Inventor · disambiguated record
Jan Häggander
Also filed as: HAEGGANDER JAN · HAGGANDER JAN
14 granted patents·1 pending application·138 citations·filing 1996–2007
92Inventor score
Top patents by PatentIndex Score
15 records- 0177US6467253B1Nozzle structure for rocket nozzles having cooled nozzle wallVOLVO AERO CORP·Filed 1998·Granted Oct 22, 2002·39 cites·8 claims
- 0271US7299622B2Component 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
- 0371US6920750B2Rocket engine member and a method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Jul 26, 2005·15 cites·28 claims
- 0467US6789316B2Method for manufacturing outlet nozzles for rocket enginesVOLVO AERO CORP·Filed 2003·Granted Sep 14, 2004·12 cites·14 claims
- 0558US6799418B2Rocket engine member and method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Oct 5, 2004·7 cites·18 claims
- 0654US7234294B1Outlet nozzle and a method for manufacturing an outlet nozzleVOLVO AERO CORP·Filed 2003·Granted Jun 26, 2007·4 cites·12 claims
- 0751US7302794B2Rocket engine member and a method for manufacturing a rocket engine memberVOLVO AERO CORP·Filed 2003·Granted Dec 4, 2007·11 cites·18 claims
- 0850US8689540B2Component configured for being subjected to high thermal load during operationHAEGGANDER JAN·Filed 2007·Granted Apr 8, 2014·4 cites·29 claims
- 0939US6308514B2Rocket engine nozzleVOLVO AERO CORP·Filed 2001·Granted Oct 30, 2001·4 cites·4 claims
- 1038US7017333B2Wall structureVOLVO AERO CORP·Filed 2003·Granted Mar 28, 2006·3 cites·10 claims
- 1137US7481784B2Wall structureVOLVO AERO CORP·Filed 2004·Granted Jan 27, 2009·2 cites·20 claims
- 1234US6574964B1Rocket nozzle contour for flow separation control and side load reductionVOLVO AERO CORP·Filed 1998·Granted Jun 10, 2003·10 cites·2 claims
- 1333US2004103640A1Outlet nozzle and a method for manufacturing an outlet nozzleVOLVO AERO CORP·Filed 2003·Application pending·0 cites
- 1429US6176077B1Rocket engine nozzleVOLVO AERO CORP·Filed 1996·Granted Jan 23, 2001·4 cites·3 claims
- 1526US6318071B2Controlled temperature rocket nozzleVOLVO AERO CORP·Filed 1996·Granted Nov 20, 2001·3 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →