Inventor · disambiguated record
Guilhem Seize
Also filed as: SEIZE GUILHEM
10 granted patents·123 citations·filing 2010–2021
87Inventor score
Files withSAFRAN AIRCRAFT ENGINES2SEIZE GUILHEM2BELLABAL FRANCOIS1BELLABAL FRANCOIS ROBERT1DUNLEAVY PATRICK1
Top patents by PatentIndex Score
10 records- 0193US8600611B2System and method for measuring fatigue for mechanical components of an aircraft and aircraft maintenance methodSEIZE GUILHEM·Filed 2010·Granted Dec 3, 2013·91 cites·12 claims
- 0290US11970280B2Assembly between an aircraft pylon and a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Apr 30, 2024·4 cites·11 claims
- 0380US9121347B2Link between the exhaust casing and a structural ring of the fan duct of a jet engineBELLABAL FRANCOIS ROBERT·Filed 2011·Granted Sep 1, 2015·8 cites·9 claims
- 0473US9828877B2Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rodsRIVIERE THOMAS GÉRARD DANIEL·Filed 2012·Granted Nov 28, 2017·7 cites·4 claims
- 0569US9067688B2Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension systemBELLABAL FRANCOIS·Filed 2011·Granted Jun 30, 2015·7 cites·8 claims
- 0667US11851201B2Turbomachine comprising a means of suspensionSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 26, 2023·2 cites·20 claims
- 0755US9359954B2In-line removable heat shield for a turbomachine suspension yokeSNECMA·Filed 2013·Granted Jun 7, 2016·1 cites·14 claims
- 0853US9321537B2Beam for suspending a turboshaft engine from an aircraft structureDUNLEAVY PATRICK·Filed 2010·Granted Apr 26, 2016·2 cites·16 claims
- 0944US9157334B2Dual-flow turbomachine for aircraft, including structural means of rigidifying the central casingGREDE AUDREY·Filed 2010·Granted Oct 13, 2015·1 cites·7 claims
- 1040US9169743B2Metallic annular connection structure for aircraft turbomachineSEIZE GUILHEM·Filed 2010·Granted Oct 27, 2015·0 cites·5 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →