초록

An accessory gearbox system for a gas turbine engine includes an accessory compressor mounted to a gearbox housing. The gearbox housing defines a seal air core, and the gearbox housing communicates a seal airflow through the seal air core.

대표청구항 ▼

1. An accessory gearbox system for a gas turbine engine comprising: a gearbox housing which defines at least one seal air core and a gearbox housing interior; andan accessory compressor mounted to said gearbox housing to communicate a seal airflow through said at least one seal air core. 2. The syst

1. An accessory gearbox system for a gas turbine engine comprising: a gearbox housing which defines at least one seal air core and a gearbox housing interior; andan accessory compressor mounted to said gearbox housing to communicate a seal airflow through said at least one seal air core. 2. The system as recited in claim 1, wherein said at least one seal air core terminates at an accessory shaft seal. 3. The system as recited in claim 2, further comprising an accessory shaft mounted through said accessory shaft seal. 4. The system as recited in claim 3, wherein said an accessory shaft seal is a labyrinth seal, and said seal airflow flows axially along said accessory shaft. 5. The system as recited in claim 1, wherein said accessory gearbox housing contains a gear train which powers at least one accessory. 6. The system as recited in claim 5, wherein said accessory compressor is driven by said gear train. 7. The system as, recited in claim 1, wherein said accessory compressor is one of a liquid ring accessory compressor and a sliding vane accessory compressor. 8. The system as recited in claim 1, wherein said accessory compressor discharges entirely air. 9. The system as recited in claim 1, wherein said gearbox housing defines a multiple of seal air cores. 10. The system as recited in claim 9, further comprising a multiple of accessory shaft seals, said seal air cores terminate at a respective one of said accessory shaft seals, said accessory compressor communicating said seal airflow through said seal air cores to said accessory shaft seals. 11. The system as recited in claim 10, wherein each of said accessory shaft seals are mounted to said gearbox housing. 12. The system as recited in claim 10, wherein there are at least four accessory shaft seals, and wherein each of said accessory shaft seals is in communication with an accessory shaft from one of a power generator, a fuel pump, an oil pump and a hydraulic pump. 13. The system as recited in claim 10, wherein said seal air cores are integrally formed with said gearbox housing. 14. The system as recited in claim 13, wherein said seal air cores define a multiple of separate flow paths within said gearbox housing. 15. The system as recited in claim 10, wherein each of said accessory shaft seals are labyrinth seals. 16. The system as recited in claim 15, further comprising a multiple of accessory shafts, each accessory shaft mounted through a respective one of said accessory shaft seals. 17. The system as recited in claim 16, wherein said seal airflow flows axially along each of said accessory shafts. 18. A gas turbine engine comprising: an engine frame section defined about an axis;an engine spool rotationally mounted along said axis;an accessory gearbox mounted to said frame section, said accessory gearbox driven by said engine spool, said accessory gearbox comprising: a gearbox housing which defines at least one seal air core and a gearbox housing interior; andan accessory compressor mounted to said gearbox housing to communicate a seal airflow through said at least one seal air core. 19. The engine as recited in claim 18, wherein said at least one seal air core terminates at an accessory shaft seal. 20. The engine as recited in claim 19, further comprising an accessory shaft mounted through said accessory shaft seal. 21. The engine as recited in claim 20, further comprising an accessory component mounted to said gearbox housing. 22. The engine as recited in claim 21, wherein said accessory component is driven by said accessory shaft. 23. The engine as recited in claim 18, wherein said engine frame section comprises a fan case. 24. The engine as recited in claim 18, wherein said gearbox housing defines a multiple of seal air cores, and further including a multiple of accessory shaft seals, said seal air cores terminate at a respective one of said accessory shaft seals, said accessory compressor communicating said seal airflow through said seal air cores to said accessory shaft seals. 25. The engine as recited in claim 24, wherein each of said seal air cores are incorporated into said gearbox housing, and wherein each of said accessory shaft seals are mounted to said gearbox housing. 26. A method of providing a seal air supply to an accessory gearbox comprising: compressing a seal air with an accessory compressor mounted to an accessory gearbox housing, said accessory gearbox housing defining at least one seal air core and a housing interior; andcommunicating the seal air through said at least one seal air core to an accessory shaft seal mounted to the accessory gearbox housing. 27. A method as recited in claim 26, further comprising the step of compressing the seal air from air within the accessory gearbox housing. 28. A method as recited in claim 26, further comprising the step of compressing the seal air from ambient air. 29. A method as recited in claim 26, further comprising driving the accessory compressor with a gear train contained within the accessory gearbox housing. 30. A method as recited in claim 26, further comprising driving the accessory compressor with an electric motor. 31. A method as recited in claim 29, further comprising driving the gear train with a gas turbine engine.