Patents by Inventor Mario LAMBEY

Mario LAMBEY 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: 10486819
    Abstract: The invention relates to a method for mounting an engine (1) on an aircraft strut (3) comprising engine suspension members (31) integral with the strut, the engine being integral with a suspension cradle (6) whereby it is suspended from the strut, the method comprising a step of hoisting the engine in a vertical direction as far as the strut then a step of approaching the strut by a movement of the engine in another direction, characterised in that an intermediate part (7) is fixed to the strut beforehand, by attaching it to said suspension members (31), said intermediate part (7) having an interface intended to cooperate with a complementary interface provided on the cradle (6), in such a way as to position the cradle relative to the intermediate part at the end of the approach movement to the strut. The invention also relates to the system for implementing the method.
    Type: Grant
    Filed: September 16, 2015
    Date of Patent: November 26, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Mario Lambey, Bruno Albert Beutin, Marc Patrick Tesniere
  • Publication number: 20170259928
    Abstract: The invention relates to a method for mounting an engine (1) on an aircraft strut (3) comprising engine suspension members (31) integral with the strut, the engine being integral with a suspension cradle (6) whereby it is suspended from the strut, the method comprising a step of hoisting the engine in a vertical direction as far as the strut then a step of approaching the strut by a movement of the engine in another direction, characterised in that an intermediate part (7) is fixed to the strut beforehand, by attaching it to said suspension members (31), said intermediate part (7) having an interface intended to cooperate with a complementary interface provided on the cradle (6), in such a way as to position the cradle relative to the intermediate part at the end of the approach movement to the strut. The invention also relates to the system for implementing the method.
    Type: Application
    Filed: September 16, 2015
    Publication date: September 14, 2017
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Mario LAMBEY, Bruno Albert BEUTIN, Marc Patrick TESNIERE
  • Patent number: 9637239
    Abstract: The invention provides a suspension structure for suspending a turboprop (10) having two unducted propellers on a structural element of an aircraft, the suspension structure comprising a cradle (18) for fastening to a structural element of the aircraft and having two lateral beams (22) connected to a main beam (20) extending parallel to a longitudinal axis (14) of the turboprop so as to form a V-shaped cradle structure, the cradle being fastened to the turboprop via two angle members (24) connecting each free end of the lateral beams of the cradle to the turboprop, via an axial link (28) connecting one end of the main beam of the cradle of the turboprop, and via at least one transverse link (30) situated in a plane extending transversely relative to the longitudinal axis of the turboprop and connecting the cradle to the turboprop.
    Type: Grant
    Filed: April 24, 2014
    Date of Patent: May 2, 2017
    Assignee: SNECMA
    Inventors: Mathieu Ange Alexis Poisson, Julien Michel Patrick Christian Austruy, François Gallet, Mario Lambey
  • Publication number: 20160159486
    Abstract: The invention provides a suspension structure for suspending a turboprop (10) having two unducted propellers on a structural element of an aircraft, the suspension structure comprising a cradle (18) for fastening to a structural element of the aircraft and having two lateral beams (22) connected to a main beam (20) extending parallel to a longitudinal axis (14) of the turboprop so as to form a V-shaped cradle structure, the cradle being fastened to the turboprop via two angle members (24) connecting each free end of the lateral beams of the cradle to the turboprop, via an axial link (28) connecting one end of the main beam of the cradle of the turboprop, and via at least one transverse link (30) situated in a plane extending transversely relative to the longitudinal axis of the turboprop and connecting the cradle to the turboprop.
    Type: Application
    Filed: April 24, 2014
    Publication date: June 9, 2016
    Applicant: SNECMA
    Inventors: Mathieu Ange Alexis POISSON, Julien Michel Patrick Christian AUSTRUY, François GALLET, Mario LAMBEY