Inventor
HENNE PRESTON A
US18 patents
⚠️ This page may combine multiple inventors who share the name “HENNE PRESTON A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GULFSTREAM AEROSPACE CORP
7 patentsUS6698684B1Mar 2, 2004
Supersonic aircraft with spike for controlling and reducing sonic boom
GULFSTREAM AEROSPACE CORP57 citations93
US9482155B2Nov 1, 2016
Isentropic compression inlet for supersonic aircraft
GULFSTREAM AEROSPACE CORP3 citations72
US11208969B2Dec 28, 2021
Air inlet arrangement and method of making the same
GULFSTREAM AEROSPACE CORP0 citations62
USRE47304EMar 19, 2019
Nozzle arrangement and method of making the same
GULFSTREAM AEROSPACE CORP1 citations62
US7634941B2Dec 22, 2009
Sub-scale sonic boom modeling
GULFSTREAM AEROSPACE CORP5 citations60
US10731556B2Aug 4, 2020
Isentropic compression inlet for supersonic aircraft
GULFSTREAM AEROSPACE CORP0 citations51
US9714084B2Jul 25, 2017
Supersonic aircraft with spike for controlling and reducing sonic boom
GULFSTREAM AEROSPACE CORP0 citations51
HENNE PRESTON A
5 patentsUS8286434B2Oct 16, 2012
Isentropic compression inlet for supersonic aircraft
HENNE PRESTON A7 citations82
US8083171B2Dec 27, 2011
Supersonic aircraft for reducing sonic boom effects at ground level
HENNE PRESTON A11 citations80
US8327645B2Dec 11, 2012
Isentropic compression inlet for supersonic aircraft
HENNE PRESTON A5 citations72
US9334801B2May 10, 2016
Supersonic aircraft jet engine installation
HENNE PRESTON A2 citations61
US8789789B2Jul 29, 2014
Supersonic aircraft with spike for controlling and reducing sonic boom
HENNE PRESTON A0 citations48
CONNERS TIMOTHY R
3 patentsUS8333076B2Dec 18, 2012
Isentropic compression inlet for supersonic aircraft
CONNERS TIMOTHY R8 citations82
US9121369B2Sep 1, 2015
Nozzle arrangement and method of making the same
CONNERS TIMOTHY R3 citations61
US9353704B2May 31, 2016
Air inlet arrangement and method of making the same
CONNERS TIMOTHY R1 citations51