Air inlet with integrated fluid diverter

1. An air inlet, comprising:

an outer surface of an enclosure;

an intake opening located in the outer surface of the enclosure for receiving a flow of air from outside the enclosure, wherein the intake opening is narrower at an upstream end of the air inlet, and the intake opening is wider at a downstream end of the air inlet;

a sidewall mechanically coupled with the outer surface around a portion of the intake opening, wherein the sidewall extends upwardly above the outer surface and downwardly below the outer surface;

an inlet ramp angled downwardly from the upstream end of the air inlet towards the downstream end of the air inlet, the inlet ramp being mechanically coupled with the sidewall above the outer surface at the upstream end and below the outer surface at the downstream end;

an inlet lip positioned transversely across the intake opening at the downstream end of the intake opening, wherein the inlet lip comprises a leading edge with a curved profile that faces upstream for separating a portion of air flow while minimizing drag;

a raised flange mechanically coupled with the sidewall that extends transversely away from the intake opening, the raised flange being elevated over the outer surface, wherein the raised flange and the sidewall form a fluid diverter that diverts fluid immediately outside the outer surface of the enclosure to flow around the air inlet, thereby avoiding ingestion of the fluid into the intake opening; and

an aerodynamic fairing mechanically coupled on the outside of the aircraft skin immediately downstream of the inlet lip, wherein the aerodynamic fairing ramps downwardly from the inlet lip to the aircraft skin to provide a low drag connecting surface between the inlet lip and the aircraft skin.

2. The air inlet of claim 1 , further comprising a channel formed between the outer surface, the sidewall, and the raised flange, the channel adapted to divert a boundary layer of fluid flow around the intake opening.

3. The air inlet of claim 1 , wherein the inlet lip is located above the inlet ramp forming an inlet throat therebetween.

4. The air inlet of claim 3 , further comprising an aerodynamic fairing mechanically coupled on the outside of the outer surface immediately downstream of the inlet lip, wherein the aerodynamic fairing ramps downwardly from the inlet lip to the outer surface to provide a low drag connecting surface between the inlet lip and the outer surface.

5. The air inlet of claim 3 , further comprising a duct mechanically coupled with the inlet ramp and the sidewall at the inlet throat, the duct being configured for receiving the flow of air from the intake opening.

6. A fluid diverting air inlet, comprising:

a raised intake opening formed through an outer surface of an aircraft, the raised intake opening configured to receive air for use in the aircraft;

the raised intake opening having a ramp angled downwardly below the outer surface to define an intake passageway, such that the raised intake opening is shallower at an upstream end and deeper at a downstream end with respect to a nominal direction of airflow;

lateral sidewalls that extend seamlessly from the ramp below the outer surface upwardly to form the raised intake opening above the outer surface, the lateral sidewalls converging together at an upstream end of the air inlet, and the lateral sidewalls diverging apart towards a downstream end of the air inlet such that the raised intake opening is narrower at an upstream end and wider at a downstream end;

flanges that extend outwardly from the tops of the lateral sidewalls such that divided air passageways for boundary layer fluids are formed beneath the flanges on each side of the raised intake opening; and

an aerodynamic fairing mechanically coupled on the outside of the aircraft skin immediately downstream of the inlet lip, wherein the aerodynamic fairing ramps downwardly from the inlet lip to the aircraft skin to provide a low drag connecting surface between the inlet lip and the aircraft skin.

7. The fluid diverting air inlet of claim 6 , wherein the divided air passageways comprise bypass channels formed along each side of the raised intake opening for directing boundary layer fluid flow around the raised intake opening, the bypass channels being (i) beneath an underside surface of the flanges; (ii) outside a facade of the lateral sidewalls; and, (iii) above the outer surface.

8. The fluid diverting air inlet of claim 6 , wherein the outer surface is an aircraft skin, and the air inlet is installed in the aircraft skin for providing a low-drag source of air that avoids ingestion of surface attached fluids.

9. The fluid diverting air inlet of claim 6 , wherein the outer surface is curved and the flanges are curved to match the outer surface such that the flanges are substantially parallel with the outer surface.

10. An integrated fluid diverter for an air inlet, comprising:

a ramp angled downwardly through an opening in an aircraft skin, wherein the ramp extends above the aircraft skin at an upstream end and below the aircraft skin at a downstream end;

a pair of sidewalls mechanically coupled with the downwardly angled ramp, wherein the pair of sidewalls extend above the opening, and the pair of sidewalls diverge to form a narrower upstream portion of the opening and a wider downstream portion of the opening;

a flange extending outwardly from the pair of sidewalls above the aircraft skin, the flange being configured to divert air flow immediately adjacent the aircraft skin from entering the opening;

an inlet lip positioned transversely across the opening at the downstream end of the ramp, wherein the inlet lip is aligned with the flange and located above the ramp forming an inlet throat therebetween, and the inlet lip having a low profile in line with the raised flange for minimizing drag; and

an aerodynamic fairing mechanically coupled on the outside of the aircraft skin immediately downstream of the inlet lip, wherein the aerodynamic fairing ramps downwardly from the inlet lip to the aircraft skin to provide a low drag connecting surface between the inlet lip and the aircraft skin.