Patents by Inventor Juan Manuel Gallardo Antolín

Juan Manuel Gallardo Antolín 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).

  • Highly slenderness rotor
    Patent number: 8066488
    Abstract: The present invention relates to a rotor for gas or steam turbines having a disk (1), an outer cover (2) and a plurality of blades (3). The disk (1) defines the portion of less diameter of the rotor and has an inner surface configured to be coupled on a shaft (100) of the turbine or connected to an axially adjacent disk (1?, 1?); an outer surface configured for housing a plurality of blades (3). The outer cover (2) defines the portion of greater diameter of the rotor. The blades (3) have a root (31) configured to be coupled on the disk (1) and a tip (32) opposite to the outer cover (2). Between these blades there is a plurality of blades (3) welded together at the tip (32) to form groups of blades (3a) and individual blades (3b) intercalated between groups of blades (3a).
    Type: Grant
    Filed: April 10, 2007
    Date of Patent: November 29, 2011
    Assignee: Industria de Turbo Propulsores, S.A.
    Inventors: Roque Corral Garcia, Juan Manuel Gallardo Antolín
  • Highly slenderness rotor
    Publication number: 20080112809
    Abstract: The present invention relates to a rotor for gas or steam turbines having a disk (1), an outer cover (2) and a plurality of blades (3). The disk (1) defines the portion of less diameter of the rotor and has an inner surface configured to be coupled on a shaft (100) of the turbine or connected to an axially adjacent disk (1?, 1?); an outer surface configured for housing a plurality of blades (3). The outer cover (2) defines the portion of greater diameter of the rotor. The blades (3) have a root (31) configured to be coupled on the disk (1) and a tip (32) opposite to the outer cover (2). Between these blades there is a plurality of blades (3) welded together at the tip (32) to form groups of blades (3a) and individual blades (3b) intercalated between groups of blades (3a).
    Type: Application
    Filed: April 10, 2007
    Publication date: May 15, 2008
    Applicant: INDUSTRIA DE TURBO PROPULSORES, S.A.
    Inventors: Roque Corral Garcia, Juan Manuel Gallardo Antolin