Inventor
Georges Habarou
Inventor
Le Bouscat, FR
Overview
Patents· 15 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines19%
Y02TClimate change mitigation technologies related to transportation16%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers14%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants12%
F02KJet-propulsion plants9%
F02CGas-turbine plants7%
F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g7%
F23MCasings, linings, walls or doors specially adapted for combustion chambers, e.g. firebridges5%
B29BPreparation or pretreatment of the material to be shaped2%
D03DWoven fabrics2%
PatentTitleYear
9,080,463'Turbine ring assembly'20158,951,017'Turbomachine blade, a rotor, a low pressure turbine, and a turbomachine fitted with such a blade'20158,496,431'Turbine ring assembly for gas turbine'20138,424,312'Exhaust system for gas turbine'20138,257,029'Turbine ring assembly for gas turbine'20128,146,372'Gas turbine combustion chamber having inner and outer walls subdivided into sectors'20128,141,371'Gas turbine combustion chamber made of CMC material and subdivided into sectors'20127,249,462'Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine'20077,168,253'Monobloc flameholder arm for an afterburner device of a bypass turbojet'20076,988,369'Combustion chamber sealing ring, and a combustion chamber including such a ring'20066,732,532'Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing'20046,385,965'System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies'20026,378,294'System for activating an adjustable tube by means of an elastic ring for a thrust nozzle'20025,348,598'Method of manufacturing a gun barrel provided with a lining'19944,669,954'Abradable turbine rings and turbines thus obtained'1987Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1987–2015Based in Le Bouscat, FR· patent location history
2002–2015Patents assigned to SNECMA (5)· patent assignee history
2012–2015Patents assigned to HABAROU GEORGES (7)· patent assignee history
2012–2013Patents assigned to SNECMA PROPULSION SOLIDE (5)· patent assignee history
2012–2013Patents assigned to BOUILLON ERIC (3)· patent assignee history
2012–2015Patents assigned to MATEO JULIEN (3)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| HABAROU GEORGESself | 7 | 2012–2015 |
| SNECMA | 5 | 2002–2015 |
| SNECMA PROPULSION SOLIDE | 5 | 2012–2013 |
| BOUILLON ERIC | 3 | 2012–2013 |
| MATEO JULIEN | 3 | 2012–2015 |
Locations
| Location | Patents | Span |
|---|---|---|
| Le Bouscat, FR | 15 | 1987–2015 |