airborne power control systems for landing an aircraft comprised of apparatus for controlling airspeed as a function of altitude during a landing maneuver; "FLARE"
Airborne power control systems for landing an aircraft comprised of apparatus for controlling airspeed as a function of altitude during a landing maneuver; "FLARE"
Marine Instruments and Components Thereof-Namely, Wind Auto Pilot System for Sailboats Comprising Power/Computer, Binnacle, Control Unit, Indicator Assembly, Wind Direction Indicator Assembly, Auto-Warm Assembly, Close Hauled Apparent Wind Indicator, Wind Speed Indicator, Speed Indicator, Wind Vane/Anemometer Assembly, Junction Box Assembly, Switch/Dimmer Control Assembly, Zero Adjust Indicator, Gyro Compass/True Wind Indicator, and Test Set; Water Angle Indicator Assembly, Water Speed Sensor Assembly, and Water Angle Sensor Assembly, Propellor Position Indicator; and Mechanism in the Nature of a Lock Comprising Disks with Interlocking Pin for Controlling the Shape of a Roller Furling Headsail on a Sailboat When Sail Is Reefed; Aircraft Instruments and Components Thereof-Namely, Angle of Attack Transducer, Angle of Attack Encoder Transducer, Lift Comparator Assembly, Limit Switching Assembly, Lift Input Assembly, Gust and Mixer Inputs Assembly, Wind Shear Indicator, Torque Limiter, Speed Control Indicator Adjustment Unit, Radio Rack Mounting Assembly, Angle of Attack Indicator, Alpha/Mach Computer, Airspeed Select Controller, Speed Command Indexer Controller, Performance Computer Controller, Performance Computer, Indexer Controller Assembly, Altitude Alerter Controller, Altitude Alerter Computer, Wind Shear Annunciator, Wind Shear Computer Assembly, Wind Shear Computer Assembly with Aural Alert; Test Sets for: Speed Command Computer, Speed Command of Attitude and Thrust Computer Module, Speed Command of Attitude and Thrust Calibration Module, Speed Command of Attitude and Thrust Acceleration Module, Servo Amplifier, Flap Transmitter, Pendulous Accelerometer, Signal Summing Unit, Prestall Warning, Characterization Module, Lift Transducer, Continuity Tester, Calibration, Comparator, Associated Ground Equipment for Control Column Shaker, Computer Module, Test Adapter-Speed Command of Attitude and Thrust Connector, Continuity Test Adapter Assembly, Apparatus in the Nature of an Electronic Circuit/Clock Combination for Use in Measuring the Time Constant of a Varying Electrical Signal, Lift Transducer Force Applicator, Pressure Transducer, Card Tester, Lift Transducer Simulator, Lift Transducer Test Weight Set, and Alpha/Mach System Analyzer
SERVO ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, [ CALIBRATION MODULE, ] COMPUTER MODULE, SPEED COMMAND COMPUTER, PENDULOUS ACCELEROMETER, AMPLIFIER FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, AIRSTREAM ANGLE SENSOR, AIRSTREAM ANGLE DATA COMPUTER, CHARACTERIZATION UNIT, ACCELERATION MODULE, LIFT DATA COMPUTER, COMPUTER FOR A SPEED COMMAND OF [ ALTITUDE ] * ATTITUDE * AND THRUST SYSTEM, [ LIFT TRANSDUCER ADAPTER, ] AND SERVOMOTOR ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT; GEAR BOX AND CLUTCH ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT
Automatic throttle control system for aircraft, namely, computers for controlling power output of aircraft engines; instruments used in aircraft automatic throttle systems; electronic controllers for engaging and disengaging automatic throttle systems for aircraft; control and display screens used in aircraft for automatic throttle system; systems for automatically maintaining a particular airspeed or engine setting in aircraft
