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Various methods and systems are provided for a turbocharger. In one example, a method includes determining a first pressure at a first location within a turbocharger and determining a second pressure at a second location within the turbocharger. The method further includes indicating degradation of

Various methods and systems are provided for a turbocharger. In one example, a method includes determining a first pressure at a first location within a turbocharger and determining a second pressure at a second location within the turbocharger. The method further includes indicating degradation of the turbocharger based on the first pressure and the second pressure.

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1. A method, comprising: determining a first pressure at a first location within a turbocharger;determining a second pressure at a seal cavity within a turbocharger casing of the turbocharger and in communication with a turbocharger seal; andindicating degradation of the turbocharger seal based on t

1. A method, comprising: determining a first pressure at a first location within a turbocharger;determining a second pressure at a seal cavity within a turbocharger casing of the turbocharger and in communication with a turbocharger seal; andindicating degradation of the turbocharger seal based on the first pressure and the second pressure. 2. The method of claim 1, wherein the first location is in an oil cavity of the turbocharger or at a diffuser in a compressor casing of the turbocharger. 3. The method of claim 1, further comprising indicating degradation of a non-contact seal of the turbocharger if the first pressure has passed a first threshold pressure or the second pressure has passed a second threshold pressure. 4. The method of claim 1, further comprising indicating degradation of a non-contact seal of the turbocharger when a difference between the first pressure and the second pressure is greater than a threshold difference. 5. The method of claim 1, further comprising determining frequency content of the second pressure, and based on the frequency content, indicating degradation of a compressor of the turbocharger. 6. The method of claim 1, further comprising indicating degradation of the turbocharger while the turbocharger is in operation coupled to an engine in a vehicle. 7. A method, comprising: determining a first pressure at a first location in a turbocharger;determining a second pressure at a seal cavity within a turbocharger casing in a turbocharger and in communication with a seal;determining frequency content of the second pressure; anddiagnosing a condition of the turbocharger based on the first pressure and the second pressure and the frequency content of the second pressure. 8. The method of claim 7, wherein the first location is in an oil cavity of the turbocharger or at a diffuser in a compressor casing of the turbocharger. 9. The method of claim 7, further comprising diagnosing a condition of the turbocharger if the first pressure has passed a first threshold pressure or the second pressure has passed a second threshold pressure. 10. The method of claim 7, further comprising diagnosing degradation of a non-contact seal of the turbocharger when a difference between the first pressure and the second pressure is greater than a threshold difference. 11. The method of claim 10, further comprising diagnosing the condition of the turbocharger while an engine to which the turbocharger is coupled is in operation, and wherein the difference between the first pressure and the second pressure varies with one or more engine operating parameters. 12. The method of claim 7, wherein the second location is a seal cavity of the turbocharger, and the method further comprises diagnosing degradation of a compressor of the turbocharger based on the frequency content of the second pressure. 13. A system, comprising: a control module configured to receive a first pressure signal from a first pressure sensor disposed in a first location of a turbocharger and to receive a second pressure signal from a second pressure sensor in a seal cavity within a turbocharger casing of the turbocharger and in communication with a seal;wherein the control module is further configured to output a control signal based on the first pressure signal and the second pressure signal. 14. A system, comprising: a turbocharger with a compressor and a turbine, the turbocharger coupled to an engine in a vehicle;a first pressure sensor configured to generate a first signal, the first pressure sensor disposed in an oil cavity of the turbocharger;a second pressure sensor configured to generate a second signal, the second pressure sensor disposed in a seal cavity within a turbocharger casing of the turbocharger and in communication with a seal; anda controller configured to identify a first pressure from the first signal and a second pressure from the second signal and to identify degradation of the turbocharger if a difference between the first pressure and the second pressure is greater than a first threshold difference. 15. The system of claim 14, wherein the first threshold difference varies with an operating condition of the engine. 16. The system of claim 14, further comprising a third pressure sensor configured to generate a third signal, the third pressure sensor disposed in a compressor casing at a diffuser of the turbocharger or in an intake manifold of the engine. 17. The system of claim 16, wherein the controller is further configured to identify degradation of the turbocharger when a difference between the second pressure and the third pressure is greater than a second threshold difference, the second threshold difference varying with an operating condition of the engine. 18. The system of claim 14, wherein the controller is further configured to identify degradation of the turbocharger when the first pressure passes a first threshold pressure and the second pressure passes a second threshold pressure. 19. The system of claim 14, wherein the controller is further configured to identify frequency content of the second signal and to identify degradation of the compressor based on the frequency content. 20. The system of claim 14, wherein the turbocharger further includes an orifice in the seal cavity of the turbocharger, the orifice configured to generate a choked air flow. 21. The system of claim 14, wherein the controller is further configured to identify degradation of a non-contact seal when the difference between the first pressure and the second pressure is greater than the first threshold difference.