AEROSPACE TEMPERATURE PRESSURE SENSORS

Brand Owner (click to sort) Address Description
ESTERLINE ESTERLINE TECHNOLOGIES CORPORATION 500 108th Avenue NE, Suite 1500 Bellevue WA 98004 Aerospace temperature and pressure sensors; [electrical penetration assemblies for containment buildings of nuclear power plants;] illuminated switches; indicators; enunciators; integrated panels providing multiple switching functions; electronic modules and input and output devices for keyboards, namely, computer keyboards, key pads, control panels, switch arrays, and computer interface boards; input components, input products and input devices, namely, encoders, joysticks, electronic computer keyboards, keypads, and computer cursor control devices, namely, trackball, touchscreens and touchpads; interface ports for connecting peripheral devices to a host computer;electronic input controllers; control panels; electronic devices, namely, light emitting diode displays, liquid crystal displays, electron-luminescent and cathode ray tube displays and indicators; slide potentiometers; electromechanical actuators and sensors; [ tachometers; optical encoders; synchros,] resolvers [, and transducers] for use in motion control technology products;ESTER LINE;
ESTERLINE ESTERLINE TECHNOLOGIES CORPORATION 500 108th Avenue NE, Suite 1500 Bellevue WA 98004 Aerospace temperature and pressure sensors; illuminated switches; illuminated indicators; enunciators; integrated panels providing multiple switching functions; electronic modules and input and output devices for keyboards, namely, computer keyboards, key pads, control panels, switch arrays, and computer interface boards; input components, input products and input devices, namely, encoders, joysticks, electronic computer keyboards, keypads, and computer cursor control devices, namely, trackball, touchscreens and touchpads; interface ports for connecting peripheral devices to a host computer; electronic input controllers; electrical control panels; electronic devices, namely, light emitting diode displays, liquid crystal displays, electron-luminescent and [ cathode ray tube displays and indicators; ] slide potentiometers; electromechanical actuators and sensors; electrical resolvers and electromechanical apparatus, namely, rotary switches, potentiometers, switch and potentiometer combinations, rotary push button switches, ammeter shunts, bonding jumpers, flexible bus assemblies, switching systems, namely, autobrake and anti-skid control switches, engine fire shut-off switches, collision avoidance switch panels, aircraft and helicopter engine start switches, flap control switches, and temperature control switches and potentiometers, switches with multiple functions for use in airplane and helicopter cockpits, integrated cockpit assemblies, cockpit instrument data loader switches, and optical encoder switches; electrical membrane switches and switch panels; relays, [ circuit breakers ] and solid state power controllers for switching and controlling electrical power; devices for switching and controlling electrical power, namely, electrical power distribution assemblies; feedback and position electric sensing assemblies for machine tools and aircraft instruments, namely, gauges; electrical instruments, namely, sensors comprising thermocouples, speed probes, resistive temperature devices (RTD), pressure sensors, torque sensors, densitometers, resistors, harnesses, and junction boxes, for measuring physical characteristics, namely, temperature, shaft speed, shaft torque, pressure, density; electronic data processing apparatus and instruments, namely, digital pressure modules, indicators, electronic speed measurement systems, resistors, harnesses, and junction boxes; aeronautical, marine and industrial instruments, namely, thermocouples, speed probes, resistive temperature devices (RTD), pressure sensors, digital pressure modules, torque sensors, densitometers, electronic speed measurement systems, resistors, harnesses, junction boxes and instrument displays; electrical and electronic indicators and display instruments for use with measuring devices and apparatus; thermometers, thermo-couples, resistance temperature sensors, apparatus for the control of temperature using resistive temperature detectors or for the control of pressure using strain gauges and pressure sensors; electrical testing and measuring apparatus, namely, thermocouples, pressure and speed sensors; harnesses and junction boxes for interconnection between sensors and processing, control or display apparatus; voice and data switching hardware and software; secure intercommunications hardware and software for use in airborne, ground and shipboard applications; audio, data and video distribution hardware and software for military and commercial applications; secure communications devices, namely, audio control devices, liquid crystal displays, integrated panels and communications control equipment; communications switches, jackboxes, headsets for use with aircraft; speakers and audio amplifiers; materials for reflecting radio and radar signals, namely, chaff; [ hardware and software, namely, a firing control