Patents by Inventor Christos Pashias

Christos Pashias 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).

  • Aircraft propeller and aircraft
    Patent number: 11679863
    Abstract: An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.
    Type: Grant
    Filed: April 21, 2022
    Date of Patent: June 20, 2023
    Assignee: DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT
    Inventor: Christos Pashias
  • AIRCRAFT PROPELLER AND AIRCRAFT
    Publication number: 20220340258
    Abstract: An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.
    Type: Application
    Filed: April 21, 2022
    Publication date: October 27, 2022
    Inventor: Christos Pashias