Granted Patent B2

US 12,377,990 · App. 18/102,510 · Granted Aug 5, 2025

Inventors: Xiaolan Hu (San Diego, CA); Katherine Urena Pimentel (Manchester, CT); Steven Poteet (Lake Forest, CA); David L. Rose (Cardiff By The Sea, CA)

Assignee: ROHR, INC.

B64D15/00F02C7/047B64D2033/0233F05D2300/51F05D2300/512

Abstract

Claims (35)

1. An air inlet section for an aircraft propulsion system nacelle, the air inlet section comprising:

an outer skin forming an outer annular body extending circumferentially about an axial centerline of the aircraft propulsion system nacelle;

an inner skin forming an inner annular body extending circumferentially about the axial centerline, and the inner skin is disposed radially inward of the outer skin; and

a lip skin extending circumferentially about the axial centerline, the lip skin extends between and to an outer end and an inner end, the outer end is disposed at the outer skin, the inner end is disposed at the inner skin, the lip skin forms an exterior lip skin surface extending from the inner end to the outer end, the exterior lip skin surface forms a leading edge of the lip skin, the exterior lip skin surface includes an outer surface portion and an inner surface portion, the outer surface portion extends from the outer end to the inner surface portion, the outer surface portion forms a hydrophobic surface, the inner surface portion extends from the inner end to the outer surface portion, the inner surface portion forms a hydrophilic surface, the hydrophilic surface disposed at the leading edge, and the hydrophilic surface extends between and to the hydrophobic surface and the inner end.

2. The air inlet section of claim 1 , wherein the hydrophilic surface is disposed radially outwardly of the leading edge.

3. The air inlet section of claim 2 , further comprising a hydrophobic coating disposed on the outer surface portion, and the hydrophobic coating forms the hydrophobic surface.

4. The air inlet section of claim 3 , wherein:

a hydrophilic coating is disposed on the inner surface portion, and the hydrophilic coating forms the hydrophilic surface;

the lip skin includes a lip skin body material forming the exterior lip skin surface;

the lip skin body material has a first contact angle, the hydrophilic coating has a second contact angle, and the hydrophobic coating has a third contact angle; and

the first contact angle is greater than the second contact angle and less than the third contact angle.

5. The air inlet section of claim 1 , further comprising a hydrophilic coating disposed on the inner surface portion, and the hydrophilic coating forms the hydrophilic surface.

6. The air inlet section of claim 1 , wherein the outer skin forms an exterior skin surface coincident with the exterior lip skin surface, and at least a portion of the exterior skin surface additionally forms the hydrophobic surface.

7. The air inlet section of claim 1 , wherein:

the lip skin includes a lip skin body material forming the exterior lip skin surface; and

the lip skin body material forms the hydrophobic surface and the hydrophilic surface.

8. The air inlet section of claim 7 , wherein the lip skin body material includes a first surface treatment for the outer surface portion and a second surface treatment for the inner surface portion, the first surface treatment forms the hydrophobic surface, and the second surface treatment forms the hydrophilic surface.

9. The air inlet section of claim 8 , wherein the lip skin body material includes aluminum.

10. An air inlet section for an aircraft propulsion system nacelle, the air inlet section comprising:

an outer skin forming an outer annular body extending circumferentially about an axial centerline of the aircraft propulsion system nacelle;

an inner skin forming an inner annular body extending circumferentially about the axial centerline, and the inner skin is disposed radially inward of the outer skin;

a lip skin extending circumferentially about the axial centerline, the lip skin extends between and to an outer end and an inner end, the outer end is disposed at the outer skin, the inner end is disposed at the inner skin, the lip skin forms an exterior lip skin surface extending from the inner end to the outer end, the exterior lip skin surface forms a leading edge of the lip skin;

a hydrophobic coating disposed on the exterior lip skin surface radially outward of the leading edge; and

a hydrophilic coating disposed on the exterior lip skin surface radially inward of the leading edge.

11. The air inlet section of claim 10 , wherein the outer skin forms an exterior skin surface coincident with the exterior lip skin surface, and the hydrophobic coating is disposed on the exterior skin surface.

12. The air inlet section of claim 10 , wherein:

the hydrophobic coating extends along the exterior lip skin surface between and to a first outer radial end and a first inner radial end; and

the hydrophilic coating extends along the exterior lip skin surface between and to a second outer radial end and a second inner radial end, the second outer radial end disposed at the first inner radial end.

13. The air inlet section of claim 12 , wherein the second outer radial end is disposed radially outward of the leading edge.

14. An aerostructure for an aircraft, the aerostructure comprising:

an outer skin;

an inner skin; and

an arcuate lip skin extending between and to an outer end and an inner end, the outer end is disposed at the outer skin, the inner end is disposed at the inner skin, the arcuate lip skin forms an exterior lip skin surface extending from the inner end to the outer end, the exterior lip skin surface forms a leading edge of the arcuate lip skin, the exterior lip skin surface includes a hydrophobic surface and a hydrophilic surface, the hydrophilic surface disposed at the leading edge, and the hydrophobic surface extending between and to the hydrophilic surface and the outer end.

15. The aerostructure of claim 14 , wherein the hydrophilic surface extends between and to the hydrophobic surface and the inner end.

16. The aerostructure of claim 14 , further comprising an anti-icing system disposed at the arcuate lip skin.

Assignments (1)

Continuity (1)

References Cited (18)