Components for a gas turbine engine
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United States of America Patent
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Dec 21, 2010
Issued Date -
N/A
app pub date -
Aug 15, 2007
filing date -
Sep 12, 2006
priority date (Note) -
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Abstract
An aerofoil assembly including an aerofoil and a spray element that supplies fluid to a gas turbine engine. The aerofoil has a first part with a leading edge when located in the gas turbine engine, and a second part with a trailing edge when located in the gas turbine engine. The first part has features that slide relative to and engage with complementary features of the second part to form a releasable arrangement.
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