Patents by Inventor Sebastien Guingo

Sebastien Guingo 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).

  • Patent number: 9702265
    Abstract: A rotary machine including a stationary portion and a rotary portion; at least one bearing provided with a stationary ring and a rotary ring, the bearing being mounted between the stationary portion and the rotary portion in order to guide the rotary portion in rotation; and a damper collar interposed between the stationary ring of the bearing and the stationary portion. The damper collar includes a flexible strip having tongues cut out therein, and the flexible strip is shaped into a ring around the stationary ring of the bearing, the shaping of the strip into a ring causing the tongues to move outwards from the collar so that the free edges of the tongues come into contact with the stationary portion.
    Type: Grant
    Filed: January 13, 2014
    Date of Patent: July 11, 2017
    Assignees: SNECMA, CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE
    Inventors: Mihai Arghir, Pierre Matta, Sebastien Guingo
  • Patent number: 9435347
    Abstract: A turbopump for feeding a low-thrust rocket engine comprises a pump, a turbine, and a common rotary shaft connected to the pump and to the turbine. First and second bearings closer respectively to the pump and to the turbine serve to support the common shaft. The second bearing is a hydrodynamic bearing connected to a gas supply source, and the turbopump also includes at least one dynamic sealing gasket around the shaft and interposed between the first and second bearings.
    Type: Grant
    Filed: August 31, 2011
    Date of Patent: September 6, 2016
    Assignee: SNECMA
    Inventors: Francois Danguy, Laurent Fabbri, Sebastien Guingo
  • Publication number: 20150369080
    Abstract: A rotary machine including a stationary portion and a rotary portion; at least one bearing provided with a stationary ring and a rotary ring, the bearing being mounted between the stationary portion and the rotary portion in order to guide the rotary portion in rotation; and a damper collar interposed between the stationary ring of the bearing and the stationary portion. The damper collar includes a flexible strip having tongues cut out therein, and the flexible strip is shaped into a ring around the stationary ring of the bearing, the shaping of the strip into a ring causing the tongues to move outwards from the collar so that the free edges of the tongues come into contact with the stationary portion.
    Type: Application
    Filed: January 13, 2014
    Publication date: December 24, 2015
    Applicant: SNECMA
    Inventors: Mihai ARGHIR, Pierre MATTA, Sebastien GUINGO
  • Publication number: 20130227931
    Abstract: A turbopump for feeding a low-thrust rocket engine comprises a pump, a turbine, and a common rotary shaft connected to the pump and to the turbine. First and second bearings closer respectively to the pump and to the turbine serve to support the common shaft. The second bearing is a hydrodynamic bearing connected to a gas supply source, and the turbopump also includes at least one dynamic sealing gasket around the shaft and interposed between the first and second bearings.
    Type: Application
    Filed: August 31, 2011
    Publication date: September 5, 2013
    Applicant: Snecma
    Inventors: Francois Danguy, Laurent Fabbri, Sebastien Guingo