136880 ⎘
Preventing or minimising internal leakage of working-fluid, e.g. between stages; Sealing means between non relatively rotating elements; Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
Axial-flow thermal turbomachine
#302Methods and apparatus for assembling gas turbine engine rotor assemblies
#303Turbine blade nested seal damper assembly
#304Gas turbine rotor
#305Skirted turbine blade
#306Lightened interblade platform for a turbojet blade support disc
#307Inter-vane platform with lateral deflection for a vane support of a turbine engine
#308Rotor assembly and annulus filler for gas turbine engine compressor
#309Nozzle guide vanes
#310Turbine blade arrangement
#311Moving blade and gas turbine using the same
#312Seal device
#313Control of leak zone under blade platform
#314Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors
#315Sealing arrangement for a rotor of a turbo machine
#316Blade damper
#317Inter-vane platform with flexible securing pins and variable shear stresses for a support disk for the vanes of a turbine engine
#318Sealing arrangement
#319Stiffness coupling and vibration damping for turbine blade shroud
#320Platform for an airfoil of a gas turbine engine