Side discharge anti-ice manifold

Power plants – Combustion products used as motive fluid – With safety device

Patent

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Details

244134R, F02G 300, B64D 1500

Patent

active

052207854

ABSTRACT:
An improved anti-ice manifold for a gas turbine engine is formed as a separate toroidal manifold arranged to be mounted forward of the inlet guide vanes. Axial discharge holes connect the manifold to interior passages in the inlet guide vanes for conveying heated gas thereto. An integral static pressure duct may also be provided in the manifold.

REFERENCES:
patent: 2474258 (1949-06-01), Kroon
patent: 3123283 (1964-03-01), Leis
patent: 4047379 (1977-09-01), Brookes et al.
patent: 5029440 (1991-07-01), Graber et al.

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