F02K 1/06

Sub-Class

Watch

Stats

Description

Class  F02K : JET-PROPULSION PLANTS


Subclass 1/06: 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)

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
10605201 Gas turbine exhaust cooling systemJun 22, 17Mar 31, 20Rolls-Royce plc
10605202 Efficient, low pressure ratio propulsor for gas turbine enginesMar 27, 18Mar 31, 20United Technologies Corporation
10578018 Geared turbofan engine gearbox arrangementNov 22, 16Mar 03, 20United Technologies Corporation
10570852 Moveable exhaust plug linerSep 21, 17Feb 25, 20United Technologies Corporation
10550797 Turbine engines with variable area nozzleFeb 11, 15Feb 04, 20MRA Systems, LLC
10514002 Variable exhaust mixer and cooler for a three-stream gas turbine engineSep 21, 16Dec 24, 19United Technologies Corporation
10502159 Electric boost actuation system for translating ringsOct 01, 14Dec 10, 19HAMILTON SUNDSTRAND CORPORATION
10487690 Actively controlled cooling air exhaust door on an aircraft engine nacelleAug 18, 14Nov 26, 19Rohr, Inc.
10436148 Convergent-divergent nozzleMar 24, 16Oct 08, 19Rolls Royce plc
10385805 Thrust vectoring nozzleOct 04, 17Aug 20, 19Rolls Royce plc
10371093 Aircraft nozzle with a variable nozzle area of a second flow pathMar 07, 14Aug 06, 19Rolls-Royce North American Technologies Inc.
10371089 System for actuating an exhaust cowlJan 20, 15Aug 06, 19United Technologies Corporation
10309315 Variable area nozzle assisted gas turbine engine restartingMar 29, 16Jun 04, 19United Technologies Corporation
10309343 Split sleeve hidden door thrust reverserNov 06, 14Jun 04, 19Rohr, Inc.
10302041 Sliding nozzle flap assemblyDec 09, 16May 28, 19United Technologies Corporation
10302042 Variable area fan nozzle with wall thickness distributionJun 09, 16May 28, 19United Technologies Corporation
10288009 Efficient, low pressure ratio propulsor for gas turbine enginesAug 31, 16May 14, 19United Technologies Corporation
10233868 Efficient, low pressure ratio propulsor for gas turbine enginesAug 31, 16Mar 19, 19United Technologies Corporation
10197007 Method and system for controlling core cowl vent areaJan 14, 16Feb 05, 19General Electric Company
10184425 Fiber optic sensing for variable area fan nozzlesJan 28, 16Jan 22, 19The Boeing Company

more results

Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2019/0323,452 TURBOFAN ENGINEMar 21, 19Oct 24, 19Rolls Royce plc
2019/0078,533 LINKAGE ASSEMBLYSep 08, 17Mar 14, 19Not available
2015/0275,766 GEARED TURBINE ENGINE WITH A D-DUCT AND A THRUST REVERSEROct 10, 13Oct 01, 15UNITED TECHNOLOGIES CORPORATION
2015/0252,751 GEARED GAS TURBINE ENGINE INTEGRATED WITH A VARIABLE AREA FAN NOZZLE WITH REDUCED NOISEMar 01, 13Sep 10, 15UNITED TECHNOLOGIES CORPORATION
2010/0162,683 TURBOFAN ENGINEOct 12, 06Jul 01, 10UNITED TECHNOLOGIES CORPORATION

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