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34 results about "Hazard zone" patented technology

Dynamic wake prediction and visualization with uncertainty analysis

A dynamic wake avoidance system utilizes aircraft and atmospheric parameters readily available in flight to model and predict airborne wake vortices in real time. A novel combination of algorithms allows for a relatively simple yet robust wake model to be constructed based on information extracted from a broadcast. The system predicts the location and movement of the wake based on the nominal wake model and correspondingly performs an uncertainty analysis on the wake model to determine a wake hazard zone (no fly zone), which comprises a plurality of “wake planes,” each moving independently from another. The system selectively adjusts dimensions of each wake plane to minimize spatial and temporal uncertainty, thereby ensuring that the actual wake is within the wake hazard zone. The predicted wake hazard zone is communicated in real time directly to a user via a realistic visual representation. In an example, the wake hazard zone is visualized on a 3-D flight deck display to enable a pilot to visualize or “see” a neighboring aircraft as well as its wake. The system substantially enhances the pilot's situational awareness and allows for a further safe decrease in spacing, which could alleviate airport and airspace congestion.
Owner:NAT AERONAUTICS & SPACE ADMINISTATION THE UNITED STATES GOVERNMENT AS REPRESENTED BY THE ADMINISTATION OF THE THE

RS-485 isolation circuit and safety barrier

The invention discloses an RS-485 isolation circuit and a safety barrier. The RS-485 isolation circuit comprises a danger zone signal conversion module, a safety zone signal conversion module, a firstisolator and a second isolator, wherein field equipment sends a first differential signal to control equipment, and the danger zone signal conversion module converts the first differential signal into a first digital signal; the first digital signal is sent to the safety zone signal conversion module through the first isolator; the safety zone signal conversion module restores the first digital signal into a first differential signal; the control equipment sends a second differential signal to the field equipment, and the safety zone signal conversion module converts the second differential signal into a second digital signal; the second digital signal is sent to the danger zone signal conversion module through the second isolator; and the danger zone signal conversion module restores thesecond digital signal into a second differential signal. The circuit can realize two-way communication between the field equipment and the control equipment, and intrinsic safety protection is added,so that intrinsic safety requirements in an industrial field environment can be met.
Owner:ZHEJIANG SUPCON TECH +1

A method and system for identifying and generating operation path of aircraft idling deicing danger zone

ActiveCN114506458BImprove the ability of absolute safety operationImprove fluencyDe-icing equipmentsICT adaptationAir velocityDirection information
The invention belongs to the technical field of aircraft deicing operation route generation, and discloses a method and system for identifying a danger zone of aircraft idling deicing and generating an operation route. Establish the boundary curve function of the idling deicing danger zone of the current flight under no wind conditions according to the flight data such as the aircraft type information and the thrust direction information of the left and right engines. The movement paths of the intake and exhaust airflows are used to calculate the boundary curve function of the danger zone. According to the calculation results, the idling deicing danger zone of the aircraft under the influence of wind is demarcated; the internal and external safety passages of the engine are established and the deicing operation path is generated. The present invention describes the boundary functions of the idling deicing danger zone such as the aircraft air inlet, exhaust port, and engine reverse thrust, adds external influences such as wind speed and wind power, and adjusts the scope of the danger zone of the intake port and the exhaust port in combination with the boundary function. The accuracy of idle deicing operation is improved.
Owner:CIVIL AVIATION UNIV OF CHINA

Surrounding monitoring device for working machines

The present invention provides a peripheral monitoring device for a working machine, comprising: an obstacle detection unit (400) for detecting the existence of an obstacle around the working machine using an image captured by a camera (13); A position calculation unit (500) that calculates the position of the obstacle based on the working machine; a dangerous area calculation unit (700) that calculates a dangerous area based on the posture and motion of the work machine; a judgment unit (800) that determines whether there is an obstacle within the calculated dangerous area ); a risk level setting unit (2000) for setting the contact risk level with respect to obstacles within the danger range; an image generation unit (600), which converts the camera image into a top view image centered on the work machine, and converts it from the The risk level setting unit looks down on the overhead view image above the obstacle for which the highest contact risk level is set, thereby creating an image including the work machine and the entire danger area on the overhead view image; and creating the The display device (1300) for displaying the image. Thereby, since the operator can instantly grasp the position of the most dangerous obstacle with respect to the work machine, the work efficiency by the work machine can be improved.
Owner:NIHON KENKI CO LTD
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