Aircraft anti-icing systems having deflector vanes
作者： Daniel H. Gally , Rick A. Johnson , Edward Charles Natsui , Victor D. Pham , Joseph James Seydel
DOI:
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摘要: Apparatus and methods to lower peak temperatures improve performance of aircraft anti-icing systems are described herein. One example apparatus includes a skin on an inlet side nacelle defining annular chamber, gas delivery system disposed within the chamber provide first mix with entrain second in define flow through deflector vane redirect chamber. The is at different temperature from gas.
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