Inventor · disambiguated record
Edward E. Coleman
Also filed as: COLEMAN EDWARD E · COLEMAN EDWARD ERNEST
12 granted patents·1 pending application·200 citations·filing 1995–2017
91Inventor score
Top patents by PatentIndex Score
13 records- 0187US6325333B1Aircraft pitch-axis stability and command augmentation systemBOEING CO·Filed 2000·Granted Dec 4, 2001·44 cites·9 claims
- 0280US5722620AAircraft pitch-axis stability and command augmentationBOEING CO·Filed 1995·Granted Mar 3, 1998·50 cites·23 claims
- 0373US7474944B2Control system and method with multiple linked inputsBOEING CO·Filed 2005·Granted Jan 6, 2009·11 cites·35 claims
- 0468US8774987B2Vertical gust suppression system for transport aircraftWALTON VINCENT M·Filed 2007·Granted Jul 8, 2014·16 cites·26 claims
- 0566US8342445B2Horizontal tail load alleviation systemBOEING CO·Filed 2008·Granted Jan 1, 2013·7 cites·14 claims
- 0659US5826833ASystem for providing an air/ground signal to aircraft flight control systemsBOEING CO·Filed 1995·Granted Oct 27, 1998·35 cites·20 claims
- 0758US8024079B2Wing-body load alleviation for aircraftBOEING CO·Filed 2008·Granted Sep 20, 2011·7 cites·20 claims
- 0856US10793260B1Methods and systems for controlling aircraft flight performanceBOEING CO·Filed 2017·Granted Oct 6, 2020·1 cites·23 claims
- 0952US9731813B2Methods and apparatus to control aircraft horizontal stabilizersBOEING CO·Filed 2014·Granted Aug 15, 2017·1 cites·13 claims
- 1045US5692708AMethod and apparatus for automatically trimming an airplane stabilizerBOEING CO·Filed 1995·Granted Dec 2, 1997·17 cites·21 claims
- 1144US8752789B2Horizontal tail load alleviation systemBOEING CO·Filed 2012·Granted Jun 17, 2014·0 cites·17 claims
- 1244US6158695AMethod of speed protection and flare compensation for use with aircraft pitch control systemBOEING CO·Filed 1999·Granted Dec 12, 2000·11 cites·27 claims
- 1334US2004078121A1Control system and method with multiple linked inputsFiled 2002·Application pending·0 cites
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