Gas turbine engine frame assembly

摘要

A fairing for mounting onto a gas turbine frame to isolate the frame from the hot gases passing the flowpath. The fairing includes mating forward and aft annular sections with each section having an outer wall and an inner wall defining the flowpath therebetween. A plurality of circumferentially-spaced hollow fairing struts radially extends between the inner and outer walls. The two sections are manufactured such that there are no misalignments or steps between the lineup of the two sections. The sections are placed over the frame struts and are coupled together.