Structural cover for gas turbine engine bolted flanges
A method enables a structural cover for a gas turbine engine (10) to be manufactured. The method includes forming a torroidial body (52) including an integrally-formed windage cover portion (70) and a seal flange portion (72), and forming a plurality of fastener openings (92) extending from a forwar...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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