B64D25/00

Systems, apparatus, and methods for detecting an environmental anomaly and initiating an enhanced automatic response using elements of a wireless node network and using sensor data from ID nodes associated with packages and environmental threshold conditions per package

An improved system detects an environmental anomaly in a shipping container and initiates a mediation response through a generated layered alert notification. The system includes sensor-based ID nodes associated with packages within the container, and a command node mounted to the container communicating with the ID nodes and an external transceiver on a vehicle transporting the container. The command node is programmed to detect sensor data from the ID nodes; compare the sensor data to package environmental thresholds in context data related to each ID node; detect the environmental anomaly when the comparison indicates an environmental condition for at least one package exceeds its environmental threshold; responsively generate a layered alert notification identifying a mediation recipient and mediation action, and establishing a mediation response priority based upon the comparison; and transmit the layered alert notification to the transceiver unit to initiate a mediation response related to the mediation action.

Systems and methods for internal and external monitoring for an environmental anomaly within a shipping container and reporting to an external transceiver to initiate a mediation response

Systems and methods are described for detecting and initiating a response to an environmental anomaly in a shipping container. Generally, a system includes two sets of ID nodes within and outside the container and a command node mounted to the container. The command node is specially adapted to monitor the different sets of ID nodes for unanticipated non-broadcasting according to communication profiles for respective ID nodes in each set and detect an unresponsive group of ID nodes and what set of ID nodes the unresponsive ones are in. The command node identifies the anomaly when the number of unresponsive ID nodes exceeds a threshold setting, automatically generates an alert notification on the anomaly with an alert level setting based upon whether the unresponsive ID nodes are in the first and/or second set of ID nodes, and initiates a mediation response by transmitting the notification to the transit vehicle transceiver.

Systems and methods for internal and external monitoring for an environmental anomaly within a shipping container and reporting to an external transceiver to initiate a mediation response

Systems and methods are described for detecting and initiating a response to an environmental anomaly in a shipping container. Generally, a system includes two sets of ID nodes within and outside the container and a command node mounted to the container. The command node is specially adapted to monitor the different sets of ID nodes for unanticipated non-broadcasting according to communication profiles for respective ID nodes in each set and detect an unresponsive group of ID nodes and what set of ID nodes the unresponsive ones are in. The command node identifies the anomaly when the number of unresponsive ID nodes exceeds a threshold setting, automatically generates an alert notification on the anomaly with an alert level setting based upon whether the unresponsive ID nodes are in the first and/or second set of ID nodes, and initiates a mediation response by transmitting the notification to the transit vehicle transceiver.

INFORMATION PROCESSING APPARATUS

A flight information acquisition unit repeatedly acquires the respective flight status of a plurality of drones in flight. A flight irregularity determination unit determines whether or not the drones are flying in a manner deviated from a flight plan. When a flight status of a drone indicating flight deviated from the flight plan has been acquired, a first collision specification unit specifies the drone at risk of collision with a drone having that flight status. When a flight status indicating that there is a possibility of crash for a drone has been acquired, a flight status processing unit (such as a flight irregularity determination unit) sets a higher priority for processing based on the flight status acquired from that drone than for processing based on the flight status acquired from another drone.

Emergency lighting system

An aircraft includes an aircraft cabin having a number of rows of seats, at least one aisle, and at least one exit. An emergency lighting system having a first and second lines on opposing sides of the aisle, each line comprising a non-continuous series of photoluminescent markers separated by at least a longitudinal distance in the direction of the respective line. An exit path identifier is arranged to guide passengers from the aisle to the exit. Each line comprises an alternating series of first and second markers. The first photoluminescent markers have a first length and the second markers have a second length, the first length either the same as or shorter than the second length. At least the second markers are located on or adjacent to a seat adjacent to the aisle and the first markers are arranged to block the non-exit paths.

AGRICULTURAL SUPPORT SYSTEM AND UNMANNED AERIAL VEHICLE

An agricultural support system includes an unmanned aerial vehicle including a sensor, and an agricultural machine to travel in an agricultural field. When an abnormality occurs in the unmanned aerial vehicle while the agricultural machine performs work in the agricultural field in cooperation with the unmanned aerial vehicle, the unmanned aerial vehicle or the agricultural machine performs an operation different from an operation during the work.

LIFE RAFT SYSTEM FOR AN AIRCRAFT
20210339875 · 2021-11-04 · ·

A life raft system for an aircraft, comprising a storage container; an inflatable life raft that is stored in the storage container in normal operation mode, an inflation device for inflating the inflatable life raft in an emergency mode, and a control unit for activating the inflation device in the emergency mode; wherein the control unit comprises a floatable control buoy with an activation member that is operable for activating the inflation device, wherein the floatable control buoy is provided for operation at a predetermined distance remote from an associated aircraft in an emergency mode.

Latch assembly and aircraft having same
11780553 · 2023-10-10 · ·

A latch assembly for a decompression panel in an aircraft includes a base and a swing arm hinged to the base and pivotable relative to the base about a hinge axis between a latched position and an unlatched position. A load pin fixed to the swing arm has a pin axis a fixed distance from the hinge axis. A spring secured to the base is positioned to exert a spring force against the swing arm when the swing arm pivots from the latched position to the unlatched position. A bracket securable to the decompression panel defines a slot retaining the load pin when the swing arm is in the latched position. The load pin is movable in the slot under relative motion of the bracket and the base with the swing arm in the latched position, and exits the slot when the swing arm pivots to the unlatched position.

Yaw alleviation mechanism for aircraft collision

A yaw alleviation device for an aircraft containing rotatable wing roots attached to wings. The device includes a spring configured to operatively connect to a wing; and a buckling member to operatively connect to the wing. The spring is configured to extend from an original unstrained position upon the buckling member undergoing buckling from an original unbuckled position to cause rotation of one or both wings in rotationally opposite directions. The buckling member may be positioned parallel and at an offset distance to the spring.

Yaw alleviation mechanism for aircraft collision

A yaw alleviation device for an aircraft containing rotatable wing roots attached to wings. The device includes a spring configured to operatively connect to a wing; and a buckling member to operatively connect to the wing. The spring is configured to extend from an original unstrained position upon the buckling member undergoing buckling from an original unbuckled position to cause rotation of one or both wings in rotationally opposite directions. The buckling member may be positioned parallel and at an offset distance to the spring.