Computers for managing aircraft engine thrust; [ Computers with dual monitors for managing aircraft control devices; ] Avionic instruments for measuring angle of attack of an aircraft in flight; Computers for warning of impending aircraft loss of lift and preventing loss of lift; Heater current monitor; Converters for translating aircraft angle of attack into different electrical formats; Avionic sensor systems, namely, processors for optimizing aircraft takeoff, climb and descent; Instruments for aligning aircraft angle-of-attack transducers, transmitters and sensors; [ Instruments used in aircraft automatic throttle systems including a processor for to prevent forces from the engine linkage from moving the throttles in the cockpit; ] Computers that warn of airflow downburst requiring corrective action; Automatic throttle control systems for aircraft; Electronic controllers for engaging and disengaging automatic throttle systems for aircraft; Autopower computer; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Control and display screens used for automatic throttle system for aircraft; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Avionic sensor systems, namely, processors for minimizing modification of throttle control assemblies in aircraft; Avionic sensor systems, namely, aircraft approach speed indicators; Avionic sensor systems, namely, aircraft speed control indicators; Avionic sensor systems, namely, instruments for indicating angle of attack of an aircraft in flight; Avionic sensor systems, namely, instruments for sensing angle of attack of an aircraft in flight; Avionic sensor systems, namely, processors for indicating angle of attack of an aircraft in flight; Ice detector; Optical ice detector; [ Sensors for detecting aircraft flap deflection angle; ] Computers for controlling aircraft performance; Avionic sensor systems, namely, processors for monitoring helicopter engine and rotor system and warning of maximum ratings for the engine, transmission or rotor system; Avionic sensor systems, namely, processors for monitoring and warning of aircraft operation near live transmission lines; Avionic sensor systems, namely, processors for converting antenna impedance; [ Avionic sensor systems, namely, processors for monitoring aircraft landing lights; ] Avionic sensor systems, namely, processors for optimizing aircraft performance in takeoffs, climbs, approaches and upset recovery; Avionic sensor systems, namely, processors for preventing aircraft stall; Avionic sensor systems, namely, processors for providing warning of impending aircraft stall; Horn used in aircraft for providing warning of impending aircraft stall; Horn assemblies for installation in aircraft cockpit
Computers for managing aircraft engine thrust; Computers with dual monitors for managing aircraft control devices; Avionic instruments for measuring angle of attack of an aircraft in flight; Computers for warning of impending aircraft loss of lift and preventing loss of lift; Heater current monitor; Converters for translating aircraft angle of attack into different electrical formats; Avionic sensor systems, namely, processors for optimizing aircraft takeoff, climb and descent; Instruments for aligning aircraft angle-of-attack transducers, transmitters and sensors; Instruments used in aircraft automatic throttle systems including a processor for to prevent forces from the engine linkage from moving the throttles in the cockpit; Computers that warn of airflow downburst requiring corrective action; Automatic throttle control systems for aircraft; Electronic controllers for engaging and disengaging automatic throttle systems for aircraft; Autopower computer; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Control and display screens used for automatic throttle system for aircraft; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Avionic sensor systems, namely, processors for minimizing modification of throttle control assemblies in aircraft; Avionic sensor systems, namely, aircraft approach