Abstract: The invention discloses a system and method of displaying UAS traffic in the cockpits of manned aircraft and also for use with other unmanned aircraft. The invention utilizes the FAA concept of remote identification for supplying the UAS data necessary to generate traffic reports. The invention discloses several different methods of communicating the UAS remote ID data to re-broadcast stations which would then re-broadcast the UAS traffic reports to receiving aircraft. The invention suggests leveraging the existing ASD-B and TIS-B FAA traffic reporting system to communicate the UAS traffic reports to the receiving aircraft.

Abstract: Processes, systems, and methods are disclosed for periodic real-time reporting, receiving and mapping of in-flight turbulence, from a reporting source to a receiving aircraft, using the existing Automatic Dependent Surveillance-Broadcast (ADS-B) messaging system. The turbulence reporting source may be a reporting aircraft or a ground station. Currently reserved ADS-B message format type codes are redefined as the turbulence message for reporting the sensed turbulence. Reception and display of the turbulence data communicated by the turbulence message may be displayed on an aircraft display system (MFD) is a variety of pilot selectable formants and overlays. Visual presentation characteristics of the reporting aircraft on the display are indicative of the sensed turbulence.

Abstract: Systems and methods are disclosed for periodic real-time reporting of in-flight turbulence experienced by aircraft using the existing Automatic Dependent Surveillance-Broadcast (ADS-B) messaging system. The invention includes both broadcast to and reception from other aircraft and ground stations using the ADS-B system. Systems and methods for displaying the received turbulence reports on a cockpit display system are also disclosed. The disclosed systems and methods accomplish the objectives of the invention on a non-interference basis with existing ADS-B system functionality by utilizing currently reserved message types and/or unused data fields for the turbulence reporting. The invention is applicable to both 1090ES and 978 UAT ADS-B systems.

Abstract: Systems and methods are disclosed for periodic real-time reporting of in-flight turbulence experienced by aircraft using the existing Automatic Dependent Surveillance-Broadcast (ADS-B) messaging system. The invention includes both broadcast to and reception from other aircraft and ground stations using the ADS-B system. Systems and methods for displaying the received turbulence reports on a cockpit display system are also disclosed. The disclosed systems and methods accomplish the objectives of the invention on a non-interference basis with existing ADS-B system functionality by utilizing currently reserved message types and/or unused data fields for the turbulence reporting. The invention is applicable to both 1090ES and 978 UAT ADS-B systems.

Abstract: Systems and methods are disclosed for periodic real-time reporting of in-flight turbulence experienced by aircraft using the existing Automatic Dependent Surveillance-Broadcast (ADS-B) messaging system. The invention includes both broadcast to and reception from other aircraft and ground stations using the ADS-B system. Systems and methods for displaying the received turbulence reports on a cockpit display system are also disclosed. The disclosed systems and methods accomplish the objectives of the invention on a non-interference basis with existing ADS-B system functionality by utilizing currently reserved message types and/or unused data fields for the turbulence reporting. The invention is applicable to both 1090ES and 978 UAT ADS-B systems.

Abstract: Systems and methods are disclosed for periodic real-time reporting of in-flight turbulence experienced by aircraft using the existing ADS-B messaging system. The invention includes both broadcast to and reception from other aircraft and ground stations using the ADS-B system. Systems and methods for displaying the received turbulence reports on a cockpit display system are also disclosed. The disclosed systems and methods accomplish the objectives of the invention on a non-interference basis with existing ADS-B system functionality by utilizing currently reserved message types and/or unused data fields for the turbulence reporting. The invention is applicable to both 1090ES and 978 UATADS-B systems.

Abstract: Wireless systems and methods are disclosed for establishing a continuous real-time data link communicating flight data of a small UAV to a first smart device over a wireless network. An airborne wireless sensor system is adapted to be removably attached to the UAV. The airborne wireless sensor system has a sensor module for sensing UAV flight data, a communication module for establishing the wireless data-link network and transmitting the sensed UAV flight data the smart device. The smart device may have a software application which permits the user to define data formats for display which may them be communicated to the airborne sensor system to use in building the data pages transmitted to the smart device. Smart devices such as smart phones, smart watches, tablet computers and the like are contemplated to be used.

Abstract: A wireless systems and methods are disclosed for establishing a continuous real-time data link communicating flight data of a small UAV to a first smart device over a wireless network. An airborne wireless sensor system is adapted to be removably attached to the UAV. The airborne wireless sensor system has a sensor module for sensing UAV flight data, a communication module for establishing the wireless data-link network and transmitting the sensed UAV flight data the smart device. The smart device may have a software application which permits the user to define data formats for display which may them be communicated to the airborne sensor system to use in building the data pages transmitted to the smart device. Smart devices such as smart phones, smart watches, tablet computers and the like are contemplated to be used.

Abstract: An apparatus and method for automatically monitoring and recording incoming and outgoing telephone call parameters and forming a call record in response thereto. The apparatus has a signal conditioning device connected to the telephone line; incoming and outgoing call decoders; line status detector device; clock; and a computation device. The incoming call record comprises the incoming call data such as caller's identity and number, the call start and end times, and the call duration, the outgoing call record comprises the outgoing call data, the call start and end times, and the call duration. The records may be printed immediately as the call is concluded or stored an printed later by account number.

Abstract: An apparatus and method for automatically monitoring and recording incoming and outgoing telephone call parameters and forming a call record in response thereto. The apparatus has signal conditioning means connected to the telephone line; incoming and outgoing call decoder means; line status detector means; clock means; and a computation means. The incoming call record comprises the incoming call data such as caller's identity and number, the call start and end times, and the call duration, the outgoing call record comprises the outgoing call data, the call start and end times, and the call duration. The records may be printed immediately as the call is concluded or stored an printed later by account number.

Abstract: An apparatus and method for automatically and independently determining aircraft altitude and alerting the pilot to deviations from a target altitude exceeding a specified tolerance. The alerter comprises an altitude sensing means for sensing the present altitude of the aircraft. The invention discloses three sources for altitude information namely, a self-contined sensor such as a pressure transducer, a Global Positioning System receive, or an altitude encoder. A target entry means is used for entering the target altitude. An indicating means signals an altitude alerting condition upon the detection of a condition wherein the absolute difference is larger than the tolerance value. The altitude alerting apparatus may also comprise a display means for display of the present aircraft altitude information.

Abstract: An apparatus and method for automatically monitoring and recording incoming and outgoing telephone call parameters and forming a call record in response thereto. The apparatus has a signal conditioning device connected to the telephone line; incoming and outgoing call decoders; line status detector device; clock; and a computation device. The incoming call record comprises the incoming call data such as caller's identity and number, the call start and end times, and the call duration, the outgoing call record comprises the outgoing call data, the call start and end times, and the call duration. The records may be printed immediately as the call is concluded or stored an printed later by account number.

Abstract: An apparatus and method for automatically and independently determining aircraft altitude and alerting the pilot to deviations from a target altitude exceeding a specified tolerance. The alerter comprises an altitude sensing means for sensing the present altitude of the aircraft. The invention discloses three sources for altitude information namely, a self-contined sensor such as a pressure transducer, a Global Positioning System receive, or an altitude encoder. A target entry means is used for entering the target altitude. An indicating means signals an altitude alerting condition upon the detection of a condition wherein the absolute difference is larger than the tolerance value. The altitude alerting apparatus may also comprise a display means for display of the present aircraft altitude information.