SAFRAN NACELLES
Patent Owner
Stats
- 142 US PATENTS IN FORCE
- 12 US APPLICATIONS PENDING
- Mar 13, 2018 most recent publication
Details
- 142 Issued Patents
- 0 Issued in last 3 years
- 0 Published in last 3 years
- 1,429 Total Citation Count
- Nov 12, 1997 Earliest Filing
- 5 Expired/Abandoned/Withdrawn Patents
Patent Activity in the Last 10 Years
Technologies
Intl Class
Technology
Matters
Rank in Class
Top Patents (by citation)
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Recent Publications
Publication #
Title
Filing Date
Pub Date
Intl Class
2018/0066,608 COMPOSITE PANEL AND AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING SUCH A PANELNov 13, 17Mar 08, 18[F02K, B32B]
2017/0370,247 METHOD FOR MANUFACTURING A PREFORM MADE OF WOVEN REINFORCEMENT FIBERS HAVING A VARIABLE CROSS-SECTIONAug 09, 17Dec 28, 17[D03D, F02K, F01D]
2017/0321,633 NACELLE REAR ASSEMBLY FOR A TURBOJET ENGINE COMPRISING A CRADLE FOR A CORE-TYPE MASTJul 19, 17Nov 09, 17[F02K, B64D, F02C, F01D]
2017/0321,634 NACELLE REAR ASSEMBLY FOR A TURBOJET ENGINE COMPRISING A SUSPENSION CRADLEJul 19, 17Nov 09, 17[F02K, B64D]
2017/0292,453 ACOUSTIC ATTENUATION PANEL FOR A TURBOJET ENGINE NACELLEJun 22, 17Oct 12, 17[F02K, F02C]
2017/0232,693 METHOD OF REPAIRING A PERFORATED SKIN OF A PANEL USING A DOUBLERMay 03, 17Aug 17, 17[B29C]
2017/0203,378 METHOD FOR PRODUCING AN ESPECIALLY LARGE AERONAUTICAL PARTMar 24, 17Jul 20, 17[B23K, F01D]
2017/0174,353 PROPULSION UNIT FOR AN AIRCRAFT AND METHOD FOR OPENING A MOVABLE COWL OF SAID PROPULSION UNITMar 08, 17Jun 22, 17[F02K, B64D, F04D]
2017/0175,308 PREFORM FOR A CURVED COMPOSITE STIFFENER FOR AN AXISYMMETRIC PART SUCH AS A COLLARMar 09, 17Jun 22, 17[D03D, B29C, D03J]
Recent Patents
Patent #
Title
Filing Date
Issue Date
Intl Class
9856826 Nacelle rear assembly for a turbojet engine comprising a suspension cradleJul 19, 17Jan 02, 18[F02K, B64D, F02C]
9518509 Method for manufacturing a structure with cellular cores for a turbojet nacelleMar 02, 15Dec 13, 16[F02K, G10K, F02C, B32B]
9518533 Device and method for assembling a fixed thrust reverser structure of an aircraft propulsion assemblyDec 12, 14Dec 13, 16[F02K, B64F, F01D]
9518535 Assembly including a reverse thrust device and system for actuating said deviceNov 30, 12Dec 13, 16[F02K]
9481054 Method for manufacturing an air intake structure for a turbojet engine nacelleAug 02, 13Nov 01, 16[B23P, B29C, B64D]
9476383 Aircraft turbojet engine thrust reverser with a reduced number of latchesJul 17, 13Oct 25, 16[F02K, B64D]
Expired/Abandoned/Withdrawn Patents
Patent #
Title
Status
Filing Date
Issue/Pub Date
Intl Class
8668441 Deformable structural framework for a turbofan nacelleExpiredOct 15, 07Mar 11, 14[B64D, F02C]
8636107 Method for repairing at least a portion of an acoustic panelExpiredJul 12, 13Jan 28, 14[E04B, B32B]
8528857 Translatable jet engine thrust reverser configuration providing improved maintenance accessExpiredNov 19, 07Sep 10, 13[F02K]
8393435 Trailing edge for an aircraft engine, of the type with moving chevronsExpiredFeb 26, 09Mar 12, 13[F02K]
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