초록 ▼

A bleed duct is configured for bleeding fan air from the fan bypass duct in a turbofan aircraft engine. The bleed duct includes a tubular conduit having an inlet and outlet at opposite ends. The conduit is configured in flow area for recovering pressure from speeding fan air bled therethrough. A shr

A bleed duct is configured for bleeding fan air from the fan bypass duct in a turbofan aircraft engine. The bleed duct includes a tubular conduit having an inlet and outlet at opposite ends. The conduit is configured in flow area for recovering pressure from speeding fan air bled therethrough. A shroud extends forwardly from the duct inlet for suppressing dynamic pressure oscillations inside the conduit without degrading the pressure recovery.

대표청구항 ▼

Accordingly, what is desired to be secured by Letters Patent of the United States is the invention as defined and differentiated in the following claims in which we claim: 1. A turbofan engine comprising: a fan powered by a core engine including a multistage compressor therein, and a fan bypass duc

Accordingly, what is desired to be secured by Letters Patent of the United States is the invention as defined and differentiated in the following claims in which we claim: 1. A turbofan engine comprising: a fan powered by a core engine including a multistage compressor therein, and a fan bypass duct surrounding said core engine; a bleed system including a primary bleed circuit for bleeding pressurized air from said compressor joined in flow communication with a heat exchanger, and a secondary bleed circuit for bleeding fan air from said fan bypass duct joined in flow communication with said heat exchanger; and said secondary bleed circuit includes a bleed conduit having a duct inlet facing forwardly inside said bypass duct, and duct outlet joined by a valve to said heat exchanger, and an acoustic suppression shroud extending forwardly from said duct inlet inside said bypass duct with a side opening at said duct inlet for suppressing pressure oscillations inside said bleed conduit when said valve is closed. 2. An engine according to claim 1 wherein said shroud projects inside said bypass duct and is coextensive with said duct inlet, and includes a shroud inlet at a forward end thereof spaced forwardly from said duct inlet. 3. An engine according to claim 2 wherein: said duct inlet and outlet are laterally offset along the longitudinal axis of said conduit to effect a laterally offset scoop containing said duct inlet and projecting inside said bypass duct; and said shroud is coextensive with said scoop at said duct inlet therein. 4. An engine according to claim 3 wherein: said bleed conduit further includes an inlet ramp extending forward from said scoop inlet inside said bypass duct; said scoop is laterally arcuate and imperforate; and said shroud is laterally arcuate and imperforate, and disposed over said inlet ramp. 5. An engine according to claim 4 wherein said shroud is integrally joined to said forward end of said scoop. 6. An engine according to claim 5 wherein said shroud is narrower in circumference than said scoop, and is laterally open forward of said scoop inlet. 7. An engine according to claim 6 wherein said shroud includes a pair of support legs at said forward end thereof fixedly joined to said conduit to support said shroud thereabove. 8. An engine according to claim 6 wherein said shroud is cantilevered from said scoop. 9. An engine according to claim 8 wherein said shroud has a maximum length at the middle thereof, and decreases in length along opposite sides thereof. 10. An engine according to claim 4 wherein said shroud is spaced from said scoop. 11. A turbofan bleed duct for a turbofan engine having a fan bypass duct surrounding a core engine, said bleed duct comprising: a tubular conduit having an annular duct inlet at a forward end configured to face forwardly inside said bypass duct and an annular duct outlet at an opposite aft end, and configured in flow area therebetween for recovering pressure from speeding fan air bled therethrough; and an acoustic suppression shroud extending forwardly from said duct inlet with a side opening thereat to suppress dynamic pressure oscillations inside said conduit. 12. A duct according to claim 11 wherein said shroud is coextensive with said duct inlet and includes a shroud inlet at a forward end thereof spaced forwardly from said duct inlet. 13. A duct according to claim 12 wherein: said duct inlet and outlet are laterally offset along the longitudinal axis of said conduit to effect a laterally offset scoop containing said duct inlet; and said shroud is coextensive with said scoop at said duct inlet therein. 14. A duct according to claim 13 wherein said shroud inlet is axially aligned with said scoop inlet to minimize disturbance of streamline flow of said fan air into said scoop inlet. 15. A duct according to claim 14 wherein said shroud is generally parallel with said scoop to minimize said streamline flow disturbance. 16. A duct according to claim 14 wherein: said scoop is laterally arcuate and imperforate; and said shroud is laterally arcuate and imperforate. 17. A duct according to claim 14 wherein said shroud is integrally joined to said forward end of said scoop. 18. A duct according to claim 17 wherein said shroud conforms in thickness with said scoop. 19. A duct according to claim 18 wherein said shroud is narrower in circumference than said scoop, and is laterally open forward of said scoop inlet. 20. A duct according to claim 18 wherein said shroud includes a pair of support legs at said forward end thereof fixedly joined to said conduit to support said shroud thereabove. 21. A duct according to claim 20 wherein said conduit further includes an inlet ramp extending forward from said scoop inlet, and said shroud support legs are fixedly joined thereto. 22. A duct according to claim 20 wherein said shroud has a rectangular profile. 23. A duct according to claim 18 wherein said shroud is cantilevered from said scoop. 24. A duct according to claim 23 wherein said shroud has a maximum length at the middle thereof, and decreases in length along opposite sides thereof. 25. A duct according to claim 24 wherein said shroud sides curve back to said scoop inlet. 26. A duct according to claim 25 wherein said shroud is rectangular in profile, and conforms in width with said scoop. 27. A duct according to claim 25 wherein said shroud is triangular in profile, and conforms in width at the base thereof with said scoop. 28. A duct according to claim 14 wherein said shroud is spaced from said scoop. 29. A duct according to claim 28 wherein said conduit further includes an inlet ramp extending forward from said scoop inlet, and said shroud comprises an arch fixedly joined to said ramp and spaced outwardly from said scoop inlet. 30. A duct according to claim 29 wherein said shroud has a rectangular profile, larger in width than said scoop, and extending in length forward therefrom. 31. A duct according to claim 30 wherein said shroud is higher than said scoop to effect a radial gap thereabove. 32. A duct according to claim 31 wherein said shroud is spaced forwardly from said scoop to effect an axial gap therebetween. 33. A duct according to claim 31 wherein said shroud overlaps said forward end of said scoop. 34. A duct according to claim 33 wherein said shroud includes scalloped sides at the aft ends thereof bridging said scoop inlet both forward and aft therefrom. 35. A turbofan bleed duct for a turbofan engine having a fan bypass duct surrounding a core engine, said bleed duct comprising: a tubular conduit having an annular duct inlet at a forward end configured to face forwardly inside said bypass duct and an annular duct outlet at an opposite aft end, and configured in flow area therebetween for recovering pressure from speeding fan air bled therethrough; and an acoustic suppression shroud extending forwardly from said duct inlet coaxially in line-of-sight alignment therewith to provide both a shroud inlet at the forward end of said shroud and a side opening at said duct inlet.