Matches 1 - 16 out of 16

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US20060144997 Method and system for health monitoring of aircraft landing gear  
The invention relates to a new method and system for health monitoring of aircraft landing gear. The system includes sensors that are attached to the landing gear structure and equipment (e.g.,...
US20120119925 Illuminated Aircraft Wheel Chock Indicator  
A visual display used to indicate when aircraft wheel chocks have been inserted against the aircraft tires and the tarmac. The display is mounted on the exterior of an aircraft terminal at an...
US20130021173 User-Defined Pages for Aircraft  
A method and apparatus for displaying aircraft information. A selection of a piece of dynamic information is detected about an aircraft on a first display on a user interface. The piece of dynamic...
US20120326894 METHOD OF PROTECTING AN AIRCRAFT LANDING GEAR WHILE THE AIRCRAFT IS BEING TOWED, AND PIN FOR COUPLING A TOWING BAR TO AN ORIENTABLE LOWER PART OF A LANDING GEAR  
A method of protecting an aircraft undercarriage (1) while it is being towed by means of a tow bar (13) hitched to a steerable bottom portion of the undercarriage, the method including the step of...
US20090207047 Wireless Landing Gear Verification System  
According to one embodiment, a verification system for an aircraft includes a cockpit instrument in communication with a wireless communication circuit. The wireless communication circuit is...
US20060220918 Rotating seal for anti-stiction of hydraulic struts  
An onboard system for use in measuring, computing and displaying the weight and center-of-gravity for aircraft, while keeping aircraft movement to a minimum. Pressure sensors are mounted in...
US20090040072 AIRCRAFT STEERING ANGLE WARNING SYSTEM  
A steering angle warning system comprising a rotation-measuring unit located on an aircraft, and an alarm unit. The rotation-measuring unit is arranged to output a first signal dependent on the...
US20150145703 METHODS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM  
Methods to monitor components of an aircraft landing system are disclosed herein. An example method includes determining a brake assembly temperature and determining a wheel temperature. The...
US20070120708 METHODS AND SYSTEMS FOR MONITORING AIRCRAFT APPROACH BETWEEN APPROACH GATES  
Using signals available into an Enhanced Ground Proximity Warning System (EGPWS), approach monitor systems and methods compare approach speed, approach angle and amount of tailwind/crosswind to...
US20150002318 SYSTEM AND METHOD FOR TIRE BURST DETECTION  
Tire pressure monitoring systems and methods for detecting a tire burst are disclosed. The system may include a tire pressure sensor, a tire pressure monitor, and a tire burst indicator. The tire...
US20090091476 LOCK SENSOR FOR AN INTERNALLY LOCKING ACTUATOR  
The present invention provides a lock sensor for use in an actuator such as is used in aircraft landing gear systems. The lock sensor comprises at least one field emitting device (46) mounted on a...
US20140210647 SWITCH ASSEMBLY AND OVER-STEER DETECTION SYSTEM  
A switch assembly is disclosed having a switch with an actuator moveable from an armed position to a disarmed position. A housing is attached to the switch and contains a cam that holds the switch...
US20100114411 SYSTEM AND METHOD FOR DETERMINING AIRCRAFT HARD LANDING EVENTS FROM INERTIAL AND AIRCRAFT REFERENCE FRAME DATA  
This invention allows for the precise determination of an aircraft's landing conditions and whether an aircraft has experienced a hard landing that exceeds the allowable design loads of the...
US20100225503 SYSTEM AND METHOD FOR DETECTING A DRAGGING BRAKE  
Systems and methods to determine whether a brake is dragging based on post-takeoff spindown data are provided. The method comprises measuring spindown of a wheel to obtain spindown data. The...
US20150284108 NOSE WHEEL TIRE PRESSURE SENSING SYSTEM AND APPARATUS  
Landing gear tire pressure sensing systems, methods and apparatuses are provided. In various embodiments, a tire pressure sensing system may be mounting to a landing gear. The system may comprise...
US20120056759 SYSTEM FOR DISPLAYING MULTIPLE OVERLAID IMAGES TO A PILOT OF AN AIRCRAFT DURING FLIGHT  
A system for displaying first and second images to a pilot of an aircraft includes, but is not limited to, a sensor subsystem that detects a light transmission originating from outside the...
Matches 1 - 16 out of 16