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(11) | EP 2 410 136 A3 |
(12) | EUROPEAN PATENT APPLICATION |
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(54) | Vortex reducing device for a gas turbine engine |
(57) A gas turbine engine (12) has a vortex reducing device (20) therein that includes
a retainer (30) and paddles (32). The retainer is arcuate in shape and has a plurality
of circumferentially spaced slots (46) that extend through it. The paddles are circumferentially
spaced about the retainer and extend outward therefrom. Each paddle is disposed between
adjacent slots.
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