Patents by Inventor Eric Dany Robert Jean Engrand

Eric Dany Robert Jean Engrand 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: 10137515
    Abstract: A scraper tool for deburring an edge of an aircraft turboshaft engine casing is arranged to be mounted in a milling device. The scraper tool includes a body including, on a first end, a connection for the milling device and, on a second end, a deburring module including a turning lathe platelet including at least one cutting edge arranged so as to deburr the casing edge. The deburring module includes a guide adapted to contact the edge to be deburred so as to follow the profile of the edge to be deburred without modifying the orientation of the turning lathe platelet.
    Type: Grant
    Filed: February 19, 2016
    Date of Patent: November 27, 2018
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Eric Dany Robert Jean Engrand
  • Publication number: 20160167144
    Abstract: A scraper tool for deburring an edge of an aircraft turboshaft engine casing is arranged to be mounted in a milling device. The scraper tool includes a body including, on a first end, a connection for the milling device and, on a second end, a deburring module including a turning lathe platelet including at least one cutting edge arranged so as to deburr the casing edge. The deburring module includes a guide adapted to contact the edge to be deburred so as to follow the profile of the edge to be deburred without modifying the orientation of the turning lathe platelet.
    Type: Application
    Filed: February 19, 2016
    Publication date: June 16, 2016
    Applicant: SNECMA
    Inventor: Eric Dany Robert Jean ENGRAND
  • Patent number: 9296052
    Abstract: A method for machining a casing of an aircraft turboshaft engine, the casing including an upstream edge and a downstream edge. The method includes: positioning the casing in a chassis; rotating the chassis at a rotational milling speed; milling a downstream edge and/or upstream edge of the casing by a milling device, so as to correct axial length of the casing; and deburring the casing edge so as to remove at least one burr formed in a vicinity of the edge as a result of the milling, the milling device including a scraper tool which turn-machines the burr as the casing is rotated.
    Type: Grant
    Filed: October 28, 2011
    Date of Patent: March 29, 2016
    Assignee: SNECMA
    Inventor: Eric Dany Robert Jean Engrand
  • Publication number: 20130216322
    Abstract: A method for machining a casing of an aircraft turboshaft engine, the casing including an upstream edge and a downstream edge. The method includes: positioning the casing in a chassis; rotating the chassis at a rotational milling speed; milling a downstream edge and/or upstream edge of the casing by a milling device, so as to correct axial length of the casing; and deburring the casing edge so as to remove at least one burr formed in a vicinity of the edge as a result of the milling, the milling device including a scraper tool which turn-machines the burr as the casing is rotated.
    Type: Application
    Filed: October 28, 2011
    Publication date: August 22, 2013
    Applicant: SNECMA
    Inventor: Eric Dany Robert Jean Engrand