High load capacity bi-directional tapered roller bearing

In a gas turbine engine, the engine including non-rotating structure and having a shaft supported from and rotatable within said structure, said shaft having at least one compressor disk fixedly secured to one end of said shaft and at least one turbine disk fixedly secured to the other end of said shaft, a bi-directional tapered roller bearing disposed on one end of said shaft for facilitating the rotation of said shaft and for transferring both primary and reverse axial thrust loads to said structure, said roller bearing including:

• (a) a cup having an annular race tapered such that said cup race has a large diameter end and a small diameter end;
• (b) a cone having an annular race spaced radially inwardly from said cup race, said cone race being tapered such that said cone race has a large diameter end and a small diameter end;
• (c) a plurality of tapered roller elements, each having a rolling surface, a small diameter end face at one end of said rolling surface, and a large diameter end face at the other end of said rolling surface, said roller elements being circumferentially spaced apart in a single row between said cup race and cone race and contacting said races along said rolling surfaces;
• an improvement wherein said bearing further comprises:
• (i) a cup thrust rib ring fixed relative to said cup, said cup thrust rib ring having an annular thrust face “A” at said large diameter end of said cup race and extending radially inwardly therefrom, said large diameter end face of each of said roller elements being disposed adjacent and facing thrust face A;
• (ii) a first cone thrust rib ring fixed relative to said cone, said first cone thrust rib ring having an annular thrust face “C” at said small diameter end of said cone race and extending radially outwardly therefrom, said small diameter end face of each of said roller elements being disposed adjacent and facing thrust face C, said thrust faces A and C being moveable into load bearing contact with, respectively, said large diameter end face of each of said rollers and said small diameter end face of each of said rollers upon the application of reverse axial thrust loads on said cup and cone that urge said cup race and said cone race further apart;
• and
• (iii) a second cone thrust rib ring fixed relative to said cone, said second cone thrust rib ring having an annular thrust face “B” at said large diameter end of said cone race and extending radially outwardly therefrom, said large diameter end face of each of said roller elements being disposed adjacent and facing thrust face B, the distance between thrust faces B and C being greater than the length of said rollers, said thrust face B being moveable into load bearing contact with said large diameter end face of each of said roller elements upon the application of primary axial thrust loads on said cup and said cone that urge said cup race and said cone race closer together.