Inventor · disambiguated record
Robert Thies
Also filed as: THIES ROBERT · THIES ROBERT W · THIES ROBERT WAYNE
10 granted patents·4 pending applications·196 citations·filing 1988–2020
87Inventor score
Top patents by PatentIndex Score
14 records- 0193US4865902AMultilayered polyolefin high shrinkage, low-shrink force shrink filmDU PONT·Filed 1988·Granted Sep 12, 1989·155 cites·24 claims
- 0284US9416734B2Accessory mounting for a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2012·Granted Aug 16, 2016·17 cites·13 claims
- 0381US8857193B2Intermediate casing for a gas-turbine engineTHIES ROBERT·Filed 2011·Granted Oct 14, 2014·9 cites·13 claims
- 0478US11346283B2Engine assembly with cover memberROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2020·Granted May 31, 2022·2 cites·19 claims
- 0572US8640436B2Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engineTHIES ROBERT·Filed 2010·Granted Feb 4, 2014·5 cites·11 claims
- 0668US10309309B2Air guiding device and aircraft engine with air guiding deviceROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jun 4, 2019·2 cites·17 claims
- 0763US8826637B2Arrangement for the discharge of oil-venting air on a gas-turbine engineTHIES ROBERT·Filed 2010·Granted Sep 9, 2014·3 cites·20 claims
- 0862US10174674B2Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed airROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jan 8, 2019·1 cites·9 claims
- 0959US9027323B2Bloom mixer for a turbofan engineTHIES ROBERT·Filed 2011·Granted May 12, 2015·2 cites·7 claims
- 1058US2007298273A1Multilayer shrink films having a core layer of EVA/ionomer blendBEMIS CLYSAR INC·Filed 2006·Application pending·0 cites
- 1156US2014302295A1Multilayer shrink films having a core layer of eva/ionomer blendCLYSAR LLC·Filed 2014·Application pending·0 cites
- 1242US10669036B2Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end elementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Jun 2, 2020·0 cites·19 claims
- 1340US2018044031A1Turbofan engine comprising an overpressure flap at a fairing being located at the secondary flow channelROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Application pending·0 cites
- 1436US2011116908A1Gas turbine engine with an arrangement for measuring the shaft rotation speedROLLS ROYCE DEUTSCHLAND·Filed 2010·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →