Fixed vane turbocharger

US11230938B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11230938-B2
Application numberUS-201616088189-A
CountryUS
Kind codeB2
Filing dateMar 30, 2016
Priority dateMar 30, 2016
Publication dateJan 25, 2022
Grant dateJan 25, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A fixed vane turbocharger includes: an impeller; a housing including, inside thereof, an impeller housing space which accommodates the impeller, a scroll flow passage formed on a radially outer side of the impeller, and a communication flow passage which brings the impeller housing space and the scroll flow passage into communication; and at least one fixed vane unit disposed in the communication flow passage and fixed to a portion of the housing on an inner side of the scroll flow passage with respect to a radial direction of the impeller. Each of the at least one fixed vane unit includes at least two vane portions and a coupling portion coupling the two vane portions, and is formed of a single sheet metal member.

First claim

Opening claim text (preview).

The invention claimed is: 1. A fixed vane turbocharger, comprising: an impeller; a housing including, inside thereof, an impeller housing space which accommodates the impeller, a scroll flow passage formed on a radially outer side of the impeller, and a communication flow passage which brings the impeller housing space and the scroll flow passage into communication; and at least one fixed vane unit disposed in the communication flow passage and fixed to a portion of the housing on an inner side of the scroll flow passage with respect to a radial direction of the impeller, wherein each of the at least one fixed vane unit includes at least two vane portions and a coupling portion coupling the two vane portions, each of the vane portions comprising a vane having a pressure surface and a suction surface, the coupling portion coupling each of side edges of the two vane portions from each of leading edges to trailing edges of the two vane portions, and wherein each of the at least one fixed vane unit has a shape formed by bending or curving a single sheet metal member, wherein the at least one fixed vane unit includes a plurality of separate fixed vane units disposed at intervals in a circumferential direction. 2. The fixed vane turbocharger according to claim 1 , wherein at least a trailing-edge side portion of the vane portion is curved so as to be convex on a side of a pressure surface. 3. The fixed vane turbocharger according to claim 1 , wherein a leading-edge side metal angle which is an angle formed by a tangent in a circumferential direction of the impeller at a leading edge of the vane portion is greater than a trailing-edge side metal angle which is an angle formed by a tangent in the circumferential direction of the impeller at a trailing edge of the vane portion. 4. The fixed vane turbocharger according to claim 1 , wherein a trailing edge of the vane portion extends in a direction inclined toward a circumferential direction from an axial direction of the impeller. 5. The fixed vane turbocharger according to claim 1 , wherein the single sheet metal member has a shape including a rectangular wave shape, a triangular wave shape, or a sine wave shape. 6. The fixed vane turbocharger according to claim 1 , wherein the fixed vane unit is configured to divide the communication flow passage such that a hub-side flow passage and a shroud-side flow passage are positioned alternately in the communication flow passage in a circumferential direction, wherein each hub-side flow passage is defined by two of the vane portions, the coupling portion coupling the two vane portions and a hub-side wall of the communication flow passage, and wherein each shroud-side flow passage is defined by two of the vane portions, the coupling portion coupling the two vane portions, and a shroud-side wall of the communication flow passage. 7. A fixed vane turbocharger, comprising: an impeller; a housing including, inside thereof, an impeller housing space which accommodates the impeller, a scroll flow passage formed on a radially outer side of the impeller, and a communication flow passage which brings the impeller housing space and the scroll flow passage into communication; and at least one fixed vane unit disposed in the communication flow passage and fixed to a portion of the housing on an inner side of the scroll flow passage with respect to a radial direction of the impeller, wherein each of the at least one fixed vane unit includes at least two vane portions and a coupling portion coupling the two vane portions, each of the vane portions comprising a vane having a pressure surface and a suction surface, the coupling portion coupling each of side edges of the two vane portions from each of leading edges to trailing edges of the two vane portions, and wherein each of the at least one fixed vane unit has a shape formed by bending or curving a single sheet metal member, wherein the at least one fixed vane unit includes a plurality of fixed vane units stacked in an axial direction of the impeller, each of the plurality of fixed vane units having a different shape. 8. The fixed vane turbocharger according to claim 7 , wherein the at least one fixed vane unit is formed by the single sheet metal member over an entire periphery in a circumferential direction of the impeller. 9. The fixed vane turbocharger according to claim 7 , wherein at least a trailing-edge side portion of the vane portion is curved so as to be convex on a side of a pressure surface. 10. The fixed vane turbocharger according to claim 7 , wherein a leading-edge side metal angle which is an angle formed by a tangent in a circumferential direction of the impeller at a leading edge of the vane portion is greater than a trailing-edge side metal angle which is an angle formed by a tangent in the circumferential direction of the impeller at a trailing edge of the vane portion. 11. The fixed vane turbocharger according to claim 7 , wherein a trailing edge of the vane portion extends in a direction inclined toward a circumferential direction from an axial direction of the impeller. 12. A fixed vane turbocharger, comprising: an impeller; a housing including, inside thereof, an impeller housing space which accommodates the impeller, a scroll flow passage formed on a radially outer side of the impeller, and a communication flow passage which brings the impeller housing space and the scroll flow passage into communication; and at least one fixed vane unit disposed in the communication flow passage and fixed to a portion of the housing on an inner side of the scroll flow passage with respect to a radial direction of the impeller, wherein each of the at least one fixed vane unit includes at least two vane portions and a coupling portion coupling the two vane portions, each of the vane portions comprising a vane having a pressure surface and a suction surface, the coupling portion coupling each of side edges of the two vane portions from each of leading edges to trailing edges of the two vane portions, and wherein each of the at least one fixed vane unit has a shape formed by bending or curving a single sheet metal member, wherein a leading-edge side portion of the vane portion is rounded so that a tip of the leading-edge side portion is positioned downstream of a leading edge of the vane portion, the leading-edge side portion including a predetermined range from the tip of the vane portion. 13. The fixed vane turbocharger according to claim 12 , wherein the at least one fixed vane unit is formed by the single sheet metal member over an entire periphery in a circumferential direction of the impeller. 14. The fixed vane turbocharger according to claim 12 , wherein at least a trailing-edge side portion of the vane portion is curved so as to be convex on a side of a pressure surface. 15. The fixed vane turbocharger according to claim 12 , wherein a leading-edge side metal angle which is an angle formed by a tangent in a circumferential direction of the impeller at a leading edge of the vane portion is greater than a trailing-edge side metal angle which is an angle formed by a tangent in the circumferential direction of the impeller at a trailing edge of the vane portion. 16. The fixed vane turbocharger according to claim 12 , wherein a trailing edge of the vane portion extends in a direction inclined toward a circumferential direction from an axial direction of the impeller.

Assignees

Inventors

Classifications

  • Improving ICE efficiencies · CPC title

  • F01D9/045Primary

    for radial flow machines or engines · CPC title

  • sinusoidal · CPC title

  • zigzag · CPC title

  • by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title

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What does patent US11230938B2 cover?
A fixed vane turbocharger includes: an impeller; a housing including, inside thereof, an impeller housing space which accommodates the impeller, a scroll flow passage formed on a radially outer side of the impeller, and a communication flow passage which brings the impeller housing space and the scroll flow passage into communication; and at least one fixed vane unit disposed in the communicati…
Who is the assignee on this patent?
Mitsubishi Heavy Ind Engine & Turbocharger Ltd
What technology area does this patent fall under?
Primary CPC classification F01D9/045. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 25 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).