Inventor · disambiguated record
Don L. Adams
Also filed as: ADAMS DON · ADAMS DON L · ADAMS SR DON L
46 granted patents·3 pending applications·909 citations·filing 1976–2021
98Inventor score
Top patents by PatentIndex Score
49 records- 0190US4168045ASpeed and collective pitch bias of helicopter longitudinal cyclic pitchUNITED TECHNOLOGIES CORP·Filed 1978·Granted Sep 18, 1979·52 cites·6 claims
- 0287US11549832B2Explosion management and methods thereofABB SCHWEIZ AG·Filed 2021·Granted Jan 10, 2023·2 cites·22 claims
- 0387US4003532AHeading hold logicUNITED TECHNOLOGIES CORP·Filed 1976·Granted Jan 18, 1977·45 cites·13 claims
- 0485US4816726AMethod of and arrangement for controlling and h-bridge electric motorUNITED TECHNOLOGIES CORP·Filed 1987·Granted Mar 28, 1989·44 cites·10 claims
- 0582US4977917AModular differential pressure transmitter/manifold for a fluid conveying pipelineADAMS DON L·Filed 1989·Granted Dec 18, 1990·41 cites·5 claims
- 0679US5222691AAutomatic turn coordination trim control for rotary wing aircraftUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jun 29, 1993·49 cites·6 claims
- 0778US5224664AAdaptive control system input limitingUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jul 6, 1993·49 cites·8 claims
- 0876US6314343B1Aircraft flight mode selector systemSIKORSKY AIRCRAFT CORP·Filed 1999·Granted Nov 6, 2001·64 cites·9 claims
- 0974US4392203AAircraft coordinated turn with lagged roll rateUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jul 5, 1983·26 cites·2 claims
- 1073US4599698AAircraft trim actuator shutdown monitor system and methodUNITED TECHNOLOGIES CORP·Filed 1983·Granted Jul 8, 1986·28 cites·39 claims
- 1172US4696445ACollective control system for a helicopterUNITED TECHNOLOGIES CORP·Filed 1986·Granted Sep 29, 1987·40 cites·4 claims
- 1272US4279391ADesensitizing helicopter control response to inadvertent pilot inputsUNITED TECHNOLOGIES CORP·Filed 1979·Granted Jul 21, 1981·20 cites·2 claims
- 1368US7369943B2Powered mobility vehicle collision damage prevention deviceADAMS DON L·Filed 2006·Granted May 6, 2008·8 cites·1 claims
- 1468US4626998AHeading reference trim systemUNITED TECHNOLOGIES CORP·Filed 1983·Granted Dec 2, 1986·22 cites·3 claims
- 1567US4484283AAircraft roll-yaw fault protocolsUNITED TECHNOLOGIES CORP·Filed 1981·Granted Nov 20, 1984·24 cites·1 claims
- 1665US4580223AIncorporation of pitch bias actuator function into an existing AFCSUNITED TECHNOLOGIES CORP·Filed 1983·Granted Apr 1, 1986·21 cites·2 claims
- 1764US4577275AFlight director go-around modeUNITED TECHNOLOGIES CORP·Filed 1983·Granted Mar 18, 1986·20 cites·4 claims
- 1863US6017106ARemovable carry handle and adapter for portable computerGATEWAY 2000 INC·Filed 1999·Granted Jan 25, 2000·52 cites·6 claims
- 1962US5117867AManifold for a differential pressure transmitterADAMS DON L·Filed 1990·Granted Jun 2, 1992·28 cites·8 claims
- 2061US5730394AVertical performance limit compensatorSIKORSKY AIRCRAFT CORP·Filed 1995·Granted Mar 24, 1998·29 cites·22 claims
- 2161US4371939ARoll attitude inhibit of aircraft coordinated turn disengagementUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·18 cites·2 claims
- 2260US4387432APulsed aircraft actuatorUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·17 cites·4 claims
- 2360US4371937ARetaining airspeed hold engagement in low speed maneuverUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·17 cites·2 claims
- 2459US4330829AHelicopter flight stability control induced oscillation suppressionUNITED TECHNOLOGIES CORP·Filed 1980·Granted May 18, 1982·24 cites·4 claims
- 2556US12276529B2Explosion management display and methods thereofABB SCHWEIZ AG·Filed 2021·Granted Apr 15, 2025·0 cites·20 claims
- 2656US4385356ANon-saturating airspeed/attitude controlsUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 24, 1983·15 cites·4 claims
- 2755US5178307AHigh speed yaw control system for rotary wing aircraftUNITED TECHNOLOGIES CORP·Filed 1991·Granted Jan 12, 1993·20 cites·13 claims
- 2855US4383299ACommand-inhibited aircraft attitude reference adjustmentUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 10, 1983·14 cites·2 claims
- 2951US4371938AAutomatic airspeed engage/disengageUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·12 cites·4 claims
- 3049US5104151ACoupler apparatus for connecting a conduit to an equipment opening having damaged threadsADAMS DON L·Filed 1991·Granted Apr 14, 1992·18 cites·6 claims
- 3149US4385355AAutomatic outer loop centering of aircraft inner loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted May 24, 1983·11 cites·5 claims
- 3249US4371936AAttitude trimmed airspeed/attitude controlsUNITED TECHNOLOGIES CORP·Filed 1981·Granted Feb 1, 1983·11 cites·3 claims
- 3344US8985158B2Welded double fabric tubeADAMS DON·Filed 2012·Granted Mar 24, 2015·1 cites·8 claims
- 3444US2004220735A1Powered mobility vehicle collision damage prevention deviceFiled 2004·Application pending·0 cites
- 3543US4127245AHelicopter pitch rate feedback bias for pitch axis maneuvering stability and load feelUNITED TECHNOLOGIES CORP·Filed 1977·Granted Nov 28, 1978·13 cites·6 claims
- 3642US4528628AShutdown monitor for a helicopter pitch bias actuatorUNITED TECHNOLOGIES CORP·Filed 1982·Granted Jul 9, 1985·8 cites·12 claims
- 3742US4314307AElectro-mechanical sensor power up circuitUS NAVY·Filed 1980·Granted Feb 2, 1982·5 cites·1 claims
- 3842US2009089871A1Methods and apparatus for digital data processor instantiationNETWORK ENGINES INC·Filed 2006·Application pending·0 cites
- 3941US9505202B2Method of making a welded double fabric tubeABC CANADA TECH GROUP LTD·Filed 2015·Granted Nov 29, 2016·0 cites·8 claims
- 4041US4387431ARoll attitude inhibit of aircraft automatic outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·7 cites·3 claims
- 4140US2013039776A1Whitewater Hand PaddlesADAMS DON·Filed 2011·Application pending·0 cites
- 4238US4885514AArrangement for controlling the position of an aircraft control surfaceUNITED TECHNOLOGIES CORP·Filed 1987·Granted Dec 5, 1989·9 cites·14 claims
- 4337US4387430APitch stick force inhibit of aircraft automatic outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Jun 7, 1983·5 cites·4 claims
- 4436US4477876ADual response aircraft reference synchronizationUNITED TECHNOLOGIES CORP·Filed 1981·Granted Oct 16, 1984·8 cites·5 claims
- 4535US4417308ADual inner loop fault inhibit of aircraft outer loopUNITED TECHNOLOGIES CORP·Filed 1981·Granted Nov 22, 1983·4 cites·2 claims
- 4633US5595211ASteam trap test stationD A MANUFACTURING CO INC·Filed 1995·Granted Jan 21, 1997·4 cites·5 claims
- 4732US5482081ASingle handle manifoldD A MANUFACTURING CO INC·Filed 1995·Granted Jan 9, 1996·4 cites·11 claims
- 4831USD454939SValve castingFiled 2001·Granted Mar 26, 2002·0 cites·1 claims
- 4930USRE36485ESteam trap test stationFiled 1998·Granted Jan 11, 2000·0 cites·5 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →