Inventor · disambiguated record
Steven D. Weiner
Also filed as: WEINER STEVEN D
18 granted patents·3 pending applications·303 citations·filing 1991–2015
94Inventor score
Top patents by PatentIndex Score
21 records- 0193US10167079B2Main rotor rotational speed control for rotorcraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Jan 1, 2019·7 cites·13 claims
- 0289USD524230SRigid coaxial rotor helicopter with auxiliary propulsion (large)SIKORSKY AIRCRAFT CORP·Filed 2005·Granted Jul 4, 2006·46 cites·1 claims
- 0387US7954766B2System and method for improved rotary-wing aircraft performance with interior/external loadsSIKORSKY AIRCRAFT CORP·Filed 2006·Granted Jun 7, 2011·37 cites·22 claims
- 0487USD524229SRigid coaxial rotor helicopter with auxiliary propulsion (small)SIKORSKY AIRCRAFT CORP·Filed 2005·Granted Jul 4, 2006·41 cites·1 claims
- 0585US9248909B2Swashplateless coaxial rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2013·Granted Feb 2, 2016·11 cites·23 claims
- 0684US10443675B2Active vibration control of a rotorcraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Oct 15, 2019·2 cites·12 claims
- 0783US5131604AHelicopter antitorque deviceUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jul 21, 1992·78 cites·16 claims
- 0881US8636248B2Retracting tailwheel assembly and finSTILLE BRANDON L·Filed 2012·Granted Jan 28, 2014·9 cites·20 claims
- 0973US10562641B2AFT exhaust system for rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2013·Granted Feb 18, 2020·6 cites·15 claims
- 1065US5108044AShroud-fin integration shelf for a helicopter empennage structureUNITED TECHNOLOGIES CORP·Filed 1991·Granted Apr 28, 1992·37 cites·7 claims
- 1161US10676181B2Gearbox for a dual rotor, rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Jun 9, 2020·0 cites·7 claims
- 1261US10443674B2Noise modes for rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Oct 15, 2019·0 cites·17 claims
- 1357US2017283049A1Differential pre-cone rotary wing arrangement and aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Application pending·0 cites
- 1456US5102067AIntegrated helicopter empennage structureUNITED TECHNOLOGIES CORP·Filed 1991·Granted Apr 7, 1992·29 cites·9 claims
- 1556US2017277201A1Nose attitude control of a rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Application pending·0 cites
- 1655US2017225797A1Aircraft design for air to air refuelingSIKORSKY AIRCRAFT CORP·Filed 2015·Application pending·0 cites
- 1750US10717521B2Hub separation in dual rotor rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Jul 21, 2020·0 cites·7 claims
- 1845US9926076B2Acceleration smoothing holding overall kinetic energy controlSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Mar 27, 2018·0 cites·10 claims
- 1941US9452829B2Yaw control of co-axial rotorSIKORSKY AIRCRAFT CORP·Filed 2013·Granted Sep 27, 2016·0 cites·20 claims
- 2036US10351233B2Vibration control of a swashplateless coaxial rotorSIKORSKY AIRCRAFT CORP·Filed 2013·Granted Jul 16, 2019·0 cites·12 claims
- 2135US10086935B2Guide vanes for a pusher propeller for rotary wing aircraftSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Oct 2, 2018·0 cites·11 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →