| Patent application number | Description | Published |
|---|
| 20090177343 | SYSTEM AND METHOD FOR SELECTABLE WEATHER OBJECT DISPLAY - Systems and methods for presenting information pertaining to a weather object on a display. A process includes displaying on the aircraft display terrain information, weather reflectivity information, and at least one hazardous weather icon corresponding to the weather, wherein the hazardous weather icon indicates a determined hazard level associated with the weather; receiving a selection to display only the hazardous weather icon; and in response to receiving the selection, continuing display of the hazardous weather icon and suppressing display of the terrain information and the weather reflectivity information. | 07-09-2009 |
| 20100019938 | SYSTEMS AND METHODS FOR RE-TRIGGERING OF A RADAR WEATHER DISPLAY - After deactivation of the presentation of weather information on a radar weather display, systems and methods re-trigger when weather conditions change so that the crew is advised of the changed weather conditions. An exemplary embodiment monitors at least one condition of the weather and in response to the monitored weather condition meeting a re-triggering criteria, presents an advisory to a crew member of the aircraft indicating at least presence of the weather. | 01-28-2010 |
| 20100019958 | SYSTEMS AND METHODS FOR LOCATION-BASED DISCRIMINATION OF TURBULENCE - Systems and methods differentiate weather, such as storm cells and/or turbulence regions, based on location relative to a planned flight path of an aircraft. An exemplary embodiment compares a location of the weather with a location of a region of space corresponding to the planned flight path of the aircraft. In response to the location of the weather region being outside of the region of space, an icon is presented on a display corresponding to the weather using a first icon format. In response to location of the weather being within the region of space, the icon corresponding to the weather is presented on the display using a second icon format, the second icon format different from the first icon format. | 01-28-2010 |
| 20100085254 | SYSTEMS AND METHODS FOR COMMUNICATION TO A GIMBAL MOUNTED DEVICE - A system and method wirelessly communicates signals between a device on a gimbal and a stationary transceiver. An exemplary system has a gimbal with a moveable portion, a device affixed to the moveable portion, a gimbal transceiver coupled to the moveable portion, and a stationary transceiver, wherein the gimbal transceiver and the stationary transceiver are configured to communicate with each other using a wireless signal. | 04-08-2010 |
| 20100092179 | SYSTEMS AND METHODS FOR GIMBAL MOUNTED OPTICAL COMMUNICATION DEVICE - Optical communication systems and methods are operable to communicate optical signals across a gimbal system. An exemplary embodiment has a first optical rotary joint with a rotor and a stator, a second optical rotary joint with a rotor and a stator, and an optical connector coupled to the stators of the first and the second optical rotary joints. The stator of the first optical rotary joint is affixed to a first rotational member of the gimbal system. The stator of the second optical rotary joint is affixed to a second rotational member of the gimbal system. A first optical connection coupled to the rotor of the first optical rotary joint and a second optical connection coupled to the rotor of the second optical rotary joint remain substantially stationary as the gimbal system orients an optical communication device in a desired position. | 04-15-2010 |
| 20100101341 | SYSTEMS AND METHODS FOR POWERING A GIMBAL MOUNTED DEVICE - Gimbal power systems and methods are operable to provide power to a device attached to the gimbal. An exemplary embodiment is configured to rotate a rotational member of the gimbal system about an axis, wherein a stator of a rotary power transformer affixed to the rotational member rotates about the axis, and wherein an end of an electrical connection coupled to a power connector of a rotor winding of the rotary power transformer remains substantially stationary as the stator of the rotary power transformer rotates about the axis. | 04-29-2010 |
| 20100188280 | SYSTEMS AND METHODS FOR DETERMINING LOCATION OF AN AIRBORNE VEHICLE USING RADAR IMAGES - Location systems and methods are operable to determine a location of an airborne vehicle. An exemplary embodiment identifies at least one object in a pre-captured image stored in an onboard memory and defined by a known location, identifies at least one ground object in a current radar image, correlates the ground object identified in the current radar image with the object identified in the pre-captured image, determines relative location between the installation vehicle and the identified object in the pre-captured image, and determines the location of the installation vehicle based upon the known location of the identified object in the pre-captured image and the determined relative location. | 07-29-2010 |
| 20100245165 | SYSTEMS AND METHODS FOR ASSESSING WEATHER IN PROXIMITY TO AN AIRBORNE AIRCRAFT - Dynamic weather model systems and methods are operable to assess weather in proximity to an airborne aircraft. An exemplary embodiment receives a radar return from the weather, determines reflectivity information from the received radar return, retrieves a weather model from a weather model data base, compares the weather with the retrieved weather model and the determined reflectivity information, predicts a characteristic of the weather based upon the comparison of the weather and the weather model, and determines if the predicted characteristic is potentially hazardous to the airborne aircraft. The weather model is defined by at least one weather modeling algorithm, and is defined by at least one of a parameter and a variable parameter range residing in a weather characteristics database. | 09-30-2010 |
| 20100302093 | SYSTEMS AND METHODS FOR AIRCRAFT TO AIRCRAFT EXCHANGE OF RADAR INFORMATION OVER LOW BANDWIDTH COMMUNICATION CHANNELS - Systems and methods communicate weather information between aircraft using low bandwidth communication transceivers. An exemplary embodiment receives weather information from a weather radar system on board a remote aircraft, processes the received weather information into weather radar image information that is displayable on at least a display, processes the weather radar image information into a reduced size dataset, and communicates the reduced size dataset to an installation aircraft over the low bandwidth communication channel, wherein the low bandwidth communication channel is generated by a low bandwidth communication transceiver on board the remote aircraft. | 12-02-2010 |
| 20100302094 | SYSTEMS AND METHODS FOR USING NEXRAD INFORMATION TO VERIFY WEATHER RADAR INFORMATION - Systems and methods distinguish weather radar returns from terrain radar returns. An exemplary embodiment receives a radar return from a weather radar system on board an installation vehicle, receives ground-based weather radar information, compares a location of the radar return received from the onboard weather radar system with a corresponding location in the received ground-based, and determines that the radar return received from the onboard weather radar system is a weather radar return when a location in the received ground-based weather radar information indicates a presence of weather at the location of the radar return. | 12-02-2010 |
