Inventor · disambiguated record
Boris Grohmann
Also filed as: GROHMANN BORIS
18 granted patents·3 pending applications·91 citations·filing 2003–2021
92Inventor score
Files withAIRBUS HELICOPTERS5Airbus Helicopters Deutschland GmbH5AIRBUS GMBH3GROHMANN BORIS3CHADUC BRUNO1
Top patents by PatentIndex Score
21 records- 0192US7766281B2System for reducing aerodynamic noise at a supplementary wing of an aircraftAIRBUS GMBH·Filed 2005·Granted Aug 3, 2010·32 cites·21 claims
- 0284US10940957B2Haptic alert mechanism for alerting an aircraft pilot, and an aircraftAIRBUS HELICOPTERS·Filed 2020·Granted Mar 9, 2021·3 cites·16 claims
- 0383US10556668B2Artificial force feel generating device for a vehicle control system of a vehicle and, in particular, of an aircraftAirbus Helicopters Deutschland GmbH·Filed 2016·Granted Feb 11, 2020·7 cites·21 claims
- 0482US8006941B2System for reducing aerodynamic noise at a supplementary wing of an aircraftAIRBUS GMBH·Filed 2010·Granted Aug 30, 2011·9 cites·15 claims
- 0578US10931163B2Electromechanical actuator with stator teeth dimensioned to operate a saturation bend for electrical flight controls of an aircraftAIRBUS HELICOPTERS·Filed 2016·Granted Feb 23, 2021·2 cites·19 claims
- 0673US8888036B2Primary flight controlsCHADUC BRUNO·Filed 2012·Granted Nov 18, 2014·8 cites·20 claims
- 0770US8162607B2Rotor blade for a rotary wing aircraftGROHMANN BORIS·Filed 2006·Granted Apr 24, 2012·13 cites·31 claims
- 0869US10577083B2Method of controlling an artificial force feel generating device for generation of an artificial feeling of force on an inceptor of a vehicle control systemAirbus Helicopters Deutschland GmbH·Filed 2018·Granted Mar 3, 2020·1 cites·15 claims
- 0966US11811291B2Electromechanical actuator with stator teeth dimensioned to operate a saturation bend for electrical flight controls of an aircraftAIRBUS HELICOPTERS·Filed 2020·Granted Nov 7, 2023·0 cites·20 claims
- 1058US8628046B2Control systemGROHMANN BORIS·Filed 2011·Granted Jan 14, 2014·3 cites·18 claims
- 1157US7880366B2Three-dimensional stack-type piezo element and piezoelectric actuator having such a stack-type piezo elementEADS DEUTSCHLAND GMBH·Filed 2006·Granted Feb 1, 2011·2 cites·18 claims
- 1254US8002162B2Friction-welding deviceMTU AERO ENGINES GMBH·Filed 2003·Granted Aug 23, 2011·5 cites·12 claims
- 1352US9643717B2System and a method for controlling pitching stabilizer means of an aircraftAIRBUS HELICOPTERS·Filed 2014·Granted May 9, 2017·2 cites·16 claims
- 1450US8191835B2Wing of an aircraftGROHMANN BORIS·Filed 2007·Granted Jun 5, 2012·4 cites·16 claims
- 1548US2021354809A1Control and monitoring device for a vehicleAirbus Helicopters Deutschland GmbH·Filed 2021·Application pending·0 cites
- 1641US9631711B2Actuator arrangement and control surface arrangement, especially for an aircraftSTORM STEFAN·Filed 2013·Granted Apr 25, 2017·0 cites·20 claims
- 1740US11305787B2Vehicle control system for autonomous, remotely-controlled, or manual operation of a vehicleAirbus Helicopters Deutschland GmbH·Filed 2020·Granted Apr 19, 2022·0 cites·14 claims
- 1839US9802699B2Adaptively-twistable blade, and an aircraft including such a bladeAIRBUS HELICOPTERS·Filed 2014·Granted Oct 31, 2017·0 cites·22 claims
- 1938US9484843B2Electric circuit with power amplifier for piezoelectric actuatorsAirbus Helicopters Deutschland GmbH·Filed 2013·Granted Nov 1, 2016·0 cites·6 claims
- 2036US2010181415A1Rotor blade for a rotary wing aircraftEUROCOPTER DEUTSCHLAND·Filed 2008·Application pending·0 cites
- 2135US2009001223A1Flexible Control Surface for an AircraftAIRBUS GMBH·Filed 2006·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →