Patents by Inventor Thibaud MANGIN

Thibaud MANGIN 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: 10906667
    Abstract: A method for transporting a turbine engine held by a transport kit by a carriage. The transport kit connected to a connection member hoists the engine to connect to an aircraft fuselage. The transport kit is a structure which includes a hoisting interface (328) arranged on a rigid hoisting arm (318) which extends over the turbine engine and is connected to a rigid transport arm (316) which extends over a lateral side of the turbine engine. The transport arm is connected to at least two engine mounts (340) solid with the turbine engine. The transport arm (316), or one of the engine mounts connected to the transport arm, includes a transport interface (324) that can be supported by a bearing element (332) of a truck (326) used for transporting the turbine engine.
    Type: Grant
    Filed: February 2, 2015
    Date of Patent: February 2, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Thierry Kohn, Stephane Baucher, Damien Cesar, Alexandre Dervaux, Franck Dubreucq, Thibaud Mangin
  • Patent number: 10550728
    Abstract: The invention relates to an assembly for the removal, transportation and maintenance of an aircraft turbine engine (10) on a maintenance trolley (34), comprising a turbine engine (10) comprising an upper means (14) for attaching the housing (16) of the turbine engine (10) to the aircraft and a first lower means (20) dedicated to transportation for attaching the housing (16) of the turbine engine (10), a maintenance trolley (34), and a member (32) comprising a means for attaching said member (34) to the housing (16) and at least one means for support and articulation of said member (32) and of the turbine engine (10) on the trolley (34), allowing the turbine engine (10) to pivot to the vertical; characterised in that the member comprises a first attachment means designed to engage with the upper means (14), a second attachment means designed to engage with the first lower means (20), and a pivot means forming the support and articulation means engaging with a complementary receiving means (44) of the trolley (
    Type: Grant
    Filed: November 22, 2017
    Date of Patent: February 4, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alexandre Dervaux, Yves Roland Crochemore, Franck Dubreucq, Thibaud Mangin
  • Publication number: 20180142576
    Abstract: The invention relates to an assembly for the removal, transportation and maintenance of an aircraft turbine engine (10) on a maintenance trolley (34), comprising a turbine engine (10) comprising an upper means (14) for attaching the housing (16) of the turbine engine (10) to the aircraft and a first lower means (20) dedicated to transportation for attaching the housing (16) of the turbine engine (10), a maintenance trolley (34), and a member (32) comprising a means for attaching said member (34) to the housing (16) and at least one means for support and articulation of said member (32) and of the turbine engine (10) on the trolley (34), allowing the turbine engine (10) to pivot to the vertical; characterised in that the member comprises a first attachment means designed to engage with the upper means (14), a second attachment means designed to engage with the first lower means (20), and a pivot means forming the support and articulation means engaging with a complementary receiving means (44) of the trolle
    Type: Application
    Filed: November 22, 2017
    Publication date: May 24, 2018
    Inventors: Alexandre DERVAUX, Yves Roland CROCHEMORE, Franck DUBREUCQ, Thibaud MANGIN
  • Publication number: 20170166331
    Abstract: Structure (310) for transporting and hoisting a turbomachine (312), said structure comprising a hoisting interface (328) arranged on a rigid hoisting arm (318) which extends over the turbomachine and is connected to a rigid transport arm (316) which extends over a lateral side of the turbomachine, this transport arm being connected to at least two engine mounts (340) solid with the turbomachine. The transport arm (316), or one of the engine mounts connected to this transport arm, comprises a transport interface (324) that can be supported by a bearing element (332) of a truck (326) used for transporting the turbomachine.
    Type: Application
    Filed: February 2, 2015
    Publication date: June 15, 2017
    Inventors: Thierry KOHN, Stephane BAUCHER, Damien CESAR, Alexandre DERVAUX, Franck DUBREUCQ, Thibaud MANGIN