Patents by Inventor Stephane Bois

Stephane Bois 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: 10125630
    Abstract: A fan disk is for a jet engine in which there flows a gas stream in a flow direction. A pin-shaped radial section of the fan disk includes a first branch, designed to be fixed to a drive shaft of the jet engine, a second branch, extending opposite the first branch and designed to support a plurality of fan blades, and a curved junction wall that extends between the first branch and the second branch.
    Type: Grant
    Filed: March 28, 2014
    Date of Patent: November 13, 2018
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Stephane Bois, Arnaud Accary, Claude Dejaune, Benjamin Kiener-Calvet, Julien Foll, Alexandre Tan-Kim, Benjamin Petard
  • Patent number: 9885389
    Abstract: A device for coupling two shafts by a gear mechanism includes a coupling part ending one of the two shafts. The coupling part is fitted concentrically into a complementary coupling part ending the other shaft. Splines of the coupling part have a constant profile along a median zone of the coupling part and which, in a first zone in continuation of the median zone, has a smaller thickness, between flanks of a spline, than a maximum thickness of the same spline in the median zone. Splines of the coupling part continue, beyond the first zone, as far as a centering zone on the same side as the first zone. The splines and the spline bottoms have, in the coupling zone between the centering zone and the first zone, a profile that continuously couples the splines and the spline bottoms to the surface of the centering zone.
    Type: Grant
    Filed: April 12, 2013
    Date of Patent: February 6, 2018
    Assignee: SNECMA
    Inventors: Stephane Bois, Guillaume Patin
  • Publication number: 20160069207
    Abstract: A fan disk is for a jet engine in which there flows a gas stream in a flow direction, pin-shaped radial section of the fan disk includes a first branch, designed to be fixed to a drive shaft of the jet engine, a second branch, extending opposite the first branch and designed to support a plurality of fan blades, and a curved junction wall that extends between the first branch and the second branch.
    Type: Application
    Filed: March 28, 2014
    Publication date: March 10, 2016
    Applicant: SNECMA
    Inventors: Stephane BOIS, Amaud ACCARY, Claude DEJAUNE, Benjamin KIENER-CALVET, Julien FOLL, Alexandre TAN-KIM, Benjamin PETARD
  • Publication number: 20150125269
    Abstract: A device for coupling two shafts by a gear mechanism includes a coupling part ending one of the two shafts. The coupling part is fitted concentrically into a complementary coupling part ending the other shaft. Splines of the coupling part have a constant profile along a median zone of the coupling part and which, in a first zone in continuation of the median zone, has a smaller thickness, between flanks of a spline, than a maximum thickness of the same spline in the median zone. Splines of the coupling part continue, beyond the first zone, as far as a centering zone on the same side as the first zone. The splines and the spline bottoms have, in the coupling zone between the centering zone and the first zone, a profile that continuously couples the splines and the spline bottoms to the surface of the centering zone.
    Type: Application
    Filed: April 12, 2013
    Publication date: May 7, 2015
    Applicant: SNECMA
    Inventors: Stephane Bois, Guillaume Patin