Gas turbine bearing support housing for the engine (10) (36) comprises in the order of radially outward from the center, an inner ring (50) defining a central bore (46), an array of inner slots (60) an intermediate ring (58), an outer web comprising an array of outer slots (64) (62), provided with inner slots and the outer slots, extending intermediate ring (58) and outer webs (62) tangentially beam positioned so as to divide the inner and outer struts extending array and radial (70), it is sized and shaped, the bearing support housing (36) further comprises an outer ring (66).
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