Inventor · Larra, FR

Frédéric Vinches

15Patents
3h-index
23Co-inventors
60Inventor score

Filing activity: Nov 2, 2004 → Apr 17, 2024

Most-cited inventions

PatentTitleAreaCited byStatus
US7347399B2 Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment Performing Operations; Transporting 7 Expired
US7258303B2 Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment Performing Operations; Transporting 4 Expired
US11325717B2 Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engine Emerging Cross-Sectional Technologies 3 Active
US11293302B2 Anterior part of a nacelle of an aircraft propulsion unit having a shock absorbing element Mechanical Engineering; Lighting; Heating 2 Active
US11591098B2 Nacelle forward part of a propulsion assembly comprising an inclined stiffening frame Performing Operations; Transporting 2 Active
US10124879B2 Aircraft having improved under-cabin space architecture Emerging Cross-Sectional Technologies 1 Active
US8777509B2 Device and method for assembling two shell elements made from a composite material Emerging Cross-Sectional Technologies 1 Active
US8196863B2 Aircraft horizontal stabilizer Performing Operations; Transporting 1 Active
US11655045B2 Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nesting Performing Operations; Transporting 1 Active
US12377996B2 Propeller propulsion system with T-shaped chassis Emerging Cross-Sectional Technologies 0 Active
US12214890B2 Propeller propulsion unit for an aircraft Emerging Cross-Sectional Technologies 0 Active
US12030659B2 Anterior part of a nacelle for an aircraft propulsion assembly, whose front frame is connected to an outer wall without penetrating it Performing Operations; Transporting 0 Active
US11679889B2 Nacelle of an aircraft propulsion assembly comprising a plurality of damper elements between a front section and a main section, and associated aircraft propulsion assembly Emerging Cross-Sectional Technologies 0 Active
US12397919B2 Assembly for fixing beams, including a support plate and two fixings on respective opposite sides of the support plate Performing Operations; Transporting 0 Active
US11673681B2 Anterior part of a nacelle of an aircraft propulsion assembly having a thermal transition region Emerging Cross-Sectional Technologies 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.