Mark:

Status Date:

06-17-1998

Registration Number:

N/A

Goods and Services:

metal valves for aircraft and space installations, and replacement parts for each of the above pneumatic starters for aircraft engines; electromechanical, electro-hydraulic, hydraulic and mechanical actuators for aircraft engines, such as jet engine air inlet hydraulic actuators and jet engine stator vane hydraulic actuators; hydromechanical actuators for aircraft flight control systems; auxiliary power units in the form of gas turbine engines; electrical, electronic and hydromechanical fuel controls for aircraft engines; hydromechanical and electrical engine air inlet controls; rocket propulsion engines; centrifugal water separators; air inlet filtration systems for gas turbine engines; fluid heat-transfer heating and cooling systems for use in aircraft and spacecraft and using mechanical or electromechanical temperature controllers; air cycle machines used as temperature controls in aircraft; water removers for use in aircraft pneumatic systems; fuel pumps, fuel controls for stationary gas turbine engines; gas turbine engine accessories, such as control valves and sensors; fan blades and vanes for aircraft engines and for wind tunnels, wind turbines; inlet filters for use in marine gas turbine engines; automatic and manual test equipment for hydromechanical and electronic fuel controls for aircraft engines; automatic and manual gas turbine aircraft engine trim and diagnostic analyzers; aircraft engine propellers; hydraulic actuators for aircraft engines, such as jet engine nozzle exhaust hydraulic actuators and jet engine thrust reverser hydraulic actuators; electronic and hydromechanical pitch control units for aircraft engine propellers; propulsion fans, and replacement parts for each of the above electromechanical controls for use in aircraft; environmental controls for aircraft; electronic flight controls for use in aircraft and spacecraft; space suit/life support systems for astronauts; environmental controls for spacecraft; electronic static power inverters; electronic static power converters; engine pressure ratio transmitters; electronic synchrophasers for aircraft propellers; data acquisition systems for aircraft, and for engines used in aircraft, marine, and land vehicles, and stationary land installations, and for vehicle systems, namely, electric and suspension systems; pressure transducers sold as part of pressure measuring systems and separately and parts thereof; electric speed sensors and indicators; electronic Automatic Stabilization Equipment (commonly called ASE) for use in aircraft, spacecraft and watercraft; temperature controls; pneumatic and electronic cabin pressure control systems; Ground Support Equipment (commonly called GSE) for aircraft, surface craft, and spacecraft, namely, maintenance and test equipment; engine fuel control test stands; gas management equipment for air revitalization and fluid conversion for use in space travel and subsurface travel; electronic synchrophasers for aircraft engine propellers; oxygen supply systems for space, aircraft and submarine use; Portable Life Support Systems (commonly called PLSS) to control environment for space travel; space suits; diagnostic computers for life support equipment; rate sensors and gyroscopes sold as part of guidance and/or control systems used in aircraft, missiles and space vehicles, and separately; electric power generating plant control simulators; pneumatic, electrical and electronic testers for aircraft engine propeller hubs, air conditioners, engine fuel controls, engine fuel pumps and aircraft and engine actuators; electronic air inlet controls for aircraft; electronic aircraft integrated data acquisition systems for monitoring, diagnosing and prognosticating aircraft subsystems, overall aircraft performance and performance of the aircraft crew; computerized flight control units to control aircraft control surfaces to effect stability augmentation and flight path control in aircraft, namely, helicopters, actuators for controlling control surfaces, namely, the tail flaps of a fixed wing aircraft or the blades of a helicopter; inertial navigation systems for aircraft, comprising gyroscopes, accelerometers, power supplies, and display electronics; guidance and control units which are computer controlled to guide and navigate a spacecraft so as to transport a payload to a selected spot in space, and to control the rate of engine fuel consumption to insure that the spacecraft has sufficient fuel to get to the selected spot in space; attitude control units using rate gyros for controlling the attitude heading of aircraft in flight and the heading of a satellite in orbit; guidance and control systems, namely, attitude controls for projectiles using rate sensors; synchrophasers for aircraft propellers; electrochemical cells, namely, gas generators, fuel cells, compressors and sensors; electronic flight controls for aircraft; accelerometers; electronic ground support equipment for use with aircraft; shipboard electronic equipment for connecting shipboard sensors, such as sonar or radar, to the ship's weapons so as to provide data signals or control signals thereto; aircraft-mounted electronic equipment operable to collect signals on the characteristics of a submarine under surveillance and transmit those signals back to a mother ship for analysis and fire control purposes; computer airborne flight performance monitor apparatus; aircraft-mounted electronic apparatus, namely, a combat computer interface to enable computers and crew to monitor ordinance activities, operation and condition throughout the aircraft; microcomputer control operable to tune the radio frequency antenna couplers which couple multiple ship radios to one or more antennae; radio telemetry apparatus operable to collect information on missile flight and performance for transmissions to ground authority; electronic apparatus for adopting aircraft radios for use aboard ship which form an electronic protective cocoon around the aircraft radio and interconnects aircraft radios to shipboard parameters such as, shipboard power, cooling systems, and environmental controls; portable electronic testers operable to ground test the various aircraft flight systems such as, aircraft avionic systems and avionic submarine warfare subsystems; electrolyzer and replacement parts therefor; electrochemical cells, namely, electrochemical gas generators, electrochemical gas compressors, electrochemical gas sensors, electrochemical power generating fuel devices, and electrochemical gas separators, namely, oxygen generation subsystems having electrolyzers, gas compressors and gas separators, and replacement parts for each; electronic controls, namely, time, humidity, temperature, pressure, current, torque and speed controls; computerized engine and vehicle analyzers for testing and diagnosing engine and vehicle performance; electronic engine monitors; infrared carbon dioxide lasers; oxygen generation for onboard aircraft storage; electronic Flight Management System (commonly called FMS) equipment for aircraft and test equipment and replacement therefor; Performance Management System (commonly called PMS) equipment for aircraft and test equipment and replacement parts therefor; Flight Inspection System (commonly called FIS) equipment for aircraft and test equipment and replacement parts therefor; and Pilot's Performance System (commonly called PPS) equipment for aircraft and test equipment and replacement parts therefor air conditioning systems for environmental control in aircraft; air purifiers for space travel; water removers and reclaimers for space travel; humidification for aircraft cockpits; and heat exchangers for use in aircraft, watercraft, and spacecraft, and replacement parts for each of the above electromechanical, electrohydraulic, hydraulic and mechanical actuators for controlling performance of helicopter rotors

Class:

Vehicles

Published for Opposition Date:

09-23-1997

Mark Drawing Status:

2S21

Business Name:

UNITED TECHNOLOGIES CORP