Inventor · disambiguated record
Richard G Stretton
Also filed as: STRETTON RICHARD G · STRETTON RICHARD GEOFFREY
54 granted patents·20 pending applications·977 citations·filing 2000–2024
98Inventor score
Top patents by PatentIndex Score
74 records- 0198US10760530B2Fan arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2019·Granted Sep 1, 2020·15 cites·11 claims
- 0298US10648475B1Turbine engineROLLS ROYCE PLC·Filed 2019·Granted May 12, 2020·17 cites·17 claims
- 0398US10583932B1Aero engine flow rateROLLS ROYCE PLC·Filed 2019·Granted Mar 10, 2020·22 cites·20 claims
- 0498US8876465B2Gas turbine engineSTRETTON RICHARD G·Filed 2011·Granted Nov 4, 2014·62 cites·19 claims
- 0597US7810312B2Heat exchanger arrangementROLLS ROYCE PLC·Filed 2007·Granted Oct 12, 2010·63 cites·12 claims
- 0697US7806363B2Engine mounting assemblyROLLS ROYCE PLC·Filed 2005·Granted Oct 5, 2010·56 cites·17 claims
- 0796US8967967B2Propfan engineSTRETTON RICHARD G·Filed 2012·Granted Mar 3, 2015·47 cites·17 claims
- 0896US7090165B2Aeroengine nacelleROLLS ROYCE PLC·Filed 2003·Granted Aug 15, 2006·101 cites·9 claims
- 0995US7398641B2Aeroengine intake having a heat exchanger within an annular closed chamberROLLS ROYCE PLC·Filed 2004·Granted Jul 15, 2008·90 cites·11 claims
- 1094US7770292B2Engine core stand arrangement and method of removal and transportation of an engine coreROLLS ROYCE PLC·Filed 2007·Granted Aug 10, 2010·48 cites·16 claims
- 1193US11053947B2Turbine engineROLLS ROYCE PLC·Filed 2020·Granted Jul 6, 2021·3 cites·17 claims
- 1293US7886520B2Gas turbine engineROLLS ROYCE PLC·Filed 2007·Granted Feb 15, 2011·70 cites·12 claims
- 1392US11204037B2Turbine engineROLLS ROYCE PLC·Filed 2021·Granted Dec 21, 2021·2 cites·13 claims
- 1492US9387923B2Gas turbine engineROLLS ROYCE PLC·Filed 2013·Granted Jul 12, 2016·17 cites·18 claims
- 1592US7861513B2Aeroengine ventilation systemROLLS ROYCE PLC·Filed 2007·Granted Jan 4, 2011·29 cites·18 claims
- 1692US7484354B2Aircraft engine arrangementROLLS ROYCE PLC·Filed 2005·Granted Feb 3, 2009·41 cites·17 claims
- 1790US9346551B2Engine installationROLLS ROYCE PLC·Filed 2014·Granted May 24, 2016·14 cites·15 claims
- 1890US7086219B2Cowl structure for a gas turbine engineROLLS ROYCE PLC·Filed 2005·Granted Aug 8, 2006·24 cites·2 claims
- 1989US10981663B2Aero engine flow rateROLLS ROYCE PLC·Filed 2020·Granted Apr 20, 2021·2 cites·17 claims
- 2088US9701412B2Aircraft engine mountROLLS ROYCE PLC·Filed 2014·Granted Jul 11, 2017·12 cites·18 claims
- 2188US7255528B2Liner for a gas turbine engine casingROLLS ROYCE PLC·Filed 2004·Granted Aug 14, 2007·37 cites·25 claims
- 2288US6434927B1Thrust reverserROLLS ROYCE PLC DERBY·Filed 2000·Granted Aug 20, 2002·44 cites·7 claims
- 2387US8444085B2Support structureSTRETTON RICHARD G·Filed 2011·Granted May 21, 2013·12 cites·11 claims
- 2487US8322652B1Thrust mount arrangement for an aircraft engineSTRETTON RICHARD G·Filed 2010·Granted Dec 4, 2012·13 cites·12 claims
- 2586US11339713B2Large-scale bypass fan configuration for turbine engine core and bypass flowsROLLS ROYCE PLC·Filed 2019·Granted May 24, 2022·3 cites·15 claims
- 2682US8297038B2Gas turbine aircraft engines and operation thereofSTRETTON RICHARD G·Filed 2010·Granted Oct 30, 2012·8 cites·27 claims
- 2780US8434995B2Duct wall for a fan of a gas turbine enginePOOL CLARE L·Filed 2010·Granted May 7, 2013·10 cites·14 claims
- 2880US2024376847A1Geared gas turbine engineROLLS ROYCE PLC·Filed 2024·Application pending·0 cites
- 2979US6892526B2Cowl structure for a gas turbine engineROLLS ROYCE PLC·Filed 2003·Granted May 17, 2005·26 cites·12 claims
- 3079US2025035037A1Turbine engine core and bypass flowsROLLS ROYCE PLC·Filed 2024·Application pending·0 cites
- 3178US6474059B2Thrust reverserROLLS ROYCE PLC·Filed 2002·Granted Nov 5, 2002·30 cites·1 claims
- 3275US11156167B2CasingROLLS ROYCE PLC·Filed 2019·Granted Oct 26, 2021·2 cites·9 claims
- 3375US9771873B2Bifurcation fairingROLLS ROYCE PLC·Filed 2015·Granted Sep 26, 2017·2 cites·12 claims
- 3475US8506234B2Duct wall for a fan of a gas turbine engineBROOKS RICHARD V·Filed 2010·Granted Aug 13, 2013·6 cites·5 claims
- 3574US10240536B2Fluid systemROLLS ROYCE PLC·Filed 2015·Granted Mar 26, 2019·2 cites·11 claims
- 3672US12163464B2Turbine engine core and bypass flows having a defined fan-turbine radial distanceROLLS ROYCE PLC·Filed 2022·Granted Dec 10, 2024·0 cites·10 claims
- 3772US11988169B2Fan arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2021·Granted May 21, 2024·0 cites·12 claims
- 3871US10968835B2Apparatus for gas turbine enginesROLLS ROYCE PLC·Filed 2019·Granted Apr 6, 2021·1 cites·9 claims
- 3971US2021148306A1Fan arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2021·Application pending·0 cites
- 4070US10539095B2Aircraft gas turbine engine nacelleROLLS ROYCE PLC·Filed 2017·Granted Jan 21, 2020·1 cites·12 claims
- 4170US8453458B2Gas turbine engine variable exhaust nozzleWHURR JOHN R·Filed 2007·Granted Jun 4, 2013·11 cites·15 claims
- 4270US2020408170A1Fan arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2020·Application pending·0 cites
- 4369US11408428B2Turbine engineROLLS ROYCE PLC·Filed 2021·Granted Aug 9, 2022·0 cites·18 claims
- 4467US12276225B2Gas turbine engineROLLS ROYCE PLC·Filed 2023·Granted Apr 15, 2025·0 cites·20 claims
- 4567US2022056916A1Turbine engineROLLS ROYCE PLC·Filed 2021·Application pending·0 cites
- 4666US10882633B2Aero engine flow rateROLLS ROYCE PLC·Filed 2020·Granted Jan 5, 2021·0 cites·18 claims
- 4766US2020347803A1Fan arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2020·Application pending·0 cites
- 4865US2020200096A1Geared gas turbine engineROLLS ROYCE PLC·Filed 2019·Application pending·0 cites
- 4962US9970313B2Unison ring assemblyROLLS ROYCE PLC·Filed 2015·Granted May 15, 2018·1 cites·4 claims
- 5060US11945595B2Support structure for attaching a gas turbine engine to an aircraft pylonROLLS ROYCE PLC·Filed 2022·Granted Apr 2, 2024·0 cites·20 claims
Showing the top 50 of 74 patent records by PatentIndex Score.
Join the waitlist — get patent alerts
Get an alert when Richard G Stretton files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →