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Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
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Patrick Morel — 12 Patents

SNSnecma: 7 patents #102 of 1,717Top 6%
SMSnecma Moteurs: 3 patents #48 of 501Top 10%
ANAlcatel N.V.: 1 patents #259 of 816Top 35%
Éragny-sur-Oise, FR: #3 of 55 inventorsTop 6%
Overall (All Time): #396,045 of 4,157,543Top 10%
12 Patents All Time
Patrick Morel has been granted 12 US patents while listed as an inventor at Snecma. The first was granted in 1990 and the most recent in January 2014. Patrick Morel ranks #396,045 of 4,157,543 US inventors in our database (top 9.5%). Patent records list Patrick Morel in Éragny-sur-Oise, FR.

Patents per Year

Patents granted per year, 1990 to 2014Bar chart with a peak of 3 patents in 2007.peak 31990: 1 patents19901998: 1 patents19982004: 1 patents20042007: 3 patents20072008: 1 patents20082009: 1 patents20092010: 2 patents20102011: 1 patents20112014: 1 patents2014

Issued Patents All Time

Showing 1–12 of 12 patents

Patent #TitleCo-InventorsDate
8622699 Device adapted to be fitted with propeller blades Francois Gallet, Wouter Balk 2014-01-07
8042341 Turbojet engine accessory gear box driveshaft; modular additional accessory Gilles Alain Charier, Regis Eugene Henri Servant 2011-10-25
7785066 Bleed system for a low-pressure compressor of a turbomachine Eric Stephan Bil, Gilles Alain Charier, Philippe Jacques Pierre Fessou 2010-08-31
7661261 Acoustic flow straightener for turbojet engine fan casing Jacques Michel Albert Julliard, Olivier Michael Molinari, Georges Jean Xavier Riou 2010-02-16
7552591 Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine Jacques Rene Bart, Bruno Albert Beutin 2009-06-30
7448808 Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement Gael Bouchy, Alain Mazelet, Daniel Martin 2008-11-11
7299621 Three-spool by-pass turbojet with a high by-pass ratio Jacques Rene Bart, Fabienne Lacorre, Yann Lebret, Vanessa Le Rousseau 2007-11-27
7237959 Breakable coupling system for a turbojet fan shaft Gael Bouchy, Bertrand Jean Joseph Marie Heurtel, Eric Masson, Bien-Aime Rakotondrainibe, Pierre Pandelakis +2 more 2007-07-03
7195444 Turbomachine with a decoupling device common to first and second bearings of its drive shaft, compressor comprising the decoupling device and decoupling device Michel Gilbert Roland Brault, Zoltan Zsiga, Gael Bouchy, Pierre Pandelakis 2007-03-27
6799416 Device for supporting and recentering the shaft of a turbojet fan after uncoupling Daniel Plona 2004-10-05
5776229 Oil separator rotor for lubrication enclosure Gerard Antoine Gilbert Blanes, Rene Joseph Antoine Cannavo, Jean-Bernard Forgue, Francis Georges Albert Garnier, Michel Hugues +2 more 1998-07-07
4972357 Digital filter with integrated decimation 1990-11-20