailed Design Report:tech. rep. / NASA. — 1982. — NASA CR-167955.192.
Handbook of Lubrication and Tribology. Volume 1. Application andMaintenance / ed. by G. E. Totten. — Taylor & Francis, 2006.193. Handbook of rotordynamics / ed. by F. F. Ehrich. — New York :McGraw-Hill, 1992.194. Hashimoto H., Matsumoto K. Improvement of operatingcharacteristics of high-speed hydrodynamic journal bearings byoptimum design: Part 1—Formulation of methodology and itsapplication to elliptical bearing design // Journal of Tribology. —2001. — Vol. 123. — Pp.
305–312.429Список литературы195. Hawthorne H. M. Brush-on-disc simulation tribo-testing of materialsfor gas turbine-compliant seal components // TribologyInternational. — 1994. — Vol. 27. — Pp. 87–95.196. Haynes International I. Haynes 25 alloy. — URL:http://www.haynesintl.com/pdf/h3057.pdf.197.
Heat generation characteristics of a Kevlar(r) fiber brush seal /E. J. Ruggiero [et al.] // 43rd AIAA/ASME/SAE/ASEE JointPropulsion Conference & Exhibit. — Cincinnati, OH, USA, 2007. —AIAA 2007-5738.198. Helm P., Pugachev A. O., Neef M. Breaking the swirl with brushseals: numerical modeling and experimental evidence // ASMETurbo Expo.
— Berlin, Germany, 2008. — DOI:10.1115/GT2008-50257. — GT2008-50257.199. Helm P., Spliethoff H., Neef M. Closing the gap: measuring bristleblow down of brush seals // 19th International Conference on FluidSealing. — Poitiers, France, 2007.200. Herrmann N., Dullenkopf K., Bauer H.-J. Flexible seal strip designfor advanced labyrinth seals in turbines // ASME Turbo Expo.
—San Antonio, TX, USA, 2013. — GT2013-95424.201. Heshmat H., Walton I. J. Innovative high-temperature compliantsurface foil face seal development // 44th AIAA/ASME/SAE/ASEEJoint Propulsion Conference & Exhibit. — Hartford, CT, USA,2008. — AIAA2008-4505.202. High speed characterization of a prototype leaf seal on an advancedseal test facility / M. J. Pekris [et al.] // ASME Turbo Expo. —Montreal, Canada, 2015.
— GT2015-43465.203. Hilfer M., Hogg S., Ingram G. Experimental validation of a curtaintype fluidic jet seal on a turbine rotor shroud // ASME TurboExpo. — Montreal, Canada, 2015. — GT2015-42624.430Список литературы204. Hirano T., Guo Z., Kirk R. Application of computational fluiddynamics analysis for rotating machinery—Part II: Labyrinth sealanalysis // Journal of Engineering for Gas Turbines and Power. —2005. — Vol. 127. — Pp. 820–826.205.
Hirs G. G. A bulk-flow theory for turbulence in lubricant films //Journal of Lubrication Technology. — 1973. — Vol. 95. —Pp. 137–146.206. Hogg S. I., Gomez Ruiz I. Fluidic jet barriers for sealingapplications // ASME Turbo Expo. — Vancouver, Canada, 2011. —GT2011-45353.207. Holle G. F., Chupp R. E., Dowler C.















