Ice phobic material to reduce runback ice

Patent metadata

Field	Value
Publication number	US-10875632-B2
Application number	US-201715806516-A
Country	US
Kind code	B2
Filing date	Nov 8, 2017
Priority date	Nov 8, 2017
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

An ice protection assembly on an airfoil includes a heater positioned on the leading edge, and one or more ice phobic layers positioned to inhibit runback ice formation on the surface of the airfoil downstream of the heater.

First claim

The invention claimed is:

1. An ice protection assembly for aircraft, the ice protection assembly comprising:
an airfoil comprising:
a leading edge;
a trailing edge;
a first surface;
a second surface;
a spar extending spanwise across a width of the airfoil from the first surface to the second surface at a largest height of the airfoil, wherein the spar is configured to provide structural support to the airfoil; and
an ice protected zone extending from the leading edge to a line upstream of the spar;

a heater mounted on the airfoil in the ice protected zone and configured to melt ice that accumulates on or near the leading edge when in operation thereby forming liquid water;
and at least one ice phobic layer attached to the airfoil and positioned on the second surface entirely downstream of the ice protected zone, wherein the at least one ice phobic layer is positioned to prevent liquid water flowing across the airfoil from refreezing downstream of the ice protected zone when the heater is in operation.

2. The ice protection assembly of claim 1 , wherein the ice phobic layer is attached on the second surface across the spar.

3. The ice protection assembly of claim 1 , wherein the ice phobic material has an ice adhesion of less than 200 psi.

4. The ice protection assembly of claim 3 , wherein the ice phobic material has an ice adhesion of less than 100 psi.

5. The ice protection assembly of claim 4 , wherein the ice phobic material has an ice adhesion of less than 45 psi.

6. A method of preventing runback ice comprising:
melting ice that accumulates on or near a leading edge of an external surface of an aircraft into water with a heater, wherein the heater is in an ice protected zone that extends on the external surface downstream of the heater and the external surface is an airfoil; and
running the water across a portion of the external surface downstream of the heater, the portion of the external surface containing at least one ice phobic layer configured to prevent runback ice formation, wherein the at least one ice phobic layer is positioned entirely downstream of the ice protected zone.

7. The method of claim 6 , wherein the ice phobic material has an ice adhesion of less than 200 psi.

8. The ice protection assembly of claim 1 , further comprising a second ice phobic layer positioned on the second surface adjacent to the at least one ice phobic layer and downstream of the spar in the direction of the trailing edge.

9. The ice protection assembly of claim 8 , further comprising a third ice phobic layer positioned on the second surface in the ice protected zone adjacent to the at least one ice phobic layer.

Assignees

• Goodrich Corp

Inventors

• Botura Galdemir Cezar
• Hu Jin

Classifications

• F05D2240/121

  related to the leading edge of a stator vane · CPC title

• F01D25/02

  De-icing means for engines having icing phenomena · CPC title

• F05D2240/306

  related to the suction side of a rotor blade · CPC title

• B64C15/12 Primary

  the power plant being tiltable · CPC title

• F05D2240/124

  related to the suction side of a stator vane · CPC title