Inventor · disambiguated record
Leonard J. Hebert
Also filed as: HEBERT LEONARD J
11 granted patents·1 pending application·263 citations·filing 1997–2018
90Inventor score
Files withBOEING CO12
Top patents by PatentIndex Score
12 records- 0189US6050527AFlow control device to eliminate cavity resonanceBOEING CO·Filed 1997·Granted Apr 18, 2000·113 cites·22 claims
- 0286US6658839B2Convergent/divergent segmented exhaust nozzleBOEING CO·Filed 2002·Granted Dec 9, 2003·47 cites·14 claims
- 0377US10793282B2Liner assembly, engine housing, and methods of assembling the sameBOEING CO·Filed 2018·Granted Oct 6, 2020·3 cites·16 claims
- 0475US9896217B2Enhanced performance jet engine mounting strutsBOEING CO·Filed 2016·Granted Feb 20, 2018·3 cites·18 claims
- 0575US6826901B2Convergent/divergent segmented exhaust nozzleBOEING CO·Filed 2003·Granted Dec 7, 2004·28 cites·22 claims
- 0667US7883049B2Jet nozzle having noise attenuating shield and method thereforBOEING CO·Filed 2007·Granted Feb 8, 2011·9 cites·20 claims
- 0762US5906097AEngine flow control deviceBOEING CO·Filed 1997·Granted May 25, 1999·37 cites·17 claims
- 0861US9546618B2Methods and apparatus for passive thrust vectoring and plume deflectionBOEING CO·Filed 2013·Granted Jan 17, 2017·2 cites·27 claims
- 0950US10118709B2Enhanced performance jet engine mounting strutsBOEING CO·Filed 2018·Granted Nov 6, 2018·0 cites·20 claims
- 1045US9964070B2Gas turbine engine nozzle including housing having scalloped root regionsBOEING CO·Filed 2013·Granted May 8, 2018·0 cites·20 claims
- 1139US5887822ASegmented engine flow control deviceBOEING CO·Filed 1997·Granted Mar 30, 1999·21 cites·12 claims
- 1235US2018029719A1Drag reducing liner assembly and methods of assembling the sameBOEING CO·Filed 2016·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →