Inventor · disambiguated record
Venkatarama K. Seetharaman
Also filed as: SEETHARAMAN VENKATARAMA K
19 granted patents·5 pending applications·53 citations·filing 2006–2022
92Inventor score
Files withUNITED TECHNOLOGIES CORP18RAYTHEON TECH CORP2SEETHARAMAN VENKATARAMA K2LITTON DAVID A1WATSON THOMAS J1
Top patents by PatentIndex Score
24 records- 0198US10369625B2Arcuate directionally solidified components and manufacture methodsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·16 cites·22 claims
- 0292US9939393B2Detection of crystallographic properties in aerospace componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 10, 2018·7 cites·21 claims
- 0388US10752554B1Intermetallic matrix compositeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 25, 2020·1 cites·20 claims
- 0487US11306595B2Wrought root blade manufacture methodsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 19, 2022·2 cites·20 claims
- 0585US7704332B2Moderate density, low density, and extremely low density single crystal alloys for high AN2 applicationsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Apr 27, 2010·4 cites·10 claims
- 0681US7476450B2Coating suitable for use as a bondcoat in a thermal barrier coating systemUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jan 13, 2009·11 cites·25 claims
- 0779US11181491B2Detection of crystallographic properties in aerospace componentsRAYTHEON TECH CORP·Filed 2018·Granted Nov 23, 2021·1 cites·15 claims
- 0878US8920937B2Zirconium modified protective coatingLITTON DAVID A·Filed 2007·Granted Dec 30, 2014·4 cites·14 claims
- 0977US10793939B2Nickel based superalloy with high volume fraction of precipitate phaseUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 6, 2020·0 cites·5 claims
- 1077US9586868B2Method for joining dissimilar engine componentsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 7, 2017·2 cites·24 claims
- 1175US10273816B2Wear pad to prevent cracking of fan bladeUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 30, 2019·5 cites·12 claims
- 1271US11773724B2Wrought root blade manufacture methodsRAYTHEON TECH CORP·Filed 2022·Granted Oct 3, 2023·0 cites·20 claims
- 1368US8366838B2Moderate density, low density, and extremely low density single crystal alloys for high AN2 applicationsUNITED TECHNOLOGIES CORP·Filed 2009·Granted Feb 5, 2013·0 cites·14 claims
- 1466US10301711B2Nickel based superalloy with high volume fraction of precipitate phaseUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 28, 2019·0 cites·14 claims
- 1562US10150159B2Casting apparatus and method for forming multi-textured, single crystal microstructureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 11, 2018·0 cites·14 claims
- 1661US10265763B2Arcuate directionally solidified components and manufacture methodsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 23, 2019·0 cites·22 claims
- 1760US11459899B2Turbine component with a thin interior partitionUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 4, 2022·0 cites·12 claims
- 1856US10661380B2Method for joining dissimilar engine componentsUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 26, 2020·0 cites·22 claims
- 1946US2011256421A1Metallic coating for single crystal alloysUNITED TECHNOLOGIES CORP·Filed 2010·Application pending·0 cites
- 2045US2012328472A1Forging of glassy aluminum-based alloysWATSON THOMAS J·Filed 2011·Application pending·0 cites
- 2144US2018051360A1Formable Superalloy Single Crystal CompositionUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 2241US10352183B2High temperature seal and methodUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 16, 2019·0 cites·15 claims
- 2341US2013052479A1Laser shock peening of airfoilsSEETHARAMAN VENKATARAMA K·Filed 2011·Application pending·0 cites
- 2440US2013183157A1Method of surface treatment for dovetail in gas turbine engine fan bladeSEETHARAMAN VENKATARAMA K·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →