F02K 1/09

Sub-Class

Watch

Stats

Description

Class  F02K : JET-PROPULSION PLANTS


Subclass 1/09: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) Varying effective area of jet pipe or nozzle (F02K 1/3 takes precedence) by axially moving an external member, e.g. a shroud (F02K 1/12 takes precedence)

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
10578018 Geared turbofan engine gearbox arrangementNov 22, 16Mar 03, 20United Technologies Corporation
10578053 Gas turbine engine variable area fan nozzle with ice managementJan 27, 17Mar 03, 20United Technologies Corporation
10502162 Dielectric seal deviceDec 09, 15Dec 10, 19Rohr Inc.
10502159 Electric boost actuation system for translating ringsOct 01, 14Dec 10, 19HAMILTON SUNDSTRAND CORPORATION
10442543 Engine cowling of an aircraft gas turbineMar 31, 16Oct 15, 19Rolls-Royce Deutschland Ltd & Co KG
10443540 Thrust reversal for turbofan gas turbine engineMay 08, 15Oct 15, 19United Technologies Corporation
10422301 Telescoping electrical cableJul 13, 15Sep 24, 19The Boeing Company
10400621 Pivot door thrust reverser with variable area nozzleFeb 27, 14Sep 03, 19United Technologies Corporation
10393065 Variable nozzle apparatusNov 09, 17Aug 27, 19United Technologies Corporation
10378479 Variable effective area fan nozzleOct 19, 15Aug 13, 19General Electric Company
10371089 System for actuating an exhaust cowlJan 20, 15Aug 06, 19United Technologies Corporation
10371094 Nozzle arrangement for a gas turbine engineJul 01, 15Aug 06, 19Rolls Royce plc
10344709 System and method for reducing idle thrust in a translating cowl thrust reverserSep 10, 15Jul 09, 19Honeywell International Inc.
10302041 Sliding nozzle flap assemblyDec 09, 16May 28, 19United Technologies Corporation
10287987 Noise reducing vaneMar 11, 14May 14, 19United Technologies Corporation
10190605 Nacelle for an aircraft turbojet engine provided with a hydraulic roto-linear actuator of a thrust reverser and of a variable-section nozzleJun 18, 18Jan 29, 19SAFRAN NACELLES
10190538 Thrust reverser deviceAug 31, 15Jan 29, 19AIRCELLE
10167815 Thrust reverser of a turbofan pod comprising a single control for movable cowlings and a variable nozzleOct 11, 16Jan 01, 19AIRCELLE
10161356 Integrated thrust reverser actuation systemJun 02, 14Dec 25, 18GE Aviation Systems LLC
10156205 Variable area fan nozzle with drive system health monitoringApr 18, 16Dec 18, 18Rohr, Inc.

more results

Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2019/0162,134 RETENTION OF A NOZZLE ASSEMBLY FOR AN ENGINENov 28, 17May 30, 19Not available
2018/0119,639 AIRCRAFT GAS TURBINE ENGINE NACELLEMay 12, 17May 03, 18Rolls Royce plc
2018/0094,605 TURBOFAN ENGINE FOR A CIVIL SUPERSONIC AIRCRAFTSep 29, 17Apr 05, 18Not available
2017/0356,387 DUAL FUNCTION CASCADE INTEGRATED VARIABLE AREA FAN NOZZLE AND THRUST REVERSERAug 11, 17Dec 14, 17Not available
2015/0308,373 METHOD OF SCHEDULING PRESSURE IN VARIABLE PRESSURE ACTUATION SYSTEMSApr 23, 14Oct 29, 15HAMILTON SUNDSTRAND CORPORATION
2014/0366,554 CROSS REFERENCE TO RELATED APPLICATIONSAug 29, 14Dec 18, 14Not available

more results

Top Owners in This Subclass

Upgrade to the Professional Level to view Top Owners for this Subclass.Learn More

Patents Issued To Date - By Filing Year

Average Time to Issuance