Inventor · disambiguated record
Robert C. Moffitt
Also filed as: MOFFITT JR ROBERT · MOFFITT ROBERT · MOFFITT ROBERT C
18 granted patents·2 pending applications·698 citations·filing 1980–2021
96Inventor score
Files withSIKORSKY AIRCRAFT CORP12UNITED TECHNOLOGIES CORP5EGOLF THOMAS A1MOFFITT LLC1The Water Factory1
Top patents by PatentIndex Score
20 records- 0196US5150857AShroud geometry for unmanned aerial vehiclesUNITED TECHNOLOGIES CORP·Filed 1991·Granted Sep 29, 1992·142 cites·7 claims
- 0292USD349647SContainer capThe Water Factory·Filed 1988·Granted Aug 16, 1994·43 cites·1 claims
- 0391US7252479B2Rotor blade for a high speed rotary-wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2005·Granted Aug 7, 2007·31 cites·40 claims
- 0487US10822076B2Dual rotor, rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Nov 3, 2020·10 cites·12 claims
- 0586US4324530AHelicopter blade with a tip having a selected combination of sweep, taper and anhedral to improve hover efficiencyUNITED TECHNOLOGIES CORP·Filed 1980·Granted Apr 13, 1982·69 cites·9 claims
- 0682US7513750B2Rotor blade tip planformSIKORSKY AIRCRAFT CORP·Filed 2006·Granted Apr 7, 2009·21 cites·12 claims
- 0782US4334828AHelicopter blade with a tip having a selected combination of sweep, taper and anhedral to improve hover efficiencyUNITED TECHNOLOGIES CORP·Filed 1980·Granted Jun 15, 1982·51 cites·9 claims
- 0878US6769872B2Active control of multi-element rotor blade airfoilsSIKORSKY AIRCRAFT CORP·Filed 2002·Granted Aug 3, 2004·34 cites·28 claims
- 0978US5620303ARotor system having alternating length rotor blades for reducing blade-vortex interaction (BVI) noiseSIKORSKY AIRCRAFT CORP·Filed 1995·Granted Apr 15, 1997·58 cites·4 claims
- 1078US5253979AVariable diameter rotor having an offset twistUNITED TECHNOLOGIES CORP·Filed 1992·Granted Oct 19, 1993·64 cites·9 claims
- 1173US5735670ARotor system having alternating length rotor blades and positioning means therefor for reducing blade-vortex interaction (BVI) noiseSIKORSKY AIRCRAFT CORP·Filed 1995·Granted Apr 7, 1998·48 cites·23 claims
- 1266US6932569B2Active control of multi-element rotor blade airfoilsSIKORSKY AIRCRAFT CORP·Filed 2002·Granted Aug 23, 2005·19 cites·25 claims
- 1365US6840741B1Leading edge slat airfoil for multi-element rotor blade airfoilsSIKORSKY AIRCRAFT CORP·Filed 2003·Granted Jan 11, 2005·19 cites·4 claims
- 1465US5108044AShroud-fin integration shelf for a helicopter empennage structureUNITED TECHNOLOGIES CORP·Filed 1991·Granted Apr 28, 1992·37 cites·7 claims
- 1564US6666648B2Directional elastomeric couplerSIKORSKY AIRCRAFT CORP·Filed 2002·Granted Dec 23, 2003·17 cites·34 claims
- 1663US7547193B2Rotor blade assembly with high pitching moment airfoil section for a rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2005·Granted Jun 16, 2009·8 cites·37 claims
- 1756US12228188B2Methods and apparatus for a 3D-printed springMOFFITT LLC·Filed 2021·Granted Feb 18, 2025·0 cites·19 claims
- 1856US2017274990A1Rotor hover figure of merit for rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Application pending·0 cites
- 1948US5620304ARotor system having alternating length rotor blades and positioning means therefor for reducing blade-vortex interaction (BVI) noiseSIKORSKY AIRCRAFT CORP·Filed 1995·Granted Apr 15, 1997·27 cites·6 claims
- 2033US2005281676A1Multi-hedral rotary wingEGOLF THOMAS A·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →