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Title
Authors
Construction of a promising face gas-dynamic seal of the aircraft engine
Bondarchuk P.V., Falaleev S.V.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Numerical investigetion of a non-contacting finger seal
Temis Y.M., Selivanov A.V., Dzeva I.Y.
Thermal deformation influence to cryogenic pumps seals operability
Ivanov A.V.
Topical issues of gas turbine engine friction unit reliability
Parovay Y.F., Ibatullin I.D.
Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes
Vinogradov A.S., Badykov R.R., Shpakov I.D.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
An experimental study of the influence of valve drive type on the dynamic loading and service life of valve seals of units
Kondrashov Y.I., Ermilova E.N., Vidyaskina A.N.
Research of serviceability of pulsed face seals with pumpback structures
Vinogradov A.S., Badykov R.R., Anokhin D.V.
Experimental research of shaft sealing with elastic element made of MR material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
Dynamik experimental researches of the face gas dynamic seal
Novikov D.K., Balyakin V.B., Sedov V.V.
Improving the reliability of radial face seals of aircraft engine rotor supports
Falaleev S.V., Bondarchuk P.V., Ibatullin I.D., Badykov R.R.
Building a diagnosis face gas dynamic seals
Falaleev S.V., Vinogradov I.S., Midyukin V.V.
Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants
Vinogradov A.S.
Analysis of radial gaps changing dynamics of the pump and turbine rocket engine turbopumps
Ivanov A.V.
Research of shaft seals made of porous wire «metal rubber» material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V., Ardakov A.Y., Osipov A.A.
Modeling flow in a ring body work o-gap-state rocket engine turbopump
Ivanov A.V., Moskvichev A.V., Tsiganov A.A.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Unification of the design of gasdynamic seal
Falaleev S.V., Sedov V.V., Midyukin V.V.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Study of seals influence to supercritical rotor characteristic
Ivanov A.V.
Rotor-vane compressor with working chambers contactless condensation optimizations variants
Kolomin I.V., Dovgjallo A.I., Galperin R.N., Gulyaev L.Y., Logashkin A.P.
Study of gradient rotor speed and support dissipation coefficient influence to supercritical rotor characteristic
Ivanov A.V.
Reduction the influence of geometric axes of the skew elements of a pair of valve-saddle on the sealing ability and resource of the valveseal
Mulyukin O.P., Samsonov V.N., Kshumanev S.V.
EDM laser alloying and texturing the sliding surface mechanical seals
Antoshevskiy B., Tarelnik V.B., Martsinkovskiy V.S.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals
Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.
Investigation of the influence of non-axisymmetric elements in secondary air system on gas turbine engine flow parameters, the temperature field and deformation of components
Tisarev A.Y., Vasilevich N.M.
Formation of the sliding surface mechanical seal different methods
Tarelnik V.B., Martsinkovskiy V.S., Antoshevskiy B.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
1 - 32 of 32 Items

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