| CPC F01D 25/16 (2013.01) [B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F01D 25/125 (2013.01); F16C 33/667 (2013.01)] | 17 Claims |

|
1. A bearing cap for a gas turbine engine, the bearing cap comprising:
a first surface on a first side, wherein the first surface is annular around a longitudinal axis;
a second surface on a second side that is opposite and downstream from the first side, wherein the second surface is annular around the longitudinal axis;
one or more air insulation cavities between the first surface and the second surface, wherein each of the one or more air insulation cavities is annular around the longitudinal axis; and
an annular mixed air cavity upstream from the one or more air insulation cavities.
|