A system and method directed to an inflatable aerial beam transported by aerial vehicles for dispensing, among others, power and fluids using the inflatable aerial beam that may be mounted between two or more aerial vehicles. The beam, may become rigid when inflated or flexible when deflated. The beams may be coupled to one or more aerial vehicles via a pivotable joint or a flexible juncture to maintain flexibility of movement of the aerial beams. The beams may include a fluid dispenser that distributes fluid to spray nozzles to dispense fluids from the inflatable beam. The fluid, chemicals, and/or power may be obtained from a remote fixed or mobile source, one or more aerial vehicles, and other types of aerial vehicles. The aerial vehicles may be controlled remotely from a fixed location or from a movable remote-control source and may include sensors for navigation and for controlling the dispensing of the fluid or power.

A first drone equipped with a high energy Directional Ultrasound Parametric Speaker Array and a second drone equipped with an Acoustic Dispersion Cannon are used to fight wildfire. The first drone is distanced far from a burning flame but in close proximity to a fire target. Both drones are guided by GPS to communicate with remote operators. Once the target is locked, the first drone blasts the target with Amplitude Modulated Ultrasound. The Ultrasound is self-demodulated into a lower frequency audio sound when it encounters a hot flame of richly charged ions. The lowered frequency sound pushes and pulls the flame forward and backward rapidly away from the combustion source, causing it to be disconnected from the flame which instantly cools down and is extinguished. The second drone blasts the combustible source with powerful sonic shockwaves to disperse the still hot particulates further apart to prevent the source being reignited.

An unmanned aerial vehicle having a fuselage, a water collection and emission equipment, wings, linear reinforcements, a landing gear and a vertical fin. The water collection and emission equipment has buoyancy units, a sealed cabin, a water pump and a water collection and emission pipe. The sealed cabin is detachably connected to the fuselage, and a compartment is arranged in the sealed cabin. The water pump is arranged in the compartment and the side wall of the sealed cabin has at least one concave part which is concave towards the direction of the inner cavity used for slowing down the swaying of water.

A hydraulically propelled drone is provided for delivering firefighting fluid to an elevated location. The drone comprises a housing having a primary inlet configured to receive the distal end of a fire hose, a primary outlet configured to receive the inlet end of a primary nozzle, a central passageway configured to conduct fluid from the primary inlet to the primary outlet, and at least one secondary outlet communicating with the central passageway. At least one lift nozzle communicates with the secondary outlet and is configured to direct fluid in a generally downward direction so as to produce an upward thrust on the drone housing, and at least one valve is contained within the housing and configured to control the flow of said fluid through the primary nozzle and the at least one lift nozzle nozzle.

The disclosure is directed to systems and methods for autonomously picking up water in support of fire fighting missions using aerial vehicles. More particularly, the disclosure is directed to systems and methods for picking up water in support of fire fighting missions using onboard sensing and decision making processes with application of the fire retardant using unmanned aerial vehicles.

A service system and method using flying service equipment are disclosed. In the service system, flying service equipment such as a drone can be remotely piloted by an operator to perform activities such as installing, configuring, and testing distributed devices such as fire detection devices in a fire alarm system. The service system performs these activities upon distributed devices of a building management system. For this purpose, the service system includes a drone, and a service payload carried by the drone for performing the activities on the distributed devices.

An unmanned aerial vehicle (UAV) can be configured for fire suppression and ignition. In some examples, the UAV includes an aerial propulsion system, an ignition system, and a control system. The ignition system includes a container of delayed-ignition balls and a dropper configured, by virtue of one or more motors, to actuate and drop the delayed-ignition balls. The control system is configured to cause the UAV to fly to a site of a prescribed burn and, while flying over the site of the prescribed burn, actuate one or more of the delayed-ignition balls. After actuating the one or more delayed-ignition balls, the UAV drops the actuated one or more delayed-ignition balls from the UAV onto the site of the prescribed burn.

Technologies and implementations for using unmanned aerial vehicles in emergency applications.

Fire fighting drone comprising an exoskeleton defining an internal space extending along an axis H and a flexible bag stably housed in the internal space, provided with a release valve and configured to contain a fire fighting liquid; a support structure provided with a plurality of thrusters adapted to perform a thrust that enables the support structure to be supported in flight; the support structure is connected to a first end portion of the exoskeleton; a plurality of movable directional wings carried by the exoskeleton, extending outwards from the exoskeleton itself and angularly movable relative to the exoskeleton around respective axes H transverse to the axis H; an electronic control unit adapted to control the thruster, to generate the release signal and adapted to control the actuators that perform the rotation of the wings; the electronic control unit is configured to control said wings to allow the rotation of the wings during the free-fall phase of said drone which is released from an aircraft and thereby performs a certain trajectory of said drone from the aircraft to a launch zone; the electronic unit is configured to enable the discharge of said liquid from said bag and the activation of the thrusters following the discharge of the liquid to enable the flight of the support structure and of the exoskeleton containing the empty bag to a landing zone.

A fire extinguishing or fire prevention device comprises an extinguishing agent conduit arrangement. The extinguishing agent conduit arrangement comprises a plurality of longitudinal conduit elements each adapted to conduct a fire extinguishing agent therethrough, and a plurality of transverse conduit elements each adapted to conduct a fire extinguishing agent therethrough. Each of the longitudinal conduit elements is connected to one of the transverse conduit elements by at least one connecting element, the connecting elements each being suitable for further conducting the fire extinguishing agent from a longitudinal conduit element into a transverse conduit element or from a transverse conduit element into a longitudinal conduit element. Further, the fire extinguishing or fire prevention device comprises at least one extinguishing agent supply line; which is arranged at the extinguishing agent conduit arrangement and adapted to provide the fire extinguishing agent into at least one of the longitudinal conduit elements or the transverse conduit elements. Further, the fire extinguishing or fire prevention device comprises a plurality of outlets disposed on the extinguishing agent conduit arrangement and adapted to discharge the fire extinguishing agent from the extinguishing agent conduit arrangement. At least one flight-capable carrier device is disposed on the extinguishing agent conduit arrangement and adapted to lift and at least temporarily keep the extinguishing agent conduit arrangement with the outlets and at least a part of the fire extinguishing agent supply line in a distance from the ground surface. The extinguishing agent supply line of the fire extinguishing or fire prevention device is connected to an extinguishing agent reservoir adapted to provide the fire extinguishing agent to the extinguishing agent conduit arrangement while the extinguishing agent conduit arrangement is lifted or kept by the at least one flight-capable carrier device.