Runback control
An ice protection system includes an aircraft surface and a gutter defined in the aircraft surface between raised rails. The gutter includes a mouth that narrows into a trailing portion of the gutter. The mouth is configured to channel water runback rivulets into the trailing portion of the gutter. The gutter can be a first gutter of a plurality of side by side gutters, each including a respective mouth narrowing into a respective trailing portion, wherein the gutters are separated from one another by respective rails.
1. An ice protection system comprising:
an aircraft surface; and
a gutter defined in the aircraft surface between raised rails, wherein the gutter includes a mouth that narrows into a trailing portion of the gutter, wherein the mouth is configured to channel water runback rivulets into the trailing portion of the gutter, wherein the gutter is a first gutter of a plurality of side by side gutters, each including a respective mouth narrowing in a direction from a leading edge to a trailing edge of the aircraft surface into a respective trailing portion, wherein the gutters are separated from one another by respective rails.
2. An ice protection system as recited in claim 1 , wherein the aircraft surface is a surface of an airfoil, wherein the airfoil includes a leading edge and a trailing edge with the aircraft surface extending at least part way between the leading edge and the trailing edge.
3. An ice protection system as recited in claim 1 , wherein the aircraft surface includes at least one of a parting strip or a shedding zone forward of the mouth of the gutter.
4. An ice protection system as recited in claim 1 , wherein the gutter includes at least one of an ice phobic or hydrophobic surface material for prevention of ice formation in the gutter.
5. An ice protection system as recited in claim 1 , wherein the gutter includes a heater configured to locally heat the gutter for prevention of ice formation in the gutter.
6. An ice protection system as recited in claim 1 , wherein the gutter terminates at a tube leading under a wing surface for removing water to a drain either through natural or induced suction, wherein the tube is heated to prevent freezing.
7. An ice protection system comprising:
an aircraft surface; and
a gutter defined in the aircraft surface between raised rails, wherein the gutter includes a mouth that narrows into a trailing portion of the gutter, wherein the mouth is configured to channel water runback rivulets into the trailing portion of the gutter, wherein the trailing portion of the gutter terminates at a protrusion that protrudes above an area of the aircraft surface adjacent to the protrusion for shedding a runback rivulet away from the aircraft surface.
8. An ice protection system as recited in claim 1 , wherein the gutter has a depth of between 0.0005 inches to 0.007 inches relative to the rails.
9. An ice protection system as recited in claim 1 , wherein each gutter includes a respective heater configured to locally heat the gutter for prevention of ice formation in the gutter.
10. An ice protection system as recited in claim 9 , wherein the heaters of the gutters are spaced apart so areas of the aircraft surface between the gutters is free of heaters.
11. An ice protection system as recited in claim 1 , wherein the aircraft surface is configured to be mounted to an airframe over an underlying aerodynamic surface.
12. An ice protection system as recited in claim 1 , wherein the aircraft surface is formed directly as an aerodynamic surface of an air frame.
13. An ice protection system as recited in claim 1 , wherein the aircraft surface is configured as part of at least one of a wing, empennage, a cowl, a propeller or fan blade, a canard, or a windshield.