Patents by Inventor Adam KRYSZTOPA

Adam KRYSZTOPA 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).

  • Air delivery system for a gas turbine engine
    Patent number: 11499479
    Abstract: A gas turbine engine having an improved air delivery system that includes features for pressurizing and/or cooling various components of the engine while minimizing the impact to the cycle efficiency of the engine, reducing the weight of the engine, and reducing the specific fuel consumption of the engine is provided.
    Type: Grant
    Filed: August 8, 2018
    Date of Patent: November 15, 2022
    Assignees: General Electric Company, GENERAL ELECTRIC COMPANY POLSKA SP. ZO.O
    Inventors: Kenneth Arthur Gould, Abdus Shamim, Jaroslaw Henryk Dekowski, Piotr Sebastian Hance, Przemyslaw Slawomir Tkaczyk, Marcin Pawel Faber, Adam Krysztopa, Piotr Lech Bar, Krzysztof Chelstowski, Craig Alan Gonyou, Robert John Parks
  • Turbine nozzle having an angled inner band flange
    Patent number: 11333041
    Abstract: An inner band assembly for at turbine nozzle of a rotary machine that includes a centerline axis, the inner band assembly comprising a platform portion, a first flange portion coupled to the platform portion and obliquely oriented with respect to the centerline axis, and a second flange coupled to the first flange and obliquely oriented with respect to the first flange. Wherein the platform portion and the first flange intersect.
    Type: Grant
    Filed: October 29, 2020
    Date of Patent: May 17, 2022
    Assignee: General Electric Company Polska Sp. Z o.o.
    Inventors: Michal Czarnecki, Michal Kowalczyk, Adam Krysztopa, Piotr Pachota
  • TURBINE NOZZLE HAVING AN ANGLED INNER BAND FLANGE
    Publication number: 20210040866
    Abstract: An inner band assembly for at turbine nozzle of a rotary machine that includes a centerline axis, the inner band assembly comprising a platform portion, a first flange portion coupled to the platform portion and obliquely oriented with respect to the centerline axis, and a second flange coupled to the first flange and obliquely oriented with respect to the first flange. Wherein the platform portion and the first flange intersect.
    Type: Application
    Filed: October 29, 2020
    Publication date: February 11, 2021
    Inventors: Michal Czarnecki, Michal Kowalczyk, Adam Krysztopa, Piotr Pachota
  • Turbine nozzle having an angled inner band flange
    Patent number: 10830100
    Abstract: A turbine nozzle for a rotary machine including a centerline axis includes an airfoil including a leading edge and a trailing edge. The airfoil defines a throat location proximate the trailing edge. The turbine nozzle also includes an inner band assembly including a platform portion coupled to the airfoil, and a first flange coupled to the platform portion. The first flange is obliquely oriented with respect to the platform portion, and the platform portion and the first flange intersect at a point axially aligned with the throat location.
    Type: Grant
    Filed: August 8, 2018
    Date of Patent: November 10, 2020
    Assignee: General Electric Company Polska Sp. Z o.o.
    Inventors: Michal Czarnecki, Michal Kowalczyk, Adam Krysztopa, Piotr Pachota
  • TURBINE NOZZLE HAVING AN ANGLED INNER BAND FLANGE
    Publication number: 20190085726
    Abstract: A turbine nozzle for a rotary machine including a centerline axis includes an airfoil including a leading edge and a trailing edge. The airfoil defines a throat location proximate the trailing edge. The turbine nozzle also includes an inner band assembly including a platform portion coupled to the airfoil, and a first flange coupled to the platform portion. The first flange is obliquely oriented with respect to the platform portion, and the platform portion and the first flange intersect at a point axially aligned with the throat location.
    Type: Application
    Filed: August 8, 2018
    Publication date: March 21, 2019
    Inventors: Michal Czarnecki, Michal Kowalczyk, Adam Krysztopa, Piotr Pachota
  • AIR DELIVERY SYSTEM FOR A GAS TURBINE ENGINE
    Publication number: 20190063324
    Abstract: A gas turbine engine having an improved air delivery system that includes features for pressurizing and/or cooling various components of the engine while minimizing the impact to the cycle efficiency of the engine, reducing the weight of the engine, and reducing the specific fuel consumption of the engine is provided.
    Type: Application
    Filed: August 8, 2018
    Publication date: February 28, 2019
    Inventors: Kenneth Arthur GOULD, Abdus SHAMIM, Jaroslaw Henryk DEKOWSKI, Piotr Sebastian HANCE, Przemyslaw Slawomir TKACZYK, Marcin Pawel FABER, Adam KRYSZTOPA, Piotr Lech BAR, Krzysztof CHELSTOWSKI, Craig Alan GONYOU, Robert John PARKS