Inventor · disambiguated record
Stony Kujala
Also filed as: KUJALA STONY · KUJALA STONY W
8 granted patents·2 pending applications·115 citations·filing 2003–2013
88Inventor score
Top patents by PatentIndex Score
10 records- 0185US8388307B2Turbine nozzle assembly including radially-compliant spring member for gas turbine engineSMOKE JASON·Filed 2009·Granted Mar 5, 2013·26 cites·17 claims
- 0276US8534076B2Combustor-turbine seal interface for gas turbine engineWOODCOCK GREGORY O·Filed 2009·Granted Sep 17, 2013·16 cites·19 claims
- 0366US6912782B2Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Jul 5, 2005·11 cites·23 claims
- 0465US7007480B2Multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Mar 7, 2006·26 cites·26 claims
- 0556US8127552B2Transition scrolls for use in turbine engine assembliesSCHUMACHER JURGEN C·Filed 2008·Granted Mar 6, 2012·7 cites·18 claims
- 0656US7093448B2Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Aug 22, 2006·18 cites·14 claims
- 0745US2014190171A1Combustors with hybrid walled linersHONEYWELL INT INC·Filed 2013·Application pending·0 cites
- 0839US7007475B2Conical helical of spiral combustor scroll device in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Mar 7, 2006·7 cites·28 claims
- 0939US6962480B2Thermally stabilized turbine scroll retention ring for uniform loading applicationHONEYWELL INT INC·Filed 2003·Granted Nov 8, 2005·4 cites·19 claims
- 1033US2005241316A1Uniform effusion cooling method for a can combustion chamberHONEYWELL INT INC·Filed 2004·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Stony Kujala files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →