F02K 1/04

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2024/0200,779 DIFFUSION CONE FOR THE REAR PART OF A JET ENGINE INCORPORATING A FLAME-HOLDER RING AT THE TRAILING EDGEApr 15, 22Jun 20, 24Not available
2024/0011,453 FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLENov 03, 21Jan 11, 24Not available
2024/0003,315 FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLENov 03, 21Jan 04, 24SAFRAN NACELLES; SAFRAN CERAMICS;
2023/0407,813 ASSEMBLY FOR A TURBOMACHINENov 03, 21Dec 21, 23SAFRAN NACELLES
2023/0407,814 FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE TURBINENov 04, 21Dec 21, 23Not available
2023/0340,926 SEALING ASSEMBLY FOR A TURBINE EJECTION CONEOct 04, 21Oct 26, 23Not available
2022/0341,373 EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENTSep 02, 20Oct 27, 22Not available
2022/0186,681 DEGASSING TUBE AND EJECTION CONE FOR A TURBINE ENGINE, AS WELL AS TOOL FOR ASSEMBLY THEREOFMar 02, 22Jun 16, 22Not available
2021/0115,876 NOZZLE-TO-ENGINE MOUNT REINFORCEMENT THROUGH WHICH MOUNTING FASTENERS ARE VISIBLEOct 16, 19Apr 22, 21Not available
2020/0291,890 INTEGRATED TAIL CONE AND MOUNTED GENERATORMar 15, 19Sep 17, 20Not available
2020/0291,889 ENGINE EXHAUST SKIN CONNECTION SYSTEMMar 12, 19Sep 17, 20Not available
2019/0323,453 TAIL CONE APPARATUS AND METHODS FOR REDUCING NOZZLE SURFACE TEMPERATURESApr 24, 18Oct 24, 19Not available
2019/0162,079 INTERNAL STRUCTURE OF A PRIMARY EXHAUST DUCTNov 19, 18May 30, 19Not available
2019/0010,894 Gas turbine having a high-speed low-pressure turbine and a turbine caseJul 05, 18Jan 10, 19Not available
2018/0045,138 NOSE CONE ASSEMBLY AND METHOD OF CIRCULATING AIR IN A GAS TURBINE ENGINEFeb 09, 15Feb 15, 18UNITED TECHNOLOGIES CORPORATION
2016/0312,662 EXHAUST ASSEMBLY CENTER BODYApr 22, 15Oct 27, 16ROHR, INC.
2015/0101,338 EXHAUST CENTERBODY FOR A TURBINE ENGINEJul 24, 14Apr 16, 15SNECMA
2015/0083,822 INTEGRATING AFTER-BODY PARTS OF AN AEROENGINEMar 28, 13Mar 26, 15HERAKLES
2015/0028,129 BICONICAL EXHAUST CONE FOR A CIVIL AVIATION JET ENGINEJul 24, 14Jan 29, 15SNECMA
2015/0000,289 GAS EJECTION CONE FOR AIRCRAFT TURBOJET ENGINESSep 12, 14Jan 01, 15AIRCELLE

Showing 1 to 20 of 25 results