Bertucchi; Jean

Patent Applications and Registrations

Patent applications and USPTO patent grants for Bertucchi; Jean.The latest application filed is for "dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan".

Company Profile

0.10.11

Bertucchi; Jean - Moissy-Cramayel FR
BERTUCCHI; Jean - Moissy-Cramayel Cedex FR
Bertucchi; Jean - Thiais FR

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan Grant 11,221,020 - Madiot , et al. January 11, 2	2022-01-11
Dimensioning Of The Skeleton Angle Of The Trailing Edge Of The Arms Crossing The By-pass Flow Of A Turbofan App 20180252230 - MADIOT; Ghislain Maxime Romuald ; et al.	2018-09-06
Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Grant 9,915,227 - Leyko , et al. March 13, 2	2018-03-13
Convergent-divergent nozzle for a turbine engine Grant 9,683,516 - Leyko , et al. June 20, 2	2017-06-20
Pylon for fixing an aircraft engine having unducted pusher propellers Grant 9,682,783 - Bensilum , et al. June 20, 2	2017-06-20
Turbomachine comprising a device for the cooling of a pylon Grant 9,540,109 - Leyko , et al. January 10, 2	2017-01-10
Assembly formed by a turbine engine and a system for attaching it to an aircraft structure Grant 9,488,106 - Gaillot , et al. November 8, 2	2016-11-08
Pipe having an upstream core having a sharp curvature Grant 9,341,082 - Bensilum , et al. May 17, 2	2016-05-17
Turbomachine Comprising A Device For The Cooling Of A Pylon App 20150284098 - LEYKO; Matthieu ; et al.	2015-10-08
Convergent-divergent Nozzle For A Turbine Engine App 20150033747 - Leyko; Matthieu ; et al.	2015-02-05
Assembly Formed By A Turbine Engine And A System For Attaching It To An Aircraft Structure App 20140202169 - Gaillot; Mathieu ; et al.	2014-07-24
Discharge System Of A Separated Twin-flow Turbojet For An Aircraft, Corresponding Turbojet And Associated Design Method App 20140061331 - LEYKO; Matthieu ; et al.	2014-03-06
Pipe Having An Upstream Core Having A Sharp Curvature App 20130336772 - Bensilum; Stephane Emmanuel Daniel ; et al.	2013-12-19
Secondary-air Nozzle Of A Two-flow Jet Engine Having Separated Flows Including A Grid Thrust Reverser App 20130032642 - Bensilum; Stephane ; et al.	2013-02-07
Pylon For Fixing An Aircraft Engine Having Unducted Pusher Propellers App 20120145824 - Bensilum; Stephane Emmanuel Daniel ; et al.	2012-06-14

uspto.report is an independent third-party trademark research tool that is not affiliated, endorsed, or sponsored by the United States Patent and Trademark Office (USPTO) or any other governmental organization. The information provided by uspto.report is based on publicly available data at the time of writing and is intended for informational purposes only.

While we strive to provide accurate and up-to-date information, we do not guarantee the accuracy, completeness, reliability, or suitability of the information displayed on this site. The use of this site is at your own risk. Any reliance you place on such information is therefore strictly at your own risk.

All official trademark data, including owner information, should be verified by visiting the official USPTO website at www.uspto.gov. This site is not intended to replace professional legal advice and should not be used as a substitute for consulting with a legal professional who is knowledgeable about trademark law.