Inventor · disambiguated record
Alain Marc Lucien Bromann
Also filed as: BROMANN ALAIN · BROMANN ALAIN M L · BROMANN ALAIN MARC LUCIEN
20 granted patents·1 pending application·235 citations·filing 1992–2019
94Inventor score
Top patents by PatentIndex Score
21 records- 0191US9926944B2Device for guiding variable pitch diffuser vanes of a turbine engineSNECMA·Filed 2014·Granted Mar 27, 2018·11 cites·8 claims
- 0290US10927699B2Variable-pitch blade control ring for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Feb 23, 2021·9 cites·11 claims
- 0382US7112040B2Method of guiding a blade having a variable pitch angleSNECMA MOTEURS·Filed 2004·Granted Sep 26, 2006·21 cites·21 claims
- 0481US7244098B2Device for adjusting the centering of a ring for synchronizing the control of pivoting vanes in a turbomachineSNECMA·Filed 2006·Granted Jul 17, 2007·21 cites·17 claims
- 0580US9212564B2Annular anti-wear shim for a turbomachineSNECMA·Filed 2013·Granted Dec 15, 2015·7 cites·12 claims
- 0680US7677866B2Device for adjusting the centring of a turbo-engine pivoting vane control synchronization ringSNECMA·Filed 2007·Granted Mar 16, 2010·10 cites·5 claims
- 0779US5288206ATurbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotorSNECMA·Filed 1992·Granted Feb 22, 1994·41 cites·11 claims
- 0878US6200091B1High-pressure turbine stator ring for a turbine engineSNECMA·Filed 1999·Granted Mar 13, 2001·73 cites·3 claims
- 0976US10385721B2System for controlling variable pitch blades for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 20, 2019·2 cites·11 claims
- 1076US7290988B2Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising themSNECMA·Filed 2006·Granted Nov 6, 2007·16 cites·19 claims
- 1171US10502087B2Assembly for controlling variable pitch vanes in a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Dec 10, 2019·1 cites·11 claims
- 1267US10100842B2Cover of a turbomachine centrifugal compressor capable of being rigidly connected via the downstream side near to the upstream edge of same, and turbomachine comprising this coverSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Oct 16, 2018·3 cites·10 claims
- 1364US10330021B2System for controlling variable-pitch vanes for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 25, 2019·1 cites·12 claims
- 1462US7458771B2Retaining of centering keys for rings under variable angle stator vanes in a gas turbine engineSNECMA·Filed 2005·Granted Dec 2, 2008·10 cites·18 claims
- 1560US9528441B2Aircraft turbofan comprising an intermediate ring with simplified downstream supportSNECMA·Filed 2014·Granted Dec 27, 2016·2 cites·9 claims
- 1649US11686205B2Angular sector for turbomachine blading with improved sealingSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jun 27, 2023·0 cites·10 claims
- 1745US11371352B2Device for holding a centripetal radial air sampling memberSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 28, 2022·0 cites·14 claims
- 1844US7214030B2Guide system for the outer pivot of a variable stator vane, for a turbojet statorSNECMA MOTEURS·Filed 2004·Granted May 8, 2007·7 cites·14 claims
- 1943US10648359B2System for controlling variable-setting blades for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 12, 2020·0 cites·11 claims
- 2035US10066509B2Turbomachine part comprising a flange with a drainage deviceSNECMA·Filed 2015·Granted Sep 4, 2018·0 cites·14 claims
- 2134US2004146398A1Assembly arrangement for blades with adjustable settingSNECMA MOTEURS·Filed 2004·Application pending·0 cites
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