Fan blade anti-icing concept
AssigneePratt & Whitney Canada Corp.
InventorsRichard IVAKITCH, David MENHEERE, Paul STONE
Life of this patent
Estimating the term…
Loading patent…
AssigneePratt & Whitney Canada Corp.
InventorsRichard IVAKITCH, David MENHEERE, Paul STONE
Estimating the term…
A fan blade anti-icing system comprises a fan hub and a fan blade extending radially outwardly from the fan hub. The fan blade has a base and an airfoil extending radially outwardly from the fan base. The airfoil having a leading edge, a trailing edge, a convex side surface between the leading and trailing edge and a concave side surface between the leading and trailing edge. The fan blade further has a radial passage extending from a blade air inlet in the blade base in communication with a source of heated air, and a rearwardly directed passage in communication with the radial passage and having a blade air outlet forward of the trailing edge and oriented tangentially to the convex side surface or concave side surface of the airfoil.
A method of impeding icing on an airfoil surface of a fan blade of an aircraft engine, the method comprising:
A method of mitigating ice accretion on an airfoil surface of a fan blade of an aircraft engine, the method comprising:
Dependencies are inferred from the claim text.