Engine nacelle heat exchanger

1. A nacelle for an engine, comprising:

an exterior housing at least partially surrounding the engine;

a front portion proximate an engine face of the engine, wherein the front portion of the nacelle defines an opening into an interior of the nacelle;

a seal disposed proximate the opening, wherein the seal is configured to selectively allow air into the interior of the nacelle, the seal comprising a K-Seal positioned on the exterior housing of the nacelle and a J-Seal positioned on the engine, the K-Seal comprising a flap configured to rest against a portion of the J-Seal;

a heat exchanger disposed within the interior of the nacelle, the heat exchanger coupled to the J-Seal via a mount, the heat exchanger configured to exchange heat between a fluid flowing within the heat exchanger and the air at the interior of the nacelle; and

wherein the nacelle further comprises one or more fans, the one or more fans configured to flow the air from outside the nacelle across the heat exchanger.

2. The nacelle of claim 1 , wherein the heat exchanger is configured to flow the fluid away from the interior of the nacelle and the fluid is used to remove heat from a system remote from the nacelle.

3. The nacelle of claim 1 , wherein the heat exchanger comprises one or more valves, the one or more valves configured to discharge the fluid into the interior of the nacelle.

4. The nacelle of claim 1 , wherein the exterior housing has a substantially round or elliptical cross-section and the opening extends around a perimeter defined at the front portion of the nacelle.

5. The nacelle of claim 1 , wherein the heat exchanger extends in an arc around the engine disposed within the nacelle proximate the engine face of the engine.

6. The nacelle of claim 1 , wherein the one or more fans are configured to control a rate of flow of the air from outside the nacelle based at least partially on a velocity of the nacelle.

7. The nacelle of claim 1 , wherein the one or more fans are configured to control a rate of flow of the air from outside the nacelle based at least partially on a temperature of the fluid at the heat exchanger.

8. The nacelle of claim 1 , wherein the seal comprises a mechanical portion configured to move in response to an input to selectively allow the air into the interior of the nacelle.

9. The nacelle of claim 1 , wherein the seal allows the air into the interior of the nacelle automatically when exposed to a pressure differential between the air outside the nacelle at the opening and the air within the interior of the nacelle above a threshold pressure differential.

10. The nacelle of claim 1 , wherein the one or more fans comprises at least two fans that are spaced around a perimeter of the nacelle.

11. An aircraft, comprising:

an engine;

a nacelle housing the engine, the nacelle comprising:

an exterior housing at least partially surrounding the engine;

a front portion proximate an engine face of the engine, wherein the front portion of the nacelle defines an opening into an interior of the nacelle;

a seal disposed proximate the opening, wherein the seal is configured to selectively allow air into the interior of the nacelle, the seal comprising a K-Seal positioned on the exterior housing of the nacelle and a J-Seal positioned on the engine, the K-Seal comprising a flap configured to rest against a portion of the J-Seal; and

a heat exchanger disposed within the interior of the nacelle, the heat exchanger coupled to the J-Seal via a mount, the heat exchanger configured to exchange heat between a fluid flowing within the heat exchanger and the air at the interior of the nacelle;

an inlet duct configured to direct the air to the engine face of the engine;

a subsystem remote from the nacelle, wherein the fluid from the heat exchanger is configured to exchange heat generated at the subsystem; and

wherein the nacelle further comprises one or more fans, the one or more fans configured to flow the air from outside the nacelle across the heat exchanger.