Inventor · disambiguated record
Matthew D. Parekh
Also filed as: PAREKH MATTHEW D
10 granted patents·21 citations·filing 2017–2019
82Inventor score
Files withUNITED TECHNOLOGIES CORP10
Top patents by PatentIndex Score
10 records- 0195US10718521B2Combustor liner panel end rail cooling interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 21, 2020·10 cites·15 claims
- 0293US10473331B2Combustor panel endrail interfaceUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 12, 2019·8 cites·17 claims
- 0372US11098612B2Blade outer air seal including cooling trenchUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 24, 2021·1 cites·15 claims
- 0471US10551066B2Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 4, 2020·1 cites·23 claims
- 0568US10830434B2Combustor liner panel end rail with curved interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 10, 2020·1 cites·4 claims
- 0663US11156359B2Combustor liner panel end rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 26, 2021·0 cites·13 claims
- 0753US11384654B2Mateface for blade outer air seals in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 12, 2022·0 cites·16 claims
- 0852US10677462B2Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 9, 2020·0 cites·15 claims
- 0951US10823411B2Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 3, 2020·0 cites·12 claims
- 1041US10378573B2Anti-rotation retaining pinUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 13, 2019·0 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →