Turbocharger

Patent metadata

Field	Value
Publication number	US-11913372-B2
Application number	US-202018018180-A
Country	US
Kind code	B2
Filing date	Nov 25, 2020
Priority date	Nov 25, 2020
Publication date	Feb 27, 2024
Grant date	Feb 27, 2024

Abstract

This turbocharger includes: an impeller which includes a hub provided to be rotatable around a center axis and a plurality of turbine blades arranged on the outside of the hub in a radial direction at intervals in a circumferential direction around the center axis; and a turbine housing which is disposed on the outside of the impeller in the radial direction and forms a scroll flow path guiding an exhaust gas toward the impeller on the inside of the radial direction while turning the exhaust gas in the circumferential direction, wherein a flow path width in the circumferential direction of at least one of a plurality of inter-blade flow path portions formed between the plurality of turbine blades is different from a flow path width of the another of the plurality of inter-blade flow path portions.

First claim

What is claimed is:

1. A turbocharger comprising:
an impeller which includes a hub provided to be rotatable around a center axis and a plurality of turbine blades arranged on the outside of the hub in a radial direction at intervals in a circumferential direction around the center axis; and
a turbine housing which is disposed on the outside of the impeller in the radial direction and forms a scroll flow path guiding an exhaust gas toward the impeller on the inside of the radial direction while turning the exhaust gas in the circumferential direction,
wherein a flow path width in the circumferential direction of at least one of a plurality of inter-blade flow path portions formed between the plurality of turbine blades is different from a flow path width of another of the plurality of inter-blade flow path portions wherein a radial dimension of the hub of a first of the plurality of inter-blade flow path portions is larger than a radial dimension of the hub of a second of the plurality of inter-blade flow path portions having a larger flow path width than that of the first of the plurality of inter-blade flow path portions.

2. The turbocharger according to claim 1 ,
wherein the plurality of turbine blades include a first group of turbine blades which are arranged at equal intervals in the circumferential direction and a second group of turbine blades which are arranged at equal intervals in the circumferential direction, and
wherein each turbine blade of the second group of turbine blades is disposed with a phase shift in the circumferential direction with respect to each turbine blade of the first group of turbine blades.

3. The turbocharger according to claim 1 ,
wherein the plurality of turbine blades are arranged to have the same minimum flow path area between the blades adjacent to each other in the circumferential direction on a downstream side of an exhaust gas flow direction and are arranged at unequal intervals in the circumferential direction on an upstream side of the exhaust gas flow direction.

4. The turbocharger according to claim 1 ,
wherein the turbine housing includes a plurality of the scroll flow paths each supplying the exhaust gas to the impeller from a plurality of different positions of the impeller in the circumferential direction.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Hoshi Toru
• NAGAYO Yukihide
• Nakaye Shoeji
• Mori Toshikazu
• Hagiwara Takaaki

Classifications

• F02B37/025 Primary

  Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title

• F02B33/40

  of non-positive-displacement type · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F05D2260/961

  by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape · CPC title

• F02B39/00 Primary

  Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00 · CPC title