Aircraft ice protection method
First Claim
1. A method of protecting an airfoil from undue ice accumulation during flight, said method comprising delay-rectifying steps for removing delay-induced ice accumulation and routine-deicing steps performed after the delay-rectifying steps;
- wherein the delay-rectifying steps and the routine-deicing steps are performed by an electrothermal device comprising a parting strip (PS) and at least a first set of spanwise-aligned deicing zones, the parting strip (PS) being positioned to heat the leading edge region of the airfoil, the first zone set comprising an upper fore zone (UF1), a lower fore zone (LF1), an upper aft zone (UA1), and a lower aft zone (LA1);
wherein the delay-rectifying steps comprise;
for a first time period (t1)continuously heating the parting strip (PS),continuously heating the first upper fore zone (UF1),continuously heating the first lower fore zone (LF1),not heating the first upper aft zone (UA1),not heating the first lower aft zone (LA1),wherein the routine-deicing steps comprise;
continuously heating the parting strip (PS),intermittently heating the first upper aft zone (UA1),intermittently heating the first lower aft zone (LA1).
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Accused Products
Abstract
A method of removing a delay-induced ice accumulation (e.g., an ice cap) from an airfoil'"'"'s leading-edge region with a zoned electrothermal device. The method comprises delay-rectifying steps which are performed prior to routine-deicing steps. The delay-rectifying steps comprise continuously heating the parting strip (PS), continuously heating the upper fore zone (UF1), and continuously heating the lower fore zone (LF1). These steps efficiently and effectively remove the delay-induced ice accumulation, whereby routine deicing can be resumed.
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Citations
19 Claims
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1. A method of protecting an airfoil from undue ice accumulation during flight, said method comprising delay-rectifying steps for removing delay-induced ice accumulation and routine-deicing steps performed after the delay-rectifying steps;
wherein the delay-rectifying steps and the routine-deicing steps are performed by an electrothermal device comprising a parting strip (PS) and at least a first set of spanwise-aligned deicing zones, the parting strip (PS) being positioned to heat the leading edge region of the airfoil, the first zone set comprising an upper fore zone (UF1), a lower fore zone (LF1), an upper aft zone (UA1), and a lower aft zone (LA1); wherein the delay-rectifying steps comprise; for a first time period (t1) continuously heating the parting strip (PS), continuously heating the first upper fore zone (UF1), continuously heating the first lower fore zone (LF1), not heating the first upper aft zone (UA1), not heating the first lower aft zone (LA1), wherein the routine-deicing steps comprise; continuously heating the parting strip (PS), intermittently heating the first upper aft zone (UA1), intermittently heating the first lower aft zone (LA1). - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
Specification