Inventor · disambiguated record
Clifton J. Crawley, Jr.
Also filed as: CRAWLEY CLIFTON J · CRAWLEY JR CLIFTON J
17 granted patents·3 pending applications·189 citations·filing 1989–2018
94Inventor score
Top patents by PatentIndex Score
20 records- 0197US10060280B2Turbine cavity sealing assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 28, 2018·17 cites·12 claims
- 0294US9097138B2Gas turbine engine buffer systemUNITED TECHNOLOGIES CORP·Filed 2013·Granted Aug 4, 2015·14 cites·15 claims
- 0393US10107126B2Non-contact seal assembly for rotational equipmentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 23, 2018·8 cites·20 claims
- 0492US8794009B2Gas turbine engine buffer systemGLAHN JORN A·Filed 2012·Granted Aug 5, 2014·11 cites·18 claims
- 0591US8769962B2Multi-circuit buffer system for a gas turbine engineGLAHN JORN A·Filed 2012·Granted Jul 8, 2014·13 cites·22 claims
- 0688US9027353B2Gas turbine engine buffer systemUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 12, 2015·7 cites·32 claims
- 0785US10094241B2Non-contact seal assembly for rotational equipmentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·5 cites·18 claims
- 0880US10087782B2Engine mid-turbine frame transfer tube for low pressure turbine case coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 2, 2018·7 cites·16 claims
- 0973US10047677B2Gas turbine engine buffer systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 14, 2018·1 cites·11 claims
- 1064US5090193AActive clearance control with cruise modeUNITED TECHNOLOGIES CORP·Filed 1989·Granted Feb 25, 1992·32 cites·2 claims
- 1161US10669888B2Non-contact seal assembly for rotational equipmentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 2, 2020·0 cites·16 claims
- 1260US10975715B2Non-contact seal assembly for rotational equipmentRAYTHEON TECH CORP·Filed 2018·Granted Apr 13, 2021·0 cites·20 claims
- 1360US10794275B2Multi-circuit buffer system for a gas turbine engineRAYTHEON TECH CORP·Filed 2017·Granted Oct 6, 2020·0 cites·17 claims
- 1458US5081830AMethod of restoring exhaust gas temperature margin in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1990·Granted Jan 21, 1992·35 cites·15 claims
- 1555US9816436B2Multi-circuit buffer system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 14, 2017·0 cites·1 claims
- 1651US5005352AClearance control method for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1989·Granted Apr 9, 1991·23 cites·5 claims
- 1749US2016201563A1Fuel management system for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1845US5076050AThermal clearance control method for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1989·Granted Dec 31, 1991·16 cites·2 claims
- 1942US2013195627A1Thrust balance system for gas turbine engineGLAHN JORN A·Filed 2012·Application pending·0 cites
- 2041US2017051751A1Seal assembly for rotational equipmentUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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