Inventor
ADAMS DON L
37 patents
⚠️ This page may combine multiple inventors who share the name “ADAMS DON L”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
28 patentsUS5222691AJun 29, 1993
Automatic turn coordination trim control for rotary wing aircraft
UNITED TECHNOLOGIES CORP49 citations92
US4816726AMar 28, 1989
Method of and arrangement for controlling and h-bridge electric motor
UNITED TECHNOLOGIES CORP44 citations92
US4696445ASep 29, 1987
Collective control system for a helicopter
UNITED TECHNOLOGIES CORP40 citations92
US4599698AJul 8, 1986
Aircraft trim actuator shutdown monitor system and method
UNITED TECHNOLOGIES CORP28 citations92
US4168045ASep 18, 1979
Speed and collective pitch bias of helicopter longitudinal cyclic pitch
UNITED TECHNOLOGIES CORP52 citations91
US5178307AJan 12, 1993
High speed yaw control system for rotary wing aircraft
UNITED TECHNOLOGIES CORP20 citations82
US4626998ADec 2, 1986
Heading reference trim system
UNITED TECHNOLOGIES CORP22 citations82
US4577275AMar 18, 1986
Flight director go-around mode
UNITED TECHNOLOGIES CORP20 citations82
US4392203AJul 5, 1983
Aircraft coordinated turn with lagged roll rate
UNITED TECHNOLOGIES CORP26 citations82
US4330829AMay 18, 1982
Helicopter flight stability control induced oscillation suppression
UNITED TECHNOLOGIES CORP24 citations82
US4279391AJul 21, 1981
Desensitizing helicopter control response to inadvertent pilot inputs
UNITED TECHNOLOGIES CORP20 citations82
US4484283ANov 20, 1984
Aircraft roll-yaw fault protocols
UNITED TECHNOLOGIES CORP24 citations81
US4580223AApr 1, 1986
Incorporation of pitch bias actuator function into an existing AFCS
UNITED TECHNOLOGIES CORP21 citations74
US4477876AOct 16, 1984
Dual response aircraft reference synchronization
UNITED TECHNOLOGIES CORP8 citations74
US4387431AJun 7, 1983
Roll attitude inhibit of aircraft automatic outer loop
UNITED TECHNOLOGIES CORP7 citations74
US4387432AJun 7, 1983
Pulsed aircraft actuator
UNITED TECHNOLOGIES CORP17 citations74
US4385355AMay 24, 1983
Automatic outer loop centering of aircraft inner loop
UNITED TECHNOLOGIES CORP11 citations74
US4385356AMay 24, 1983
Non-saturating airspeed/attitude controls
UNITED TECHNOLOGIES CORP15 citations74
US4383299AMay 10, 1983
Command-inhibited aircraft attitude reference adjustment
UNITED TECHNOLOGIES CORP14 citations74
US4371937AFeb 1, 1983
Retaining airspeed hold engagement in low speed maneuver
UNITED TECHNOLOGIES CORP17 citations74
US4371936AFeb 1, 1983
Attitude trimmed airspeed/attitude controls
UNITED TECHNOLOGIES CORP11 citations74
US4371938AFeb 1, 1983
Automatic airspeed engage/disengage
UNITED TECHNOLOGIES CORP12 citations74
US4371939AFeb 1, 1983
Roll attitude inhibit of aircraft coordinated turn disengagement
UNITED TECHNOLOGIES CORP18 citations74
US4127245ANov 28, 1978
Helicopter pitch rate feedback bias for pitch axis maneuvering stability and load feel
UNITED TECHNOLOGIES CORP13 citations72
US4528628AJul 9, 1985
Shutdown monitor for a helicopter pitch bias actuator
UNITED TECHNOLOGIES CORP8 citations70
US4885514ADec 5, 1989
Arrangement for controlling the position of an aircraft control surface
UNITED TECHNOLOGIES CORP9 citations69
US4417308ANov 22, 1983
Dual inner loop fault inhibit of aircraft outer loop
UNITED TECHNOLOGIES CORP4 citations63
US4387430AJun 7, 1983
Pitch stick force inhibit of aircraft automatic outer loop
UNITED TECHNOLOGIES CORP5 citations63
ADAMS DON L
4 patentsUS5117867AJun 2, 1992
Manifold for a differential pressure transmitter
ADAMS DON L28 citations92
US4977917ADec 18, 1990
Modular differential pressure transmitter/manifold for a fluid conveying pipeline
ADAMS DON L41 citations92
US7369943B2May 6, 2008
Powered mobility vehicle collision damage prevention device
ADAMS DON L8 citations73
US5104151AApr 14, 1992
Coupler apparatus for connecting a conduit to an equipment opening having damaged threads
ADAMS DON L18 citations73