Assignee
VOLVO AERO CORP
SE·63 granted patents·28 pending applications·926 citations·filing 1992–2010
Top patents by PatentIndex Score
91 records- 0197US7404294B2Gas turbine and a method for controlling a gas turbineVOLVO AERO CORP·Filed 2005·Granted Jul 29, 2008·117 cites·10 claims
- 0296US7389583B2Method of manufacturing a stator componentVOLVO AERO CORP·Filed 2005·Granted Jun 24, 2008·32 cites·17 claims
- 0388US7766213B2Device and method for monitoring a welding area and an arrangement and a method for controlling a welding operationVOLVO AERO CORP·Filed 2004·Granted Aug 3, 2010·73 cites·29 claims
- 0486US7557324B2Backstream-preventing thermal spraying deviceVOLVO AERO CORP·Filed 2003·Granted Jul 7, 2009·73 cites·16 claims
- 0583US7614150B2Method for manufacturing a stator or rotor componentVOLVO AERO CORP·Filed 2003·Granted Nov 10, 2009·30 cites·14 claims
- 0678US7753311B2Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engineVOLVO AERO CORP·Filed 2005·Granted Jul 13, 2010·16 cites·14 claims
- 0777US7740161B2Engine wall structure and a method of producing an engine wall structureVOLVO AERO CORP·Filed 2005·Granted Jun 22, 2010·8 cites·14 claims
- 0877US6467253B1Nozzle structure for rocket nozzles having cooled nozzle wallVOLVO AERO CORP·Filed 1998·Granted Oct 22, 2002·39 cites·8 claims
- 0976US7200933B2Method for manufacturing a stator componentVOLVO AERO CORP·Filed 2003·Granted Apr 10, 2007·35 cites·18 claims
- 1075US6591499B1Method for manufacturing outlet nozzles for rocket enginesVOLVO AERO CORP·Filed 1999·Granted Jul 15, 2003·27 cites·8 claims
- 1174US6945032B2Method for manufacturing outlet nozzles for rocket enginesVOLVO AERO CORP·Filed 2004·Granted Sep 20, 2005·13 cites·5 claims
- 1272US7802962B2Bearing support structure and a gas turbine engine comprising the bearing support structureVOLVO AERO CORP·Filed 2005·Granted Sep 28, 2010·16 cites·20 claims
- 1371US8002168B2Method of producing an engine wall structureVOLVO AERO CORP·Filed 2005·Granted Aug 23, 2011·6 cites·18 claims
- 1471US7299622B2Component for being subjected to high thermal load during operation and a method for manufacturing such a componentVOLVO AERO CORP·Filed 2004·Granted Nov 27, 2007·20 cites·28 claims
- 1571US6920750B2Rocket engine member and a method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Jul 26, 2005·15 cites·28 claims
- 1668US7544040B2Support structure in a turbine or compressor device and a method for assembling the structureVOLVO AERO CORP·Filed 2006·Granted Jun 9, 2009·17 cites·7 claims
- 1768US6915640B2Method and a device for supplying fuel to a combustion chamberVOLVO AERO CORP·Filed 2003·Granted Jul 12, 2005·16 cites·9 claims
- 1867US6789316B2Method for manufacturing outlet nozzles for rocket enginesVOLVO AERO CORP·Filed 2003·Granted Sep 14, 2004·12 cites·14 claims
- 1965US6797912B2Method and a device for manufacturing a stator component or rotor componentVOLVO AERO CORP·Filed 2003·Granted Sep 28, 2004·11 cites·16 claims
- 2063US7991593B2Optimisation of sequential combinatorial processVOLVO AERO CORP·Filed 2004·Granted Aug 2, 2011·12 cites·64 claims
- 2163US7520055B2Method for manufacturing a stator or rotor componentVOLVO AERO CORP·Filed 2004·Granted Apr 21, 2009·9 cites·15 claims
- 2263US6883331B2Method and arrangement for providing a gas turbine, and engine-braking thereforeVOLVO AERO CORP·Filed 2003·Granted Apr 26, 2005·18 cites·25 claims
- 2362US7905448B2Annular torsional rigid static component for an aircraft engineVOLVO AERO CORP·Filed 2005·Granted Mar 15, 2011·9 cites·18 claims
- 2462US7900460B2Outlet device for a jet engine and a jet engine comprising such an outlet deviceVOLVO AERO CORP·Filed 2005·Granted Mar 8, 2011·9 cites·18 claims
- 2562US6901661B2Method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine componentVOLVO AERO CORP·Filed 2003·Granted Jun 7, 2005·9 cites·21 claims
- 2662US5816050ALow-emission combustion chamber for gas turbine enginesVOLVO AERO CORP·Filed 1994·Granted Oct 6, 1998·27 cites·6 claims
- 2761US5549770AMethod for manufacturing compositesVOLVO AERO CORP·Filed 1993·Granted Aug 27, 1996·16 cites·16 claims
- 2860US6034318AThermoelectric generator unitVOLVO AERO CORP·Filed 1997·Granted Mar 7, 2000·26 cites·10 claims
- 2959US7798778B2Wheel for a rotating flow machineVOLVO AERO CORP·Filed 2004·Granted Sep 21, 2010·10 cites·29 claims
- 3058US6907662B2Method for manufacturing outlet nozzles for rocket enginesVOLVO AERO CORP·Filed 2003·Granted Jun 21, 2005·5 cites·12 claims
- 3158US6799418B2Rocket engine member and method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Oct 5, 2004·7 cites·18 claims
- 3257US7570369B2Method and a device for measurement of edgesVOLVO AERO CORP·Filed 2005·Granted Aug 4, 2009·4 cites·36 claims
- 3354US7234294B1Outlet nozzle and a method for manufacturing an outlet nozzleVOLVO AERO CORP·Filed 2003·Granted Jun 26, 2007·4 cites·12 claims
- 3452US6251317B1Method for manufacturing a ceramic composite materialVOLVO AERO CORP·Filed 1997·Granted Jun 26, 2001·15 cites·3 claims
- 3551US7302794B2Rocket engine member and a method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Dec 4, 2007·11 cites·18 claims
- 3651US5713522AExhaust nozzle flap for turbojet afterburnerVOLVO AERO CORP·Filed 1996·Granted Feb 3, 1998·28 cites·2 claims
- 3750US8347601B2Device for pivoting at least one pivotable element in a gas turbine engineVOLVO AERO CORP·Filed 2006·Granted Jan 8, 2013·4 cites·21 claims
- 3849US6334303B1Flameholder device for afterburners in gas turbine enginesVOLVO AERO CORP·Filed 1997·Granted Jan 1, 2002·18 cites·8 claims
- 3948US2010116792A1Method of joining pieces of metal material and a welding deviceVOLVO AERO CORP·Filed 2006·Application pending·0 cites
- 4047US7341176B2Method of tying two or more components togetherVOLVO AERO CORP·Filed 2003·Granted Mar 11, 2008·6 cites·19 claims
- 4147US6960542B2Method for preparation of test bodiesVOLVO AERO CORP·Filed 2003·Granted Nov 1, 2005·2 cites·6 claims
- 4247US5567518ACeramic composite, particularly for use at temperatures above 1400 degrees celsiusVOLVO AERO CORP·Filed 1992·Granted Oct 22, 1996·10 cites·5 claims
- 4346US7185498B1Modular gas turbineVOLVO AERO CORP·Filed 2003·Granted Mar 6, 2007·9 cites·11 claims
- 4445US7481059B2Method and apparatus for providing an afterburner fuel-feed arrangementVOLVO AERO CORP·Filed 2004·Granted Jan 27, 2009·8 cites·15 claims
- 4545US2005246894A1Method for manufacturing a stator or rotor componentVOLVO AERO CORP·Filed 2005·Application pending·0 cites
- 4645US2010180575A1Engine wall structure and a method of producing an engine wall structureVOLVO AERO CORP·Filed 2010·Application pending·0 cites
- 4744US7096675B2Device for a combustion chamber in a gas turbine for controlling the intake of gas to a combustion zoneVOLVO AERO CORP·Filed 2004·Granted Aug 29, 2006·8 cites·27 claims
- 4843US2010192351A1Method for producing an annular wall structureVOLVO AERO CORP·Filed 2007·Application pending·0 cites
- 4941US7258934B2Thermal barrier coating and a method of applying such a coatingVOLVO AERO CORP·Filed 2003·Granted Aug 21, 2007·8 cites·22 claims
- 5040US7779541B2Method for manufacturing a stator or rotor componentVOLVO AERO CORP·Filed 2004·Granted Aug 24, 2010·2 cites·2 claims
Showing the top 50 of 91 patent records by PatentIndex Score.
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