Method of manufacturing a heat shield for a fuel manifold

Details Method of manufacturing a heat shield for a fuel manifold Method of manufacturing a heat shield for a fuel manifold

B - Operations, Transporting

23

P

B23P 15/00 (2006.01) F02C 7/22 (2006.01) F02C 7/24 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2604278

A method of manufacturing a heat shield for a manifold ring of a gas turbine engine, comprising forming a tubular portion of heat shield material with an arcuate longitudinal axis, deforming the tubular portion such that a cross-section thereof defines a profile corresponding to at least two complementary heat shield portions configured to cooperate to significantly surround at least a circumferential portion of the manifold ring, and cutting the tubular portion to divide the tubular portion into each of the heat shield portions.

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