Inventor · disambiguated record
Bradley C. Schafer
Also filed as: SCHAFER BRADLEY · SCHAFER BRADLEY C
9 granted patents·7 pending applications·92 citations·filing 1989–2024
83Inventor score
Files withRAYTHEON TECH CORP5RTX CORP5UNITED TECHNOLOGIES CORP3SCHAFER BRADLEY C2GREEN CLOUD PROCESS LLC1
Top patents by PatentIndex Score
16 records- 0181US4991389ABleed modulation for transient engine operationUNITED TECHNOLOGIES CORP·Filed 1989·Granted Feb 12, 1991·50 cites·5 claims
- 0274US12326096B2Core turning systemRTX CORP·Filed 2024·Granted Jun 10, 2025·0 cites·16 claims
- 0372US12018578B1Core turning systemRTX CORP·Filed 2023·Granted Jun 25, 2024·0 cites·17 claims
- 0468US12448924B2Aircraft hybrid duplex-triplex control architectureRTX CORP·Filed 2023·Granted Oct 21, 2025·0 cites·19 claims
- 0558US5752379ANon-recoverable surge and blowout detection in gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 1995·Granted May 19, 1998·36 cites·6 claims
- 0658US2016162817A1Vehicle Reconditioning Workflow SystemGREEN CLOUD PROCESS LLC·Filed 2014·Application pending·0 cites
- 0757US12060839B1Optimized bowed rotor control methodRTX CORP·Filed 2023·Granted Aug 13, 2024·0 cites·18 claims
- 0852US11959386B2Monitoring fluid consumption of gas turbine engine during an engine cycleRAYTHEON TECH CORP·Filed 2022·Granted Apr 16, 2024·0 cites·19 claims
- 0951US11700567B2Waveguide system with redundancyRAYTHEON TECH CORP·Filed 2020·Granted Jul 11, 2023·0 cites·20 claims
- 1051US8235325B2Fan variable area nozzle positional measurement systemSCHAFER BRADLEY C·Filed 2006·Granted Aug 7, 2012·6 cites·16 claims
- 1150US2024175409A1Integrated thrust reverser and brake control for an aircraftRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1247US2025137386A1Gas turbine engine drone inspection systemRTX CORP·Filed 2023·Application pending·0 cites
- 1343US2023166857A1Final takeoff speed determination for an aircraftRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1440US2019120140A1Gas turbine engine with vacuum generator for reducing bearing compartment pressureUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 1539US2023129383A1System and method for gas turbine engine rotor bow mitigationRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 1630US2010095650A1Translating core cowl for a gas turbine engineSCHAFER BRADLEY C·Filed 2006·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →