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HUREL DUBOIS AVIONS

Overview
  • Total Patents
    88
About

HUREL DUBOIS AVIONS has a total of 88 patent applications. Its first patent ever was published in 1951. It filed its patents most often in France, EPO (European Patent Office) and United States. Its main competitors in its focus markets engines, pumps and turbines, environmental technology and machine tools are LAIR JEAN-PIERRE, LAIR JEAN PIERRE and ANDERSON JACK H.

Patent filings per year

Chart showing HUREL DUBOIS AVIONSs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Fournier Alain 30
#2 Standish Robert 20
#3 Laboure Bernard 11
#4 Kennedy John Francis 7
#5 Standish Robert R 6
#6 Brusson Jean-Pierre 5
#7 Kennedy John F 5
#8 Meyer Pascal 5
#9 Theret Patrice 4
#10 Jouan Jean-Alain 4

Latest patents

Publication Filing date Title
FR2812035A1 Improvements on drive inverters for jet engines of the grid type
FR2811716A1 Improvements on the platform at aerial of aerial, with a common tuyere
EP0926333A1 Thrust reverser configuration
FR2771074A1 Sandwich structure housing and manufacturing method
FR2764000A1 Ejection structure equipped with a push-inverter with two rear doors and a flat output section
EP0852290A1 Thrust reverser for high bypass fan engine
FR2754199A1 Method of manufacturing, by diffusion welding and superplastic deformation, of a part comprising a cavity and application to the creation of stiffeners in an aircraft constituent structure
US5720449A Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors
US5934613A Sealing for a pivoting door reverser
FR2742482A1 Nozzle driver with adjustable section for a jet aircraft engine
US5671598A Forward mounted pivoting door reverser with efflux control device
EP0763654A1 Electro/hydraulic system for a 2 door thrust reverser
FR2734868A1 Two-door push-inverter assembly
FR2728626A1 Drive inverter for a reaction engine with a conveyor edge
FR2718377A1 Device for clipping parts.
FR2712635A1 Door thrust reverser for aircraft engines fitted with security systems preventing inadvertent opening of the doors.
FR2711733A1 Door thrust reverser for jet aircraft engine fitted with an auxiliary flap.
FR2698913A1 Door thrust reverser assembly equipped with a jet control device.
FR2697292A1 Thrust reversing assembly for jet aircraft engine providing an axial leakage space in the reversing position and engine equipped with such an assembly.
FR2695436A1 Thrust reverser door comprising acoustic damping means.