Patents by Inventor Jose Luis Lazaro Bercianos

Jose Luis Lazaro Bercianos has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Two-sided turbocharger wheel with differing blade parameters
    Patent number: 10233756
    Abstract: A two-sided turbocharger compressor wheel and a housing forming a diffuser for the compressor. A first side and a second side of the compressor wheel are characterized by different values of a trim and of an annulus area. A first side of the diffuser surrounds the first side of the compressor wheel, and a second side of the diffuser surrounds the second side of the compressor wheel. The first and second sides of the diffuser are characterized by different annulus area ratios. The blades of the first and second sides of the compressor wheel are angularly offset from one another. The compressor wheel is configured for greater flow through the side of the compressor wheel that faces away from a related turbine wheel.
    Type: Grant
    Filed: August 27, 2013
    Date of Patent: March 19, 2019
    Assignee: GARRETT TRANSPORTATION I INC.
    Inventors: Hua Chen, Annie Li, Michael Zhao, Wei Dai, Jose Luis Lazaro Bercianos, Vit Houst, Daniel Turecek, Vaclav Kares, Milan Nejedly, Michal Mokos
  • Functionally asymmetric two-sided turbocharger wheel and diffuser
    Patent number: 10006290
    Abstract: A two-sided turbocharger compressor wheel and a housing forming a diffuser for the compressor. A first side and a second side of the compressor wheel are characterized by different values of a trim and of an annulus area. A first side of the diffuser surrounds the first side of the compressor wheel, and a second side of the diffuser surrounds the second side of the compressor wheel. The first and second sides of the diffuser are characterized by different annulus area ratios. The blades of the first and second sides of the compressor wheel are angularly offset from one another. The compressor wheel is configured for greater flow through the side of the compressor wheel that faces away from a related turbine wheel.
    Type: Grant
    Filed: August 27, 2013
    Date of Patent: June 26, 2018
    Assignee: Honeywell International Inc.
    Inventors: Vit Houst, Daniel Turecek, Vaclav Kares, Milan Nejedly, Michal Mokos, Hua Chen, Annie Li, Michael Zhao, Wei Dai, Jose Luis Lazaro Bercianos
  • FUNCTIONALLY ASYMMETRIC TWO-SIDED TURBOCHARGER WHEEL AND DIFFUSER
    Publication number: 20150063980
    Abstract: A two-sided turbocharger compressor wheel and a housing forming a diffuser for the compressor. A first side and a second side of the compressor wheel are characterized by different values of a trim and of an annulus area. A first side of the diffuser surrounds the first side of the compressor wheel, and a second side of the diffuser surrounds the second side of the compressor wheel. The first and second sides of the diffuser are characterized by different annulus area ratios. The blades of the first and second sides of the compressor wheel are angularly offset from one another. The compressor wheel is configured for greater flow through the side of the compressor wheel that faces away from a related turbine wheel.
    Type: Application
    Filed: August 27, 2013
    Publication date: March 5, 2015
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Vit Houst, Daniel Turecek, Vaclav Kares, Milan Nejedly, Michal Mokos, Hua Chen, Annie Li, Michael Zhao, Wei Dai, Jose Luis Lazaro Bercianos
  • STRUCTURALLY ASYMMETRIC TWO-SIDED TURBOCHARGER WHEEL
    Publication number: 20150064002
    Abstract: A two-sided turbocharger compressor wheel and a housing forming a diffuser for the compressor. A first side and a second side of the compressor wheel are characterized by different values of a trim and of an annulus area. A first side of the diffuser surrounds the first side of the compressor wheel, and a second side of the diffuser surrounds the second side of the compressor wheel. The first and second sides of the diffuser are characterized by different annulus area ratios. The blades of the first and second sides of the compressor wheel are angularly offset from one another. The compressor wheel is configured for greater flow through the side of the compressor wheel that faces away from a related turbine wheel.
    Type: Application
    Filed: August 27, 2013
    Publication date: March 5, 2015
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Hua Chen, Annie Li, Michael Zhao, Wei Dai, Jose Luis Lazaro Bercianos, Vit Houst, Daniel Turecek, Vaclav Kares, Milan Nejedly, Michal Mokos