Inventor · disambiguated record
Arnold C. Newton
Also filed as: NEWTON ARNOLD · NEWTON ARNOLD C
26 granted patents·1,850 citations·filing 1985–2003
98Inventor score
Files withROLLS ROYCE PLC26
Top patents by PatentIndex Score
26 records- 0197US5497961AGas turbine engine nacelle assemblyROLLS ROYCE PLC·Filed 1992·Granted Mar 12, 1996·180 cites·11 claims
- 0296US5867979AGas turbine engine systemROLLS ROYCE PLC·Filed 1997·Granted Feb 9, 1999·209 cites·16 claims
- 0396US5746391AMounting for coupling a turbofan gas turbine engine to an aircraft structureROLLS ROYCE PLC·Filed 1996·Granted May 5, 1998·256 cites·31 claims
- 0496US5694765AShaft power transfer in gas turbine engines with machines operable as generators or motorsROLLS ROYCE PLC·Filed 1994·Granted Dec 9, 1997·318 cites·31 claims
- 0593US6378293B1Gas turbine engine bearing arrangementROLLS ROYCE PLC·Filed 2000·Granted Apr 30, 2002·72 cites·8 claims
- 0693US4731991AGas turbine engine thrust reverserROLLS ROYCE PLC·Filed 1986·Granted Mar 22, 1988·61 cites·11 claims
- 0790US6070407ADucted fan gas turbine engine with variable area fan duct nozzleROLLS ROYCE PLC·Filed 1996·Granted Jun 6, 2000·67 cites·2 claims
- 0885US6729140B2Electrical machineROLLS ROYCE PLC·Filed 2002·Granted May 4, 2004·44 cites·15 claims
- 0985US5687561ADucted fan gas turbine engine accessory driveROLLS ROYCE PLC·Filed 1996·Granted Nov 18, 1997·71 cites·3 claims
- 1085US4968217AVariable pitch arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 1989·Granted Nov 6, 1990·64 cites·12 claims
- 1183US4716724AGas turbine engine powerplant with flow control devicesROLLS ROYCE PLC·Filed 1987·Granted Jan 5, 1988·37 cites·3 claims
- 1282US4823547AThrust reverserROLLS ROYCE PLC·Filed 1987·Granted Apr 25, 1989·35 cites·12 claims
- 1381US5860276ADucted fan gas turbine engine mountingROLLS ROYCE PLC·Filed 1997·Granted Jan 19, 1999·64 cites·4 claims
- 1481US5860275AMethod of combining ducted fan gas turbine engine modules and aircraft structureROLLS ROYCE PLC·Filed 1997·Granted Jan 19, 1999·77 cites·10 claims
- 1581US5253470AGas turbine engine startingROLLS ROYCE PLC·Filed 1992·Granted Oct 19, 1993·59 cites·6 claims
- 1680US6170253B1Cascade structure arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 1998·Granted Jan 9, 2001·62 cites·5 claims
- 1778US6832486B2Electrical machineROLLS ROYCE PLC·Filed 2003·Granted Dec 21, 2004·19 cites·13 claims
- 1874US4766723ATurbofan gas turbine engine and mountings thereforeROLLS ROYCE PLC·Filed 1987·Granted Aug 30, 1987·30 cites·15 claims
- 1970US7107755B2Engine arrangementROLLS ROYCE PLC·Filed 2002·Granted Sep 19, 2006·29 cites·12 claims
- 2059US5516258ADucted fan gas turbine engine nacelle assemblyROLLS ROYCE PLC·Filed 1995·Granted May 14, 1996·34 cites·10 claims
- 2154US6349537B1Vehicle main and auxiliary power unitsROLLS ROYCE PLC·Filed 2000·Granted Feb 26, 2002·11 cites·5 claims
- 2253US4682733AThrust reverserROLLS ROYCE PLC·Filed 1985·Granted Jul 28, 1987·14 cites·2 claims
- 2345US4930307ADucted fan gas turbine engine with surge controllerROLLS ROYCE PLC·Filed 1988·Granted Jun 5, 1990·12 cites·3 claims
- 2443US4934139ATurbofan gas turbine engineROLLS ROYCE PLC·Filed 1989·Granted Jun 19, 1990·11 cites·1 claims
- 2537US5598701AFrangible connection for a thrust reverser for a ducted fan gas turbineROLLS ROYCE PLC·Filed 1995·Granted Feb 4, 1997·8 cites·7 claims
- 2636US5493856AThrust reverser control mechanismROLLS ROYCE PLC·Filed 1994·Granted Feb 27, 1996·6 cites·4 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →