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A method and system for a jet pump is provided. The jet pump system includes a pre-mixing bowl includes a nozzle, a mixing section at least partially surrounding the nozzle, and a first inlet opening configured to receive a first flow of fluid and direct the first flow of fluid to an inlet of the no

A method and system for a jet pump is provided. The jet pump system includes a pre-mixing bowl includes a nozzle, a mixing section at least partially surrounding the nozzle, and a first inlet opening configured to receive a first flow of fluid and direct the first flow of fluid to an inlet of the nozzle. The pre-mixing bowl further includes a second inlet opening configured to receive a second flow of fluid and to direct the second flow of fluid to the mixing section. The second inlet opening includes a first inlet opening area. The second inlet opening includes an entry angle into the pre-mixing bowl that is oblique with respect to the central axis. The pre-mixing bowl further includes a third inlet opening configured to receive a third flow of fluid to direct the third flow of fluid to the mixing section.

대표청구항 ▼

1. An aircraft air management system (AMS) comprising: a first pressurized fluid source of relatively higher pressure air;a second pressurized fluid source of relatively lower pressure air than the first pressurized fluid source; anda jet pump, wherein the jet pump includes a pre-mixing bowl compris

1. An aircraft air management system (AMS) comprising: a first pressurized fluid source of relatively higher pressure air;a second pressurized fluid source of relatively lower pressure air than the first pressurized fluid source; anda jet pump, wherein the jet pump includes a pre-mixing bowl comprising:a nozzle comprising a central axis;a mixing section at least partially surrounding said nozzle;a first inlet opening configured to receive a first flow of fluid from the first pressurized fluid source and direct the first flow of fluid to an inlet of said nozzle; anda second inlet opening configured to receive a second flow of fluid from the second pressurized fluid source and to direct the second flow of fluid to said mixing section, said second inlet opening comprising a first inlet opening area, said second inlet opening comprising an entry angle into said pre-mixing bowl that is oblique with respect to the central axis;a third inlet opening configured to receive a third flow of fluid from the second pressurized fluid source and to direct the third flow of fluid to said mixing section, said third inlet opening comprising a second inlet opening area, said third inlet opening comprising an entry angle into said pre-mixing bowl that is oblique with respect to the central axis; andan outlet opening configured to direct the first, second and third flows of fluid from said pre-mixing bowl; anda mixing tube extending from said outlet opening aligned with the central axis. 2. The air management system of claim 1, wherein said nozzle comprises a conical shape. 3. The air management system of claim 1, wherein said nozzle comprises a plurality of lobed passages. 4. The air management system of claim 3, wherein said plurality of lobed passages extend helically along the central axis and define a helical flow path through said nozzle. 5. The air management system of claim 3, wherein at least one of said plurality of lobed passages comprises a polygonal cross-section. 6. The air management system of claim 3, wherein at least one of said plurality of lobed passages comprises a cross-section having arcuate portions. 7. The air management system of claim 1, wherein first inlet opening is configured to selectively receive a modulated flow of fluid from said first pressurized fluid source. 8. The air management system of claim 1, wherein at least one of said second and said third inlet openings are configured to receive an inlet flow of fluid having a non-uniform flow gradient across a face of said opening. 9. The air management system of claim 1, wherein an area of said second opening and an area of said third inlet opening are different with respect to each other. 10. The air management system of claim 1, wherein said second inlet opening and said third inlet opening are angled with respect to the central axis to direct their respective flows toward said outlet opening. 11. The air management system of claim 1, wherein the first inlet opening area is larger than the second inlet opening such that a velocity of the flow of fluid though said second inlet opening is greater than the flow of fluid though said first inlet opening, the uneven flow between said first inlet opening and said second inlet opening promoting a swirl in said pre-mixing bowl. 12. An aircraft comprising an air management system (AMS), said AMS comprising: a jet pump apparatus comprising:a pre-mixing bowl comprising:a nozzle comprising a central axis;a mixing section at least partially surrounding said nozzle;a first inlet opening configured to receive a first flow of fluid from a first pressurized fluid source and direct the first flow of fluid to an inlet of said nozzle; anda second inlet opening configured to receive a second flow of fluid from a second pressurized fluid source and to direct the second flow of fluid to said mixing section, said second inlet opening comprising a first inlet opening area, said second inlet opening comprising an entry angle into said pre-mixing bowl that is oblique with respect to the central axis;a third inlet opening configured to receive a third flow of fluid from the second pressurized fluid source and to direct the third flow of fluid to said mixing section, said third inlet opening comprising a second inlet opening area, said third inlet opening comprising an entry angle into said pre-mixing bowl that is oblique with respect to the central axis; andan outlet opening configured to direct the first, second and third flows of fluid from said pre-mixing bowl; anda mixing tube extending from said outlet opening aligned with the central axis. 13. The aircraft of claim 12, wherein said nozzle comprises a conical shape. 14. The aircraft of claim 12, wherein said nozzle comprises a plurality of lobed passages. 15. The aircraft of claim 14, wherein said plurality of lobed passages extend helically along the central axis and define a helical flow path through said nozzle. 16. The aircraft of claim 12, wherein an area of said second opening and an area of said third inlet opening are different with respect to each other. 17. The aircraft of claim 12, wherein said second opening and said third inlet opening are angled with respect to the central axis to direct their respective flows toward said outlet opening. 18. The aircraft of claim 12, wherein the first inlet opening area is larger than the second inlet opening such that a velocity of the flow of fluid though said second inlet opening is greater than the flow of fluid though said first inlet opening, the uneven flow between said first inlet opening and said second inlet opening promoting a swirl in said pre-mixing bowl.