Inventor · disambiguated record
Thomas J. Bronson
Also filed as: BRONSON THOMAS · BRONSON THOMAS J
7 granted patents·4 pending applications·81 citations·filing 2007–2021
85Inventor score
Top patents by PatentIndex Score
11 records- 0192US9625156B2Gas turbine engines having fuel injector shrouds with interior ribsHONEYWELL INT INC·Filed 2013·Granted Apr 18, 2017·15 cites·17 claims
- 0287US7665306B2Heat shields for use in combustorsHONEYWELL INT INC·Filed 2007·Granted Feb 23, 2010·26 cites·16 claims
- 0375US8616004B2Quench jet arrangement for annular rich-quench-lean gas turbine combustorsZUPANC FRANK J·Filed 2009·Granted Dec 31, 2013·15 cites·16 claims
- 0472US8171740B2Annular rich-quench-lean gas turbine combustors with plunged holesBRONSON THOMAS J·Filed 2009·Granted May 8, 2012·13 cites·16 claims
- 0561US8584466B2Circumferentially varied quench jet arrangement for gas turbine combustorsBRONSON THOMAS J·Filed 2010·Granted Nov 19, 2013·2 cites·14 claims
- 0660US8141365B2Plunged hole arrangement for annular rich-quench-lean gas turbine combustorsBRONSON THOMAS J·Filed 2009·Granted Mar 27, 2012·7 cites·17 claims
- 0750US9897320B2Effusion cooled dual wall gas turbine combustorsBRONSON THOMAS J·Filed 2009·Granted Feb 20, 2018·3 cites·20 claims
- 0843US2022213797A1Turbomachine with low leakage seal assembly for combustor-turbine interfaceHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 0941US2011185739A1Gas turbine combustors with dual walled linersHONEYWELL INT INC·Filed 2010·Application pending·0 cites
- 1040US2022213796A1Turbomachine with low leakage seal assembly for combustor-turbine interfaceHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 1140US2010212324A1Dual walled combustors with impingement cooled ignitersHONEYWELL INT INC·Filed 2009·Application pending·0 cites
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