unit; acoustic signaling equipment, namely, torpedo decoys, scuba diver recall signal devices, and surface-to-submarine signaling devices; radio interference filters; smoke generators; ] scientific, nautical, surveying, photographic, cinematographic, optical, weighing, measuring, signaling, checking, supervision, lifesaving and teaching apparatus and instruments, namely, computer software for allowing flight operators to predetermine if primary-means navigation over oceanic or remote areas is possible; [ scientific, photographic, optical, measuring, signaling, checking, supervision and teaching apparatus and instruments, namely, communication systems, namely, radio receivers, radio transmitters, radio multiplexers, ] test sets, used to test and measure voltage, current, power, phase and other electrical/electronic parameters during the manufacture of electronic equipment and the subsequent operation, maintenance and repair of said equipment; airborne satellite communications antennas; miniaturized electronic devices utilizing active and passive electronic components, namely, hybrid micro-circuits; [ electronic power supply units to generate and supply electrical power of the required form to dependant electrical/electronic apparatus; power conversion units, namely, power conversion units for use to convert voltage levels to required needs; ] aircraft navigation equipment, namely, global positioning systems, radar, and sensors for the determination of positions and distances; instruments used on an aircraft flight deck for monitoring, calculating, and displaying aircraft engine status and parameters; visual display panel units to monitor and display electrical, electronic and mechanical systems parameters, in graphic and/or alphanumeric form, utilizing cathode ray tube, incandescent, fiber optic, and solid state (LCD and LED) forms of illumination; custom panels and display systems comprised of a keyboard, display assemblies, a bracket LED and LCD, circuit card assembly, rotary controls, encoders, toggle switches and high performance optical filters; global positioning system products, namely, global positioning system sensors, global positioning system units for ground stations, airborne use and related software, global positioning system receivers for original equipment manufacturers; electronic flight bag (EFB) for aircraft, comprised of an electronic display and data processing system for cockpit or flightdeck, used for displaying electronic charts, maps, graphical weather information, en-route and approach charts for pre-flight planning, for performing fuel calculations and displaying aviation data; overhead mounted heads-up display consisting primarily of a control panel and an optical unit which receives amplified deflection signals and projects a display on a single adjustable combiner glass; compact antenna system comprised principally of a protective radome, an active array aperture, a power supply, and a controller, for all aircraft types within the aviation market; integrated cockpit avionics suite consisting of integrated avionics computers, flight displays, navigation/systems displays and a suite of communication, navigation and surveillance subsystems; certified aviation GPS receiver; airborne terminal navigation/landing system comprised of antenna coupler units, receiver-processor and central display units; portable mission display specifically designed to facilitate military and para-military airborne mission effectiveness through improved real-time situational awareness; hardware package consisting of optical components namely, lens, infrared detectors; radar components, namely, antenna, transmitter/receiver; signal processors/circuitry, image processors/circuitry and interface/control processors/circuitry in an avionics enclosure with appropriate interference protection components, together with a software package consisting of signal processing software, image processing software and interface/control software that creates an image of a scene in order to assist pilot aviation operations; aerospace push-button switches and indicators; integrated panels providing multiple switching functions; light emitting diode (LED) displays for avionics; night vision filters [ ; defense equipment, namely, scuba diver recall signal devices; surface-to-submarine signaling devices ];Color is not claimed as a feature of the mark.;
 

Where the owner name is not linked, that owner no longer owns the brand

   
Technical Examples
  1. Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system can further include a movable control surface coupled to the fuselage and extending generally in a horizontal plane. The control surface can be movable to a deflected position in which the control surface can be positioned to create a flow pattern proximate to the fuselage when the aerospace vehicle is located in a flow field. The flow pattern can be positioned to create a pressure differential between the first portion of the fuselage and the second portion of the fuselage. The first and second portions can be located so that the pressure differential produces a yawing moment on the aerospace vehicle.