Inventor · disambiguated record
Preston A. Henne
Also filed as: HENNE PRESTON A
18 granted patents·2 pending applications·201 citations·filing 1987–2017
94Inventor score
Files withGULFSTREAM AEROSPACE CORP9HENNE PRESTON A5CONNERS TIMOTHY R3MC DONNELL DOUGLAS CORP2ROLLS ROYCE DEUTSCHLAND1
Top patents by PatentIndex Score
20 records- 0187US8286434B2Isentropic compression inlet for supersonic aircraftHENNE PRESTON A·Filed 2011·Granted Oct 16, 2012·7 cites·12 claims
- 0286US6698684B1Supersonic aircraft with spike for controlling and reducing sonic boomGULFSTREAM AEROSPACE CORP·Filed 2002·Granted Mar 2, 2004·57 cites·39 claims
- 0382US8333076B2Isentropic compression inlet for supersonic aircraftCONNERS TIMOTHY R·Filed 2006·Granted Dec 18, 2012·8 cites·6 claims
- 0478US9482155B2Isentropic compression inlet for supersonic aircraftGULFSTREAM AEROSPACE CORP·Filed 2012·Granted Nov 1, 2016·3 cites·7 claims
- 0578US8327645B2Isentropic compression inlet for supersonic aircraftHENNE PRESTON A·Filed 2011·Granted Dec 11, 2012·5 cites·9 claims
- 0678US8083171B2Supersonic aircraft for reducing sonic boom effects at ground levelHENNE PRESTON A·Filed 2007·Granted Dec 27, 2011·11 cites·22 claims
- 0778US4858852ADivergent trailing-edge airfoilMC DONNELL DOUGLAS CORP·Filed 1987·Granted Aug 22, 1989·35 cites·5 claims
- 0871US7878759B2Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristicsROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Feb 1, 2011·25 cites·49 claims
- 0970USRE47304ENozzle arrangement and method of making the sameGULFSTREAM AEROSPACE CORP·Filed 2017·Granted Mar 19, 2019·1 cites·19 claims
- 1070US9334801B2Supersonic aircraft jet engine installationHENNE PRESTON A·Filed 2012·Granted May 10, 2016·2 cites·27 claims
- 1170US9121369B2Nozzle arrangement and method of making the sameCONNERS TIMOTHY R·Filed 2012·Granted Sep 1, 2015·3 cites·19 claims
- 1268US7634941B2Sub-scale sonic boom modelingGULFSTREAM AEROSPACE CORP·Filed 2008·Granted Dec 22, 2009·5 cites·9 claims
- 1361US9353704B2Air inlet arrangement and method of making the sameCONNERS TIMOTHY R·Filed 2012·Granted May 31, 2016·1 cites·20 claims
- 1460US5322246AIce prevention device for airfoilsMC DONNELL DOUGLAS CORP·Filed 1991·Granted Jun 21, 1994·38 cites·8 claims
- 1556US11208969B2Air inlet arrangement and method of making the sameGULFSTREAM AEROSPACE CORP·Filed 2015·Granted Dec 28, 2021·0 cites·14 claims
- 1652US10731556B2Isentropic compression inlet for supersonic aircraftGULFSTREAM AEROSPACE CORP·Filed 2016·Granted Aug 4, 2020·0 cites·2 claims
- 1747US9714084B2Supersonic aircraft with spike for controlling and reducing sonic boomGULFSTREAM AEROSPACE CORP·Filed 2013·Granted Jul 25, 2017·0 cites·14 claims
- 1841US8789789B2Supersonic aircraft with spike for controlling and reducing sonic boomHENNE PRESTON A·Filed 2011·Granted Jul 29, 2014·0 cites·8 claims
- 1939US2007145192A1Supersonic aircraft with spike for controlling and reducing sonic boomGULFSTREAM AEROSPACE CORP·Filed 2006·Application pending·0 cites
- 2038US2005224630A1Supersonic aircraft with spike for controlling and reducing sonic boomGULFSTREAM AEROSPACE CORP·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →