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name:-0.0076680183410645
name:-0.0077240467071533
name:-0.0074048042297363
Boutaleb; Mohamed-Lamine Patent Filings

Boutaleb; Mohamed-Lamine

Patent Applications and Registrations

Patent applications and USPTO patent grants for Boutaleb; Mohamed-Lamine.The latest application filed is for "aircraft propulsion assembly comprising air-liquid heat exchangers".

Company Profile
8.5.7
  • Boutaleb; Mohamed-Lamine - Moissy-Cramayel FR
  • Boutaleb; Mohamed-Lamine - Paris 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
PatentDate
Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved design
Grant 11,125,091 - Zaccardi , et al. September 21, 2
2021-09-21
Outlet guide vane for turbomachine, comprising a lubricant cooling passage equipped with a thermal conducting matrix compressed between the intrados and extrados walls
Grant 11,015,468 - Zaccardi , et al. May 25, 2
2021-05-25
Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function
Grant 10,697,312 - Boutaleb , et al.
2020-06-30
Aircraft Propulsion Assembly Comprising Air-liquid Heat Exchangers
App 20200049028 - Oriol; Sebastien ;   et al.
2020-02-13
Aircraft Turbo Machine Exit Guide Vane Comprising A Bent Lubricant Pas Sage Of Improved Design
App 20190338661 - ZACCARDI; Cedric ;   et al.
2019-11-07
Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vane
Grant 10,392,952 - Zaccardi , et al. A
2019-08-27
Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function
Grant 10,378,556 - Zaccardi , et al. A
2019-08-13
Outlet Guide Vane For Turbomachine, Comprising A Lubricant Cooling Passage Equipped With A Thermal Conducting Matrix Compressed Between The Intrados And Extrados Walls
App 20190078452 - ZACCARDI; Cedric ;   et al.
2019-03-14
Outlet Guide Vane For Aircraft Turbomachine, With Improved Lubricant Cooling Function
App 20180258779 - Boutaleb; Mohamed-Lamine ;   et al.
2018-09-13
Output Director Vane For An Aircraft Turbine Engine, With An Improved Lubricant Cooling Function Using A Heat Conduction Matrix Housed In An Inner Duct Of The Vane
App 20170284417 - ZACCARDI; Cedric ;   et al.
2017-10-05
Outlet Guide Vane For Aircraft Turbine Engine, Presenting An Improved Lubricant Cooling Function
App 20170204879 - ZACCARDI; Cedric ;   et al.
2017-07-20

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