A fire extinguisher apparatus that consists on a loading lever network that gets built in the transport equipment allowing manipulation of the device that is directly introduced to the fire to compress it and by this, stopping the combustion process. Simultaneously, the said extinguishing apparatus will inject a series of substances over the flames, drastically reducing temperature of the fire zone, avoiding reignition when the device collapses on the different interventions these have.

The Main Lever of such network is originally built in to the transport equipment and one end will branch different tips which will form a net of smaller lever which will hang the TFI device. A tension cable will go across the upper part of the Main lever to bring more resistance and provide much more strength by preventing arcing of the lever when handling very heavy loads. A pipeline network that extends and is supported over and through the lever network, transports the cooling substances from the fluid deposits until the injecting sprinklers are arranged in the upper part of the attack devices.

A disposable unmanned aerial glider (UAG) with pre-determined UAG flight capabilities. The UAG comprises a flight module comprising at least one aerodynamic arrangement; and a fuselage module comprising a container configured for storing therein a payload and having structural integrity. The container is pressurized so as to maintain structural integrity thereof at least during flight, so that the UAG flight capabilities are provided only when the container is pressurized.

When distribution material is distributed over a target site on a ground surface from an aircraft, a distribution supporting apparatus offers support information to a pilot dropping the distribution material to efficiently distribute the distribution material. The distribution supporting apparatus includes: an input section to which information items on at least an aircraft velocity, an aircraft altitude, and a wind velocity are input; a computation section configured to compute a location at which the distribution material dropped from the aircraft arrives on the ground surface and a density distribution of the distribution material on the ground surface based on the information items input to the input section; and a display control section configured to display, on a display, the support information relating to the location and density distribution computed by the computation section.

Provided is a dropping-type fire extinguishing body that, in fire extinguishing using a gel-like fire extinguishing agent, can allow the fire extinguishing agent to be smoothly conveyed and dropped.

A dropping-type fire extinguishing body 1 to be dropped onto the fire site to extinguish the fire, wherein a gelling agent 3 is contained in a bag body 2 formed of a water-permeable material and water is permeated into the body and is mixed with the gelling agent to prepare a gel-like fire extinguishing agent, thereby filling the gel-like fire extinguishing agent into the inside of the bag body.

An artillery shell is fired out of a gun towards a fire. A trigger releases a fire-retarding material from the artillery shell to retard the fire.

Damage mitigating apparatus comprises in one embodiment a damage mitigating aerial vehicle that has sensors for detecting flight related characteristics and a communication unit for commanding activation of parachute deploying apparatus and of a lift generator deactivation unit following determination of a flight failure. In one embodiment, an aerial vehicle transmits a critical failure alarm signal to an unmanned aircraft traffic management system (UTM) following detection of the failure, and the UTM transmits a warning signal to neighboring aerial vehicles that are predicted to be in a vicinity of the descent path of the failed aerial vehicle to avoid collision with the failed aerial vehicle. The damage mitigating apparatus facilitates performance of a damage mitigating operation.

An expandable probe for filling a water tank in an aircraft from a body of water includes an inflatable hose having a proximal end fixed with a housing in the aircraft, a distal end fixed with a scooping head, an elastomeric internal conduit, and an inflatable bladder substantially surrounding the conduit. The conduit has a proximal end in communication with the water tank of the aircraft and a distal end fixed with a water scoop of the scooping head. An air supply is adapted to inflate and extend the inflatable hose to an extended configuration extending outside an open rear end of the housing below the lower side of the aircraft. Lowering the aircraft allows the scooping head to contact the body of water such that water enters the scoop and travels up the conduit to the water tank.

A forest fire retardant composition contains a retardant compound that includes a halide salt, a non-halide salt, a metal oxide, a metal hydroxide, or combinations thereof. The forest fire retardant composition may include at least one anhydrous salt and at least one hydrate salt. The halide salt may be magnesium chloride, calcium chloride, or both. The magnesium chloride hydrate has a formula MgCl.sub.2(H.sub.2O).sub.x, wherein x is at least one of x=1, 2, 4, 6, 8, or 12. The calcium chloride hydrate has a formula CaCl.sub.2(H.sub.2O).sub.x, wherein x is at least one of 1, 2, 4, or 6. The composition may be in the form of a dry concentrate, a liquid concentrate, or a final diluted product. The final diluted product is effective in suppressing, retarding, and controlling forest fires while exhibiting corrosion resistance and low toxicity.

Aspects of the disclosed embodiments relate to an aerial firefighting system for a helicopter, the firefighting system including: an external reservoir for storing water, wherein the reservoir includes a water outlet; a supporting frame coupled to an outer surface of the reservoir; and a moveable robotic nozzle fluidly connected to the water outlet and mounted on the supporting frame or attached to a hose reel for distributing water on a fire; wherein the moveable nozzle is operable by a user from within the helicopter to control the direction that the water is distributed.

A GPS tracking and mapping wild fire defense system network configured for defending homes and neighborhoods against threat of wild fire by proactively spraying environmentally-safe anti-fire (AF) chemical liquid on property surfaces to inhibit fire ignition and flame spread in the presence of wild fire. The GPS tracking and mapping wild fire defense system network includes: a command center in operable communication with a wireless communication network; and one or more GPS-tracked anti-fire liquid spraying systems, each having an integrated supply tank and a spray pump deployable at properties having building structures, for spraying the properties with environmentally-clean anti-fire chemical liquid using a spray nozzle assembly connected to said spray pump by way of a fluid connection. The system network further includes: a GPS system for transmitting GPS reference signals from a constellation of GPS satellites deployed in orbit around the Earth, to a GPS transceiver installed aboard each GPS-tracking anti-fire liquid spraying system, for GPS processing and GPS-coordinate location; and one or more mobile computing systems, each for use by a registered user including property parcel owners, spray contractors, and other stakeholders on the system network, to request and receive services supported by said system network. Each mobile computing system has a display screen supporting: messaging services; display of maps indicating where wild fires have been identified and mapped, tracked and ranked in terms of risk to the user and GPS-specified property; and scheduling of spray task to be performed, and recording tasks that been completed, and which are in progress, on the GPS tracking and mapping wild fire defense system network.