P

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 patents
US5222691AJun 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 patents

D A MANUFACTURING CO INC

2 patents

(unassigned)

2 patents

SIKORSKY AIRCRAFT CORP

1 patent