F02K

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Description

JET-PROPULSION PLANTS (arrangement or mounting of jet-propulsion plants in land vehicles or vehicles in general B60K; arrangement or mounting of jet-propulsion plants in waterborne vessels B63H; controlling aircraft attitude, flight direction, or altitude by jet reaction B64C; arrangement or mounting of jet-propulsion plants in aircraft B64D; plants characterised by the power of the working fluid being divided between jet propulsion and another form of propulsion, e.g. propeller, F02B, F02C; features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C)

Subclasses

Not Available
Subclass Title
1/00 Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97)
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
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)
1/08 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 or transversely deforming an internal member, e.g. the exhaust cone
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)

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Recent Patents

Not Available
Patent #TitleFiling DateIssue DatePatent Owner
9,120,250 Structure comprising an annular housing made of composite material Oct 06, 11 Sep 01, 15 GKN AEROSPACE SERVICES LIMITED, GKN AEROSPACE SERVICES LIMITED
9,121,346 Pump system for TMS AOC reduction Mar 14, 12 Sep 01, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,121,347 Link between the exhaust casing and a structural ring of the fan duct of a jet engine Feb 09, 11 Sep 01, 15 SNECMA, SNECMA
9,121,367 Gas turbine engine compressor arrangement Apr 24, 13 Sep 01, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,121,368 Efficient, low pressure ratio propulsor for gas turbine engines May 31, 12 Sep 01, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,121,369 Nozzle arrangement and method of making the same Jul 03, 12 Sep 01, 15 GULFSTREAM AEROSPACE CORPORATION, GULFSTREAM AEROSPACE CORPORATION
9,121,412 Efficient, low pressure ratio propulsor for gas turbine engines Jul 05, 11 Sep 01, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,121,465 Bleed outlet structure for a bleed valve Aug 22, 11 Sep 01, 15 ROLLS-ROYCE PLC, ROLLS ROYCE PLC
9,115,602 Exhaust diffuser including flow mixing ramp for a gas turbine engine Oct 15, 13 Aug 25, 15 SIEMENS AKTIENGESELLSCHAFT, SIEMENS AKTIENGESELLSCHAFT
9,115,666 Slotted multi-nozzle grid with integrated cooling channels Oct 09, 12 Aug 25, 15 RAYTHEON COMPANY, RAYTHEON COMPANY
9,115,668 Thrust reversal device Jul 15, 10 Aug 25, 15 AIRCELLE, AIRCELLE
9,115,669 Gas turbine engine exhaust nozzle cooling valve Oct 28, 11 Aug 25, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,115,897 Gas turbine engine systems and methods involving enhanced fuel dispersion Sep 04, 08 Aug 25, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,108,385 Honeycomb core structure for use in a structural panel for a jet engine nacelle Jan 27, 10 Aug 18, 15 AIRCELLE, AIRCELLE
9,108,711 Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets Mar 18, 10 Aug 18, 15 SOUTHERN METHODIST UNIVERSITY, SOUTHERN METHODIST UNIVERSITY
9,109,462 Energy-absorbing fan case for a gas turbine engine Dec 15, 11 Aug 18, 15 UNITED TECHNOLOGIES CORPORATION, UNITED TECHNOLOGIES CORPORATION
9,109,465 Gas turbine engine fan casing having a flange for fastening pieces of equipment Feb 05, 13 Aug 18, 15 SNECMA, SNECMA
9,109,509 Unit for an aircraft thruster Nov 07, 12 Aug 18, 15 AIRCELLE, AIRCELLE
9,109,535 Propulsion system and method May 03, 10 Aug 18, 15 AIRCELLE, Not available
9,109,536 Engine thrust reverser lock Mar 14, 13 Aug 18, 15 WOODWARD HRT, INC., WOODWARD HRT, INC.

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Recent Publications

Not Available
Publication #TitleFiling DatePub DatePatent Owner
2015/0240,745 ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLE Apr 30, 14 Aug 27, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0240,746 INJECTOR PLATE FOR A ROCKET ENGINE Jul 11, 14 Aug 27, 15 ATYAM, DEEPAK,
2015/0233,251 GAS TURBINE ENGINE AIRFOIL Feb 18, 15 Aug 20, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0233,252 GAS TURBINE ENGINE AIRFOIL Feb 19, 15 Aug 20, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0233,298 REDUCTION IN JET FLAP INTERACTION NOISE WITH GEARED TURBINE ENGINE Feb 22, 13 Aug 20, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0233,322 ACTUATING DEVICE INCLUDING A PRIMARY LOCKING DEVICE Oct 08, 13 Aug 20, 15 SAGEM DEFENSE SECURITE,
2015/0233,323 GAS TURBINE ENGINE AIRFOIL Feb 19, 15 Aug 20, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0233,324 TWO-MODE IGNITOR AND A TWO-MODE METHOD OF INJECTION FOR IGNITING A ROCKET ENGINE Aug 13, 13 Aug 20, 15 SNECMA,
2015/0224,840 Airtrain & Hydroairtrain Feb 10, 14 Aug 13, 15 ,
2015/0226,155 THRUST DEFLECTING DEVICE AND AIRCRAFT ENGINE Jun 09, 14 Aug 13, 15 MTU AERO ENGINES AG,
2015/0226,156 Non-Axisymmetric Fixed or Variable Fan Nozzle for Boundary Layer Ingestion Propulsion Jun 04, 14 Aug 13, 15 UNITED TECHNOLOGIES CORPORATION,
2015/0226,157 THRUST REVERSER CASCADE Feb 10, 14 Aug 13, 15 MRA SYSTEMS, INC.,

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Patents Issued To Date - By Filing Year

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