A rotor wheel for an engine includes a plurality of impeller vanes and a plurality of fluid passages defined by adjacent impeller vanes. The fluid passages are radially disposed across at least a portion of the rotor wheel. One or more impeller inserts may be disposed within one or more of the plura
A rotor wheel for an engine includes a plurality of impeller vanes and a plurality of fluid passages defined by adjacent impeller vanes. The fluid passages are radially disposed across at least a portion of the rotor wheel. One or more impeller inserts may be disposed within one or more of the plurality of fluid passages, respectively. The impeller inserts define an impeller passage with a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages.
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1. A rotor wheel for an engine, the rotor wheel comprising: a plurality of impeller vanes;a plurality of fluid passages defined by adjacent ones of the impeller vanes such that the plurality of fluid passages are radially disposed across at least a portion of the rotor wheel;one or more correspondin
1. A rotor wheel for an engine, the rotor wheel comprising: a plurality of impeller vanes;a plurality of fluid passages defined by adjacent ones of the impeller vanes such that the plurality of fluid passages are radially disposed across at least a portion of the rotor wheel;one or more correspondingly shaped impeller inserts disposed within one or more of the plurality of fluid passages, respectively, the one or more impeller inserts defining an impeller passage with a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages, and wherein the impeller inserts comprise a pocket or hole. 2. A rotor wheel according to claim 1, wherein the impeller passage is narrower than the fluid passages between the adjacent ones of the impeller vanes. 3. A rotor wheel according to claim 2, wherein the impeller passage is formed by milling after installation in the fluid passages. 4. A rotor wheel according to claim 1, wherein the impeller inserts are secured in a dovetail in the fluid passages. 5. A rotor wheel according to claim 1, wherein the impeller inserts are secured in the fluid passages by a pin. 6. A rotor wheel according to claim 1, wherein the impeller inserts are secured in the fluid passages by welding. 7. A rotor wheel according to claim 1, wherein the impeller inserts comprise an insert positioned in the fluid passages, the impeller passage milled in the insert, a top plate slot milled in the insert, and a top plate secured in the top plate slot. 8. A rotor wheel according to claim 1, wherein the impeller vanes comprise at least one slot configured to accommodate the one or more impeller inserts. 9. A rotor wheel according to claim 8, wherein the at least one slot comprises an impeller slot machined in one of the adjacent impeller vanes. 10. A rotor wheel according to claim 8, wherein the at least one slot comprises a weld slot defining a space between the one or more impeller inserts and the impeller vanes for receiving a weld material. 11. An impeller insert for a rotor wheel in an engine, wherein the rotor wheel includes a plurality of impeller vanes, adjacent ones of which defining a plurality of fluid passages such that the plurality of fluid passages are radially disposed across at least a portion of the rotor wheel, the impeller insert being correspondingly shaped to fit within one or more of the fluid passages and comprising an impeller passage having a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages, and wherein the impeller insert comprises a pocket or hole. 12. An impeller insert according to claim 11, comprising an insert positionable in the fluid passages, the impeller passage milled in the insert, a top plate slot milled in the insert, and a top plate secured in the top plate slot. 13. A method of tuning fluid flow across a rotor wheel in an engine, the rotor wheel including a plurality of impeller vanes and a plurality of fluid passages defined by adjacent ones of the impeller vanes such that the plurality of fluid passages are radially disposed across at least a portion of the rotor wheel, the method comprising: positioning one or more correspondingly shaped impeller inserts within one or more of the plurality of fluid passages, respectively; and defining an impeller passage in the impeller inserts with a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages, and wherein the impeller inserts comprise a pocket or hole. 14. A method according to claim 13, wherein the positioning step comprises securing the impeller inserts, and wherein the defining step comprises milling the impeller passage in the impeller inserts. 15. A method according to claim 14, further comprising, after milling the impeller passage, milling a top plate slot and securing a top plate in the top plate slot. 16. A method according to claim 13, further comprising, before the positioning step, machining the impeller vanes so that the fluid passages for receiving the impeller inserts are at least one of wider and deeper. 17. A method according to claim 13, further comprising, before the positioning step, machining a weld slot in the impeller vanes for receiving a weld material to secure the impeller inserts. 18. A method according to claim 13, further comprising replacing the impeller inserts with alternative impeller inserts having different impeller geometries, thereby modifying or tuning flow and pressure across the rotor wheel.
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이 특허에 인용된 특허 (6)
Yuri, Masanori; Laurello, Vincent; Ellis, Charles; Noguchi, Mitsuhiro; Fujii, Keita, Gas turbine and method of bleeding gas therefrom.
Quinones Armando J. (Cincinnati OH) Rieck ; Jr. Harold P. (West Chester OH) Albrecht Richard W. (Fairfield OH) Sullivan Michael A. (Ballston Spa NY) Weisgerber Robert H. (Loveland OH) Plemmons Larry , Turbine disk cooling system.
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