Guide vane assembly for a gas turbine engine

摘要

A guide vane assembly for a gas turbine engine includes a plurality of circumferentially-spaced guide vanes (502) including at least a first, a second, and a third guide vane (532, 534, 536). The second guide vane is positioned between the first and third guide vanes. The plurality of guide vanes is oriented such that a first circumferential spacing (540) is defined between the first and second guide vanes and a second circumferential spacing (542) is defined between the second and third guide vanes. The second circumferential spacing is different from the first circumferential spacing.