Inventor · disambiguated record
Stuart C. Wright
Also filed as: WRIGHT STUART C
31 granted patents·641 citations·filing 1981–2011
98Inventor score
Top patents by PatentIndex Score
31 records- 0185US4816726AMethod of and arrangement for controlling and h-bridge electric motorUNITED TECHNOLOGIES CORP·Filed 1987·Granted Mar 28, 1989·44 cites·10 claims
- 0279US5222691AAutomatic turn coordination trim control for rotary wing aircraftUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jun 29, 1993·49 cites·6 claims
- 0378US5224664AAdaptive control system input limitingUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jul 6, 1993·49 cites·8 claims
- 0474US5213282AManeuver feel system for a rotary wing aircraftUNITED TECHNOLOGIES CORP·Filed 1991·Granted May 25, 1993·40 cites·10 claims
- 0574US4392203AAircraft coordinated turn with lagged roll rateUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jul 5, 1983·26 cites·2 claims
- 0673US4599698AAircraft trim actuator shutdown monitor system and methodUNITED TECHNOLOGIES CORP·Filed 1983·Granted Jul 8, 1986·28 cites·39 claims
- 0772US4696445ACollective control system for a helicopterUNITED TECHNOLOGIES CORP·Filed 1986·Granted Sep 29, 1987·40 cites·4 claims
- 0871US5169090AAttitude synchronization for model following control systemsUNITED TECHNOLOGIES CORP·Filed 1991·Granted Dec 8, 1992·38 cites·12 claims
- 0968US4626998AHeading reference trim systemUNITED TECHNOLOGIES CORP·Filed 1983·Granted Dec 2, 1986·22 cites·3 claims
- 1067US4484283AAircraft roll-yaw fault protocolsUNITED TECHNOLOGIES CORP·Filed 1981·Granted Nov 20, 1984·24 cites·1 claims
- 1166US5141177AModel following control systemUNITED TECHNOLOGIES CORP·Filed 1991·Granted Aug 25, 1992·30 cites·17 claims
- 1265US4580223AIncorporation of pitch bias actuator function into an existing AFCSUNITED TECHNOLOGIES CORP·Filed 1983·Granted Apr 1, 1986·21 cites·2 claims
- 1364US4577275AFlight director go-around modeUNITED TECHNOLOGIES CORP·Filed 1983·Granted Mar 18, 1986·20 cites·4 claims
- 1461US4371939ARoll attitude inhibit of aircraft coordinated turn disengagementUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·18 cites·2 claims
- 1560US4387432APulsed aircraft actuatorUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·17 cites·4 claims
- 1660US4371937ARetaining airspeed hold engagement in low speed maneuverUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·17 cites·2 claims
- 1756US4385356ANon-saturating airspeed/attitude controlsUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 24, 1983·15 cites·4 claims
- 1855US5178307AHigh speed yaw control system for rotary wing aircraftUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jan 12, 1993·20 cites·13 claims
- 1955US4594714ADual-actuator monitorUNITED TECHNOLOGIES CORP·Filed 1983·Granted Jun 10, 1986·15 cites·2 claims
- 2055US4383299ACommand-inhibited aircraft attitude reference adjustmentUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 10, 1983·14 cites·2 claims
- 2151US4371938AAutomatic airspeed engage/disengageUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·12 cites·4 claims
- 2250US5299759AHelicopter turn coordination and heading hold mode controlUNITED TECHNOLOGIES CORP·Filed 1992·Granted Apr 5, 1994·21 cites·13 claims
- 2349US4385355AAutomatic outer loop centering of aircraft inner loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 24, 1983·11 cites·5 claims
- 2449US4371936AAttitude trimmed airspeed/attitude controlsUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·11 cites·3 claims
- 2545US8862377B2Method and system for detecting forces on aircraftKHIAL KARIM·Filed 2011·Granted Oct 14, 2014·1 cites·16 claims
- 2642US4528628AShutdown monitor for a helicopter pitch bias actuatorUNITED TECHNOLOGIES CORP·Filed 1982·Granted Jul 9, 1985·8 cites·12 claims
- 2741US4387431ARoll attitude inhibit of aircraft automatic outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·7 cites·3 claims
- 2838US4592055AOuter-loop monitor for aircraft automatic flight control systemUNITED TECHNOLOGIES CORP·Filed 1983·Granted May 27, 1986·6 cites·1 claims
- 2937US4387430APitch stick force inhibit of aircraft automatic outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·5 cites·4 claims
- 3036US4477876ADual response aircraft reference synchronizationUNITED TECHNOLOGIES CORP·Filed 1981·Granted Oct 16, 1984·8 cites·5 claims
- 3135US4417308ADual inner loop fault inhibit of aircraft outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Nov 22, 1983·4 cites·2 claims
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