Patents by Inventor Thomas Ceyrowsky

Thomas Ceyrowsky 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).

  • Radial compressor
    Patent number: 9976566
    Abstract: A radial compressor has at least one compressor stage. The compressor stage includes: an impeller having moving blades on a rotor side arranged in a flow channel of the compressor stage. The flow channel is bounded by a hub contour and a housing contour or cover disc contour. Each moving blade has a flow inlet edge and a flow outlet edge. In the region of the compressor stage on the hub contour of the flow channel, initially a curvature change from a first concave curvature into a convex curvature and following this a curvature change from the convex curvature into a second concave curvature is formed; and/or on the housing contour or cover disc contour of the flow channel, initially a curvature change from a first convex curvature into a concave curvature and following this a curvature change from the concave curvature into a second convex curvature is formed.
    Type: Grant
    Filed: October 30, 2014
    Date of Patent: May 22, 2018
    Assignee: MAN Diesel & Turbo SE
    Inventors: André Hildebrandt, Thomas Ceyrowsky
  • Radial compressor and compressor arrangement with such a radial compressor
    Patent number: 9790945
    Abstract: A radial compressor for a compressor arrangement comprising the radial compressor and an axial compressor includes an inlet flow channel bounded by a radially inner hub contour and a radially outer housing contour, in which inlet guide blades are arranged. Via the inlet flow channel a medium to be compressed is supplied to an impeller having moving blades. The inlet flow channel runs diagonally to an axis of rotation of the impeller.
    Type: Grant
    Filed: December 17, 2014
    Date of Patent: October 17, 2017
    Assignee: MAN Diesel & Turbo SE
    Inventors: Alf-Peter Tiedtke, Andre Hildebrandt, Thomas Ceyrowsky, Hauke Strohmeyer
  • RADIAL COMPRESSOR AND COMPRESSOR ARRANGEMENT WITH SUCH A RADIAL COMPRESSOR
    Publication number: 20150167675
    Abstract: A radial compressor for a compressor arrangement comprising the radial compressor and an axial compressor includes an inlet flow channel bounded by a radially inner hub contour and a radially outer housing contour, in which inlet guide blades are arranged. Via the inlet flow channel a medium to be compressed is supplied to an impeller having moving blades. The inlet flow channel runs diagonally to an axis of rotation of the impeller.
    Type: Application
    Filed: December 17, 2014
    Publication date: June 18, 2015
    Inventors: Alf-Peter TIEDTKE, Andre Hildebrandt, Thomas Ceyrowsky, Thomas Strohmeyer
  • Radial Compressor
    Publication number: 20150118061
    Abstract: A radial compressor has at least one compressor stage. The compressor stage includes: an impeller having moving blades on a rotor side arranged in a flow channel of the compressor stage. The flow channel is bounded by a hub contour and a housing contour or cover disc contour. Each moving blade has a flow inlet edge and a flow outlet edge. In the region of the compressor stage on the hub contour of the flow channel, initially a curvature change from a first concave curvature into a convex curvature and following this a curvature change from the convex curvature into a second concave curvature is formed; and/or on the housing contour or cover disc contour of the flow channel, initially a curvature change from a first convex curvature into a concave curvature and following this a curvature change from the concave curvature into a second convex curvature is formed.
    Type: Application
    Filed: October 30, 2014
    Publication date: April 30, 2015
    Inventors: André Hildebrandt, Thomas Ceyrowsky