About 30,000 Trademarks found for “rotech flight safety inc”

Health care and medical services, including inhalation therapy services and inhalation therapy medication related services

The mark consists of stylized word "ROTECH" in dimensional block letters with horizontal lines through the letters.

[ Medical staff recruitment and placement services; medical staffing services, namely, recruitment and placement of nurses, nurses' aides, paramedics, emergency medical technicians, physicians and other healthcare professionals and medical specialists; ] distributorship services in the field of respiratory and durable medical equipment and apparatus, namely, resuscitation equipment, nebulisers, portable oxygen systems and respiratory systems, masks, nasal pillows, tubing, head gear, filters, wheelchairs, scooters, walkers, canes, hospital beds, lift chairs and recliners, patient lifts and slings, and therapeutic and pressure relief mattresses

Distributorship services in the field of medical equipment and apparatus, including, stationary oxygen systems and respiratory systems and supplies, bathroom aides, diabetic monitors and supplies, breast pumps, muscle stimulators, lymphedema pumps and supplies, oximetry equipment, enteral pumps and enteral nutrition and supplies, phototherapy equipment, ventilators, incontinent products, ostomy products, wheelcharis, apnea monitors and supplies, cervical traction equipment, and continuous positive airway pressure patient ventalation equipment, and therapeutic ventilators and masks, acessories and supplies, hospital bed accessories

IN THE STATEMENT COLUMN 2, LINE 5, "3-36-2002" SHOULD BE DELETED, AND 9-1-1981 SHOULD BE DELETED.

Statement(s): Column 2, line 6, First Use:03-26-2002, should be deleted, and 09-01-1981, should be inserted.

Aircraft Instruments and Components Thereof, Including Lift Detector, Lift Transducer, Lift Computer, Lift Computer Adjustment Unit, Speed Control Indicator/Lift Computer, Lift Coupler, Lift Signal Comparator, Lift Signal Analyzer, Lift System Test Indicator, Lift Computer Adjustment Unit Analyzer, Lift Transducer Test Gauge, Lift Transducer Test Weight, Signal Summing Unit, Signal Summing and Relay Unit, Signal Summing and Relay Unit Adjustment Head, Adapter Unit, Signal Comparator, Flap Potentiometer, Flap Position Potentiometer, Flap Transmitter, Flap Position Transmitter, Flap Condition Transmitter, Flap Condition Potentiometer, Instrument Vibrator, Instrument Panel Vibrator, Control Vibrator, Control Shaker, Coaxial Control Shaker, Rudder Pedal Shaker, Control Shaker Striker Assembly, Instrument Panel Adapter, Pre-Stall Warning Unit, Gear Pre-Stall Warning Unit, Automatic Power Controller, Servo Amplifier, Ground Plane Accelerometer, Thrust Transducer, Anti-Icing Heater, Lift Signal Calibrator, Indicators, Gyroscope, Magnetic Amplifier, Transformer, [ Reactor, Choke, Inductor, Resistor, Potentiometer, Solid State Diode, Transistor, Rectifiers, Capacitor, Relays (Power, Sensitive, Polar, Nonpolar, and Time Delay), Switch, Chopper, ] Anti-Icing Electric Heater, [ Electric Lights, ] Electric Motor, Servo Motor, [ Counter, ] Servo Amplifier, Servo Disconnect, [ Vibration Isolator, Connector, ] Absolute Pressure Transducer, Differential Pressure Transducer [, Light Filter, Insulator, Socket, Cable, Wire, Chassis, Terminal Board ]

IN THE STATEMENT, COLUMN 2, LINE 6, "ALTITUDE" SHOULD BE DELETED AND "ATTITUDE" SHOULD BE INSERTED.

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

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

Color is not claimed as a feature of the mark.