Impermeable, abradable seal and method for the production thereof
AssigneeTechnetics Corporation
InventorsGregory P. Jarrabet, Lixion Lu
Life of this patent
Estimating the term…
Loading patent…
AssigneeTechnetics Corporation
InventorsGregory P. Jarrabet, Lixion Lu
Estimating the term…
Gas turbine engines employ a variety of abradable liners to decrease the clearance between the rotating components and the surrounding casing. There is normally a trade-off between porosity, (and concomitant permeability) and the abradability of the liner material, such that materials with good abradability are permeable to gas flow--resulting in performance losses. Permeability of porous liners is decreased by infiltrating the liner with a low-viscosity liquid containing a metal or metal oxide. After infiltration, the viscosity of the liquid is substantially increased to prevent its egress from the porous liner. Thereafter, the liner is heated at an elevated temperature to drive off the remaining liquid and provide an oxide which blocks the passages and decreases the permeability of the liner.
In the production of an abradable liner material, comprising a rigid, skeleton-like matrix, the pores of which are at least partially filled with a metal or metal compound, to substantially decrease the permeability of the liner under the high temperature applications encountered in such turbomachinery, the improvement which comprises,
Dependencies are inferred from the claim text.