Fairing for a turbine frame strut

摘要

A fairing (60) for use with a gas turbine frame strut. The fairing is cast as an integral single piece comprising a first sidewall (80) and a second sidewall (82) connected together at a leading edge (84) and a trailing edge (86), such that at least one cooling chamber (88) is defined therebetween. The fairing comprises at least one partition (94) and at least one parting line (140). The at least one partition is formed integrally with and extends between the first and second sidewalls, at least one parting line divides said fairing into a forward portion (144) and a separate aft portion (146) which are removably coupled together.