Inventor · disambiguated record
Bradley Reed Tucker
Also filed as: TUCKER BRADLEY · TUCKER BRADLEY R · TUCKER BRADLEY REED
16 granted patents·3 pending applications·145 citations·filing 2007–2020
93Inventor score
Top patents by PatentIndex Score
19 records- 0195US8047771B2Turbine nozzles and methods of manufacturing the sameHONEYWELL INT INC·Filed 2008·Granted Nov 1, 2011·24 cites·20 claims
- 0295US7931407B2Systems for supplying oil from an oil source to a bearing assemblyHONEYWELL INT INC·Filed 2007·Granted Apr 26, 2011·22 cites·20 claims
- 0388US9139480B2Protective coatings and coated components comprising the protective coatingsRAYBOULD DEREK·Filed 2011·Granted Sep 22, 2015·8 cites·19 claims
- 0485US8388307B2Turbine nozzle assembly including radially-compliant spring member for gas turbine engineSMOKE JASON·Filed 2009·Granted Mar 5, 2013·26 cites·17 claims
- 0579US9970307B2Turbine nozzles with slip joints impregnated by oxidation-resistant sealing material and methods for the production thereofHONEYWELL INT INC·Filed 2014·Granted May 15, 2018·8 cites·20 claims
- 0678US9719362B2Turbine nozzles and methods of manufacturing the sameHONEYWELL INT INC·Filed 2013·Granted Aug 1, 2017·6 cites·17 claims
- 0777US9657642B2Turbine sections of gas turbine engines with dual use of cooling airHONEYWELL INT INC·Filed 2014·Granted May 23, 2017·7 cites·9 claims
- 0877US9611748B2Stationary airfoils configured to form improved slip joints in bi-cast turbine engine components and the turbine engine components including the sameHONEYWELL INT INC·Filed 2013·Granted Apr 4, 2017·6 cites·17 claims
- 0976US8534076B2Combustor-turbine seal interface for gas turbine engineWOODCOCK GREGORY O·Filed 2009·Granted Sep 17, 2013·16 cites·19 claims
- 1071US9896938B2Gas turbine engines with internally stretched tie shaftsHONEYWELL INT INC·Filed 2015·Granted Feb 20, 2018·2 cites·16 claims
- 1171US9885245B2Turbine nozzles and cooling systems for cooling slip joints thereinHONEYWELL INT INC·Filed 2014·Granted Feb 6, 2018·4 cites·18 claims
- 1270US8616832B2Turbine assemblies with impingement coolingSMOKE JASON·Filed 2009·Granted Dec 31, 2013·10 cites·20 claims
- 1368US9506365B2Gas turbine engine components having sealed stress relief slots and methods for the fabrication thereofHONEYWELL INT INC·Filed 2014·Granted Nov 29, 2016·3 cites·19 claims
- 1459US9844826B2Methods for manufacturing a turbine nozzle with single crystal alloy nozzle segmentsHONEYWELL INT INC·Filed 2014·Granted Dec 19, 2017·1 cites·13 claims
- 1555US2019022781A1Methods for manufacturing a turbine nozzle with single crystal alloy nozzle segmentsHONEYWELL INT INC·Filed 2017·Application pending·0 cites
- 1653US9068469B2Gas turbine engines with abradable turbine seal assembliesTUCKER BRADLEY REED·Filed 2011·Granted Jun 30, 2015·2 cites·18 claims
- 1749US11499478B2Asymmetric inlet particle separator for gas turbine engineHONEYWELL INT INC·Filed 2020·Granted Nov 15, 2022·0 cites·20 claims
- 1849US2009087307A1Reduced pressure load finger seal assemblyHONEYWELL INT INC·Filed 2007·Application pending·0 cites
- 1938US2016305004A1Coated substrates and methods of producing the sameHONEYWELL INT INC·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →