Inventor
Arnold C. Newton
Inventor
Derby, GB
Overview
Patents· 27 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F02Cprimary
F02CGas-turbine plants20%
F02KJet-propulsion plants17%
Y02TClimate change mitigation technologies related to transportation12%
B64DEquipment for fitting in or to aircraft11%
F01DNon-positive displacement machines or engines, e.g. steam turbines11%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants9%
B64CAeroplanes5%
F04DNon-positive-displacement pumps3%
F16CShafts3%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers3%
PatentTitleYear
11,118,629Curved beam centering spring for a thrust bearing20217,107,755'Engine arrangement'20066,832,486'Electrical machine'20046,729,140'Electrical machine'20046,378,293'Gas turbine engine bearing arrangement'20026,349,537'Vehicle main and auxiliary power units'20026,170,253'Cascade structure arrangement for a gas turbine engine'20016,070,407'Ducted fan gas turbine engine with variable area fan duct nozzle'20005,867,979'Gas turbine engine system'19995,860,276'Ducted fan gas turbine engine mounting'19995,860,275'Method of combining ducted fan gas turbine engine modules and aircraft structure'19995,746,391'Mounting for coupling a turbofan gas turbine engine to an aircraft structure'19985,694,765'Shaft power transfer in gas turbine engines with machines operable as generators or motors'19975,687,561'Ducted fan gas turbine engine accessory drive'19975,598,701'Frangible connection for a thrust reverser for a ducted fan gas turbine'19975,516,258'Ducted fan gas turbine engine nacelle assembly'19965,497,961'Gas turbine engine nacelle assembly'19965,493,856'Thrust reverser control mechanism'19965,253,470'Gas turbine engine starting'19934,968,217'Variable pitch arrangement for a gas turbine engine'19904,934,139'Turbofan gas turbine engine'19904,930,307'Ducted fan gas turbine engine with surge controller'19904,823,547'Thrust reverser'19894,731,991'Gas turbine engine thrust reverser'19884,716,724'Gas turbine engine powerplant with flow control devices'19884,766,723'Turbofan gas turbine engine and mountings therefore'19874,682,733'Thrust reverser'1987Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1987–2006Patents assigned to ROLLS ROYCE PLC (26)· patent assignee history
1987–2006Based in Derby, GB· patent location history
1990Based in Ockbrook, GB· patent location history
2021Patents assigned to RAYTHEON TECH CORP (1)· patent assignee history
2021Patents assigned to UNITED TECHNOLOGIES CORP (1)· patent assignee history
2021Based in Ellington, CT, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| ROLLS ROYCE PLC | 26 | 1987–2006 |
| RAYTHEON TECH CORP | 1 | 2021 |
| UNITED TECHNOLOGIES CORP | 1 | 2021 |
Locations
| Location | Patents | Span |
|---|---|---|
| Derby, GB | 25 | 1987–2006 |
| Ellington, CT, US | 1 | 2021 |
| Ockbrook, GB | 1 | 1990 |