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Title
Authors
Construction of a promising face gas-dynamic seal of the aircraft engine
Bondarchuk P.V., Falaleev S.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.
Study of seals influence to supercritical rotor characteristic
Ivanov A.V.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
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.
EDM laser alloying and texturing the sliding surface mechanical seals
Antoshevskiy B., Tarelnik V.B., Martsinkovskiy V.S.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
Analysis of radial gaps changing dynamics of the pump and turbine rocket engine turbopumps
Ivanov A.V.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Formation of the sliding surface mechanical seal different methods
Tarelnik V.B., Martsinkovskiy V.S., Antoshevskiy B.
Thermal deformation influence to cryogenic pumps seals operability
Ivanov A.V.
Unification of the design of gasdynamic seal
Falaleev S.V., Sedov V.V., Midyukin V.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.
Numerical investigetion of a non-contacting finger seal
Temis Y.M., Selivanov A.V., Dzeva I.Y.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
Study of gradient rotor speed and support dissipation coefficient influence to supercritical rotor characteristic
Ivanov A.V.
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.
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.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
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.
Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants
Vinogradov A.S.
Topical issues of gas turbine engine friction unit reliability
Parovay Y.F., Ibatullin I.D.
Building a diagnosis face gas dynamic seals
Falaleev S.V., Vinogradov I.S., Midyukin V.V.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
1 - 28 of 28 Items

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