Inventor · disambiguated record
Guillaume Bodard
Also filed as: BODARD GUILLAUME · BODARD GUILLAUME MICHEL MARCEL
7 granted patents·3 pending applications·10 citations·filing 2011–2022
75Inventor score
Top patents by PatentIndex Score
10 records- 0169US9617954B2Primary cowl of a turbofan comprising a rotating ring having micro-jetsSNECMA·Filed 2012·Granted Apr 11, 2017·4 cites·8 claims
- 0259US9249755B2Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzleSNECMA·Filed 2013·Granted Feb 2, 2016·2 cites·15 claims
- 0358US9938901B2Attachment pylon for a turbine engineSNECMA·Filed 2012·Granted Apr 10, 2018·3 cites·11 claims
- 0453US10995702B2Heating system for convergent-divergent secondary nozzleSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted May 4, 2021·0 cites·8 claims
- 0553US8881502B2Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling itSNECMA·Filed 2013·Granted Nov 11, 2014·1 cites·13 claims
- 0651US11149685B2Modified acoustic secondary nozzleSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Oct 19, 2021·0 cites·11 claims
- 0742US2025237182A1Outlet nozzle provided with chevrons for aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 0839US2016215727A1Afterbody for a mixed-flow turbojet engine comprising a lobed mixer and chevrons with a non-axisymmetric inner surfaceSNECMA·Filed 2014·Application pending·0 cites
- 0931US9422887B2Device for reducing the noise emitted by the jet of an aircraft propulsion engineBODARD GUILLAUME·Filed 2011·Granted Aug 23, 2016·0 cites·6 claims
- 1031US2012192543A1Exhaust nozzle for a bypass airplane turbojet having a deployable secondary cover and a retractable central bodyAEBERLI SEBASTIEN JEAN-PAUL·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →