A blade 30 at least part of which is arranged in use to rotate outside of a casing of a gas turbine engine 10. The blade 30 has a main body 32, a tip fence 36 and a blend region 40 defining a curve between the main body 32 and the fence 36. The blend region 40 has a radius of curvature below five inches and the fence 36 extends anhedrally from the blend region 40 with respect to the main body 32.
Rotor blade
Rotorblatt
Pale de rotor
19.10.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rotor blade, rotor, hovercar and preparation method of rotor blade
Europäisches Patentamt | 2023
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