Inventor · disambiguated record
Christopher J. Hanlon
Also filed as: HANLON CHRISTOPHER J
24 granted patents·5 pending applications·73 citations·filing 2012–2024
94Inventor score
Top patents by PatentIndex Score
29 records- 0195US12180846B2Electric heating for turbomachinery clearance control powered by hybrid energy storage systemRAYTHEON TECH CORP·Filed 2022·Granted Dec 31, 2024·2 cites·19 claims
- 0295US11168616B2Hybrid electric fan with improved low pressure compressorUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 9, 2021·6 cites·13 claims
- 0393US12031485B1Water storage precooling and water cycle chillerRAYTHEON TECH CORP·Filed 2023·Granted Jul 9, 2024·4 cites·20 claims
- 0493US10760444B2Electric heating for turbomachinery clearance control powered by hybrid energy storage systemUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 1, 2020·6 cites·8 claims
- 0592US11415044B2Multi-engine architecture with linkages to multiple spoolsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 16, 2022·6 cites·16 claims
- 0692US11015523B2Turbofan with bleed supercharged auxiliary engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 25, 2021·9 cites·19 claims
- 0790US9650954B2Gas turbine engine with distributed fansUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 16, 2017·7 cites·19 claims
- 0886US10161316B2Engine bypass valveUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 25, 2018·5 cites·19 claims
- 0985US11680531B2Adaptive bleed schedule in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jun 20, 2023·1 cites·20 claims
- 1084US12134984B1Fluidic compressor inlet guide vanesRTX CORP·Filed 2023·Granted Nov 5, 2024·1 cites·17 claims
- 1182US11125168B2Dirt mitigation in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 21, 2021·3 cites·20 claims
- 1280US11840958B2Turbofan with offset gas generator and auxiliary power coreRTX CORP·Filed 2021·Granted Dec 12, 2023·1 cites·17 claims
- 1379US9951721B2Three-stream gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 24, 2018·6 cites·17 claims
- 1479US2025043730A1Gas turbine engine with electrically driven compressorRTX CORP·Filed 2024·Application pending·0 cites
- 1577US11111809B2Electric heating for turbomachinery clearance controlUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 7, 2021·2 cites·15 claims
- 1677US8862362B2Scheduling of variable area fan nozzle to optimize engine performanceTEICHOLZ MATTHEW D·Filed 2012·Granted Oct 14, 2014·11 cites·14 claims
- 1774US10119477B2Gas turbine engine with a multi-spool driven fanUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 6, 2018·2 cites·17 claims
- 1870US11261800B2Adaptive bleed schedule in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 1, 2022·1 cites·20 claims
- 1966US12196137B2Gas turbine engine with electrically driven compressorRTX CORP·Filed 2021·Granted Jan 14, 2025·0 cites·11 claims
- 2066US11421545B2Electric heating for turbomachinery clearance control powered by hybrid energy storage systemRAYTHEON TECH CORP·Filed 2020·Granted Aug 23, 2022·0 cites·17 claims
- 2162US11952947B2Hybrid electric fan with stall free low pressure compressorRAYTHEON TECH CORP·Filed 2021·Granted Apr 9, 2024·0 cites·16 claims
- 2256US10837359B2Gas turbine engine with distributed fansRAYTHEON TECH CORP·Filed 2017·Granted Nov 17, 2020·0 cites·20 claims
- 2355US12312996B2Aircraft powerplant with steam system and bypassRAYTHEON TECH CORP·Filed 2023·Granted May 27, 2025·0 cites·20 claims
- 2455US2019048796A1Turbine clearance control system and method for improved variable cycle gas turbine engine fuel burnUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2551US2025382922A1Bleeding core air from a turbine engine core flowpathRTX CORP·Filed 2024·Application pending·0 cites
- 2651US2025146441A1Turbine cooling air pressure boost systemRTX CORP·Filed 2023·Application pending·0 cites
- 2749US11781479B2Turbofan gas turbine engine with combusted compressor bleed flowRTX CORP·Filed 2021·Granted Oct 10, 2023·0 cites·11 claims
- 2847US2017328231A1Turbine clearance control system and method for improved variable cycle gas turbine engine fuel burnUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2937US11236639B2Gas turbine engine and an airflow control systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 1, 2022·0 cites·20 claims
Join the waitlist — get patent alerts
Get an alert when Christopher J. Hanlon files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →