F02K 1/04

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Description

Class  F02K : JET-PROPULSION PLANTS


Subclass 1/04: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) Mounting of an exhaust cone in the jet pipe

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
10570780 Exhaust assembly mounting configurationNov 03, 17Feb 25, 20Rohr Inc.
10563543 Exhaust diffuserMay 31, 16Feb 18, 20General Electric Company
10527000 Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sectionsNov 30, 16Jan 07, 20AIRBUS HELICOPTERS DEUTSCHLAND GMBH
10472976 Machinable CMC insertJun 03, 16Nov 12, 19Rolls-Royce Corporation; Rolls-Royce American Technologies, Inc.;
10443448 Propulsive assembly having decouplable casing portionsAug 30, 16Oct 15, 19SAFRAN AIRCRAFT ENGINES
10337453 Attachment feature for a core panelApr 21, 15Jul 02, 19Rohr Inc.
10316695 Metallic attachment system integrated into a composite structureDec 10, 15Jun 11, 19General Electric Company
10302017 Light weight component with acoustic attenuation and method of makingApr 12, 16May 28, 19United Technologies Corporation
10246198 Alignment system for exhaust installationAug 29, 14Apr 02, 19United Technologies Corporation
RE47304 Nozzle arrangement and method of making the sameAug 31, 17Mar 19, 19Gulfstream Aerospace Corporation
10184402 Ceramic matrix composite turbine exhaust case for a gas turbine engineApr 09, 18Jan 22, 19United Technologies Corporation
10180105 Adjustable cable for exhaust duct liner hangerSep 10, 15Jan 15, 19United Technologies Corporation
10132242 Connecting gas turbine engine annular membersApr 26, 13Nov 20, 18GENERAL ELECTRIC COMPANY
10119424 Attachment assembly and gas turbine engine with attachment assemblyMay 08, 15Nov 06, 18General Electric Company
10100664 Ceramic centerbody and method of makingJul 19, 13Oct 16, 18General Electric Company
10066581 Structure for fastening after-body parts of an aeroengineMar 28, 13Sep 04, 18SAFRAN NACELLES
10036277 Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing deviceJun 12, 13Jul 31, 18SNECMA
10018057 Method of mounting a turbine wheel axial retention deviceFeb 10, 15Jul 10, 18United Technologies Corporation
10006309 Exhaust diffuser for a gas turbineSep 26, 14Jun 26, 18ANSALDO ENERGIA IP UK LIMITED
10006307 Turbine engine casing having a cut-out flangeJul 07, 14Jun 26, 18SNECMA

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
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

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Patents Issued To Date - By Filing Year

Average Time to Issuance