Inventor · disambiguated record
Mark Heintjes
Also filed as: HEINTJES MARK
11 granted patents·1 pending application·39 citations·filing 2006–2015
86Inventor score
Top patents by PatentIndex Score
12 records- 0178US8868261B2Monitoring device for an actuation system of an aircraft, actuation system and method for reconfiguring the actuation systemAIRBUS OPERATIONS GMBH·Filed 2013·Granted Oct 21, 2014·8 cites·21 claims
- 0267US8746614B2System for actuating at least one positioning flap of an aircraft and a method for monitoring the systemHEINTJES MARK·Filed 2008·Granted Jun 10, 2014·10 cites·17 claims
- 0361US9334044B2Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive systemAIRBUS OPERATIONS GMBH·Filed 2015·Granted May 10, 2016·1 cites·9 claims
- 0458US9108740B2Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive systemAIRBUS OPERATIONS GMBH·Filed 2013·Granted Aug 18, 2015·2 cites·6 claims
- 0558US7963484B2Lift-augmenting flap, in particular for a leading edge flap, for an aerodynamically effective wingAIRBUS GMBH·Filed 2006·Granted Jun 21, 2011·7 cites·30 claims
- 0657US8224502B2Method and device for fault detection in the load path of a spindle actuatorBRUECKNER INA·Filed 2008·Granted Jul 17, 2012·8 cites·20 claims
- 0751US9261150B2Drive system for a high lift system of an aircraft and method for detecting a misalignment between a transmission shaft and an opening in a drive system for a high lift system of an aircraftAIRBUS OPERATIONS GMBH·Filed 2014·Granted Feb 16, 2016·1 cites·20 claims
- 0850US9688418B2Method for determining a state of a component in a high lift system of an aircraft, high lift system of an aircraft, and aircraft having such a high lift systemAIRBUS OPERATIONS GMBH·Filed 2015·Granted Jun 27, 2017·1 cites·15 claims
- 0950US8356477B2Dual linear actuatorAIRBUS OPERATIONS GMBH·Filed 2008·Granted Jan 22, 2013·1 cites·7 claims
- 1036US9242719B2Wing of an aircraft or spacecraft, comprising a mobile flow bodyHEINTJES MARK·Filed 2010·Granted Jan 26, 2016·0 cites·20 claims
- 1134US9701419B2Method for determining a state of a component in a high lift system of an aircraftAIRBUS OPERATIONS GMBH·Filed 2015·Granted Jul 11, 2017·0 cites·16 claims
- 1228US2016114881A1Method for determining a state of a component in a high lift system of an aircraft, high lift system of an aircraft and aircraft having such a high lift systemAIRBUS OPERATIONS GMBH·Filed 2015·Application pending·0 cites
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