Rotor blade for a gas turbine engine and method of designing an airfoil
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Grantee
United Technologies Corporation
Representative
Application number
EP09252818B1
Kind
B1
Document number
2199543
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Rotor blade for a gas turbine engine and method of designing an airfoil

2199543 - EP09252818B1 - EPO

Application Dec 17, 2009 - Publication Feb 05, 2020

Jody Kirchner Sanjay S. Hingorani Yuan Dong

Description

Claims

Patent References

Patent Publication Date Title
EP90630254A1 14/08/1991 Airfoil for the compression section of a rotary machine
EP04254703A1 09/02/2005 Compressor airfoil
EP93305719A2 16/02/1994 A fan
EP00310798A2 13/06/2001 Double bowed compressor airfoil
EP07121584A2 11/06/2008 Advanced booster rotor blade
WO2009/103528A2 N/A N/A
1689681 06/06/2000 Swept fan blade
EP1505302A N/A N/A
EP1930598A N/A N/A
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