speed indicators; Avionic sensor systems, namely, aircraft speed control indicators; Avionic sensor systems, namely, instruments for indicating angle of attack of an aircraft in flight; Avionic sensor systems, namely, instruments for sensing angle of attack of an aircraft in flight; Avionic sensor systems, namely, processors for indicating angle of attack of an aircraft in flight; Ice detector; Optical ice detector; Sensors for detecting aircraft flap deflection angle; Computers for controlling aircraft performance; Avionic sensor systems, namely, processors for monitoring helicopter engine and rotor system and warning of maximum ratings for the engine, transmission or rotor system; Avionic sensor systems, namely, processors for monitoring and warning of aircraft operation near live transmission lines; Avionic sensor systems, namely, processors for converting antenna impedance; Avionic sensor systems, namely, processors for monitoring aircraft landing lights; Avionic sensor systems, namely, processors for optimizing aircraft performance in takeoffs, climbs, approaches and upset recovery; Avionic sensor systems, namely, processors for preventing aircraft stall; Avionic sensor systems, namely, processors for providing warning of impending aircraft stall; Horn used in aircraft for providing warning of impending aircraft stall; Horn assemblies for installation in aircraft cockpit
SERVO MOTOR, [ SERVO MOTOR/GENERATOR, TRANSFORMER, REACTOR, CHOKE, INDUCTOR, TRANSISTOR, RECTIFIER, CAPACITOR, RELAY, SWITCH, CHOPPER, ELECTRIC ANTIICING HEATER, ELECTRIC LIGHT, ] ELECTRIC MOTOR [, ELECTRICAL CONNECTOR, INSULATOR, SOCKET, CABLE, WIRE AND CHASSIS, TERMINAL BOARD, LIGHT FILTER, VIBRATION ISOLATOR, METAL COMPONENT CARD AND PRINTED CIRCUIT CARD ]; AERONAUTICAL AND NAVIGATIONAL INSTRUMENTS-, namely, LIFT DETECTORS, LIFT TRANSDUCERS, LIFT TRANSDUCER TEST GAUGE, LIFT TRANSDUCER TEST WEIGHT, LIFT TRANSDUCER ADAPTER UNIT, LIFT TRANSDUCER TEST SET, LIFT COMPUTER, LIFT COMPUTER ADJUSTMENT UNIT, LIFT COMPUTER ADJUSMENT UNIT ANALYZER, SIGNAL SUMMING UNIT, SIGNAL SUMMING AND RELAY UNIT, LIFT SIGNAL COMPARATOR, LIFT SIGNAL ANALYZER, SIGNAL SUMMING AND RELAY UNIT ADJUSTMENT UNIT, SPEED CONTROL INDICATOR/LIFT COMPUTER, SPEED CONTROL INDICATOR, SPEED COMMAND INDICATOR, INDICATOR FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, LANDING SPEED INDICATOR, LIFT RATIO INDICATOR, [ SPEED RATIO INDICATOR, ] LIFT SYSTEM TEST INDICATOR, LIFT SIGNAL CALIBRATOR, [ LIFT DATA COMPUTER, LIFT SIGNAL COMPARATOR, SIGNAL COMPARATOR, LIFT COUPLER, ] SPEED COMMAND COMPUTER, COMPUTER FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, [ COMPUTER CHARACTERIZATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER ACCELERATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER CALIBRATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, ROTATION/GO-AROUND COMPUTER, ] FLAP POSITION POTENTIOMETER, FLAP POSITION TRANSMITTER, INSTRUMENT VIBRATOR, INSTRUMENT PANEL VIBRATOR, CONTROL SHAKER, COAXIAL CONTROL SHAKER, RUDDER PEDAL SHAKER, WARNING UNIT, DUAL WARNING UNIT, DUAL WARNING AND FLASHER UNIT, LANDING GEAR WARNING UNIT, [ COUNTER, PENDULOUS ACCELEROMETER, GROUND PLANE ACCELEROMETER, VERTICAL ACCELEROMETER, VERTICAL GYROSCOPE, THRUST TRANSDUCER, ] ABSOLUTE PRESSURE TRANSDUCER, DIFFERENTIAL PRESSURE TRANSDUCER, SERVO ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, CLUTCH ASSEMBLY, CLUTCH, REVERSE LOCKING CLUTCH, GEARBOX ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, AMPLIFIER FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, COMPUTER/AMPLIFIER FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, AIRSTREAM ANGLE SENSOR, AIRSTREAM ANGLE DATA COMPUTER, INDICATOR [, INSTRUMENT PANEL ADAPTER, MAGNETIC AMPLIFIER, SERVO AMPLIFIER, SERVO DISCONNECT, POTENTIOMETER, RESISTOR AND DIODE ]
