Inventor · disambiguated record
Andrew E. Breault
Also filed as: BREAULT ANDREW E
12 granted patents·10 pending applications·0 citations·filing 2022–2025
79Inventor score
Top patents by PatentIndex Score
22 records- 0177US2025290422A1Gas turbine engine with bypass tobi cooling/purge flow and methodRTX CORP·Filed 2025·Application pending·0 cites
- 0275US12510030B2Aft mounted pusher fan for gas turbine engineRTX CORP·Filed 2024·Granted Dec 30, 2025·0 cites·14 claims
- 0372US12421863B2Turbine engine tip clearance control system with thrust bearingRAYTHEON TECH CORP·Filed 2023·Granted Sep 23, 2025·0 cites·15 claims
- 0471US12352185B1Open rotor variable pitch blade with retracting inboard trailing edgeRTX CORP·Filed 2024·Granted Jul 8, 2025·0 cites·20 claims
- 0569US12320270B2Gas turbine engine with bypass TOBI cooling/purge flow and methodRAYTHEON TECH CORP·Filed 2023·Granted Jun 3, 2025·0 cites·20 claims
- 0668US12018620B1AFT mounted pusher fan for gas turbine engineRTX CORP·Filed 2022·Granted Jun 25, 2024·0 cites·20 claims
- 0767US12448901B1Thermal management system for gas turbine engine with open propulsorRTX CORP·Filed 2024·Granted Oct 21, 2025·0 cites·20 claims
- 0865US12460577B2AFT gear based engine with heat recovery systemRTX CORP·Filed 2024·Granted Nov 4, 2025·0 cites·16 claims
- 0963US2025369825A1Actuatable inspection probe for non-destructive inspectionRTX CORP·Filed 2024·Application pending·0 cites
- 1062US11920487B1Gas turbine engine including flow path flex seal with cooling air bifurcationRAYTHEON TECH CORP·Filed 2022·Granted Mar 5, 2024·0 cites·19 claims
- 1158US12397924B2Open rotor aircraft propulsion system with bypass flowpathRTX CORP·Filed 2024·Granted Aug 26, 2025·0 cites·19 claims
- 1255US12404812B1Open rotor aircraft propulsion system with bypass flowpathRTX CORP·Filed 2024·Granted Sep 2, 2025·0 cites·17 claims
- 1353US12378893B2Buffer air assembly for an aircraft engineRAYTHEON TECH CORP·Filed 2023·Granted Aug 5, 2025·0 cites·16 claims
- 1451US12460819B2Continuous flow fuel systemRTX CORP·Filed 2024·Granted Nov 4, 2025·0 cites·13 claims
- 1550US2024353105A1Gas turbine engine configured for decreased diffuser windage and method of assembling the sameRTX CORP·Filed 2024·Application pending·0 cites
- 1649US2025154906A1Turbine engine accessory system with multiple gearboxesRTX CORP·Filed 2023·Application pending·0 cites
- 1749US2025297579A1Open pusher rotor with remote exhaustRTX CORP·Filed 2024·Application pending·0 cites
- 1848US2025027445A1Buffer air assembly for an aircraft engineRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1948US2025197013A1Open rotor aircraft propulsion system with anti-icing systemRTX CORP·Filed 2023·Application pending·0 cites
- 2048US2024410587A1Gas turbine engine with improved high pressure compressor leakage path guide structureRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 2148US2025243783A1Intermediate case for aircraft propulsion system housingRTX CORP·Filed 2024·Application pending·0 cites
- 2247US2024426245A1Water actuated tip clearance control system for turbine engineRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →