A sealable capsule configured to contain one or more fire extinguishing materials is provided. The sealable capsule can include an upper and a lower shell, an internal bladder and a mechanism for releasing the fire extinguishing materials. The upper shell can include a valve, one or more through-holes filled and sealed with a corresponding number of plugs, and one or more rods, each extending from the plug to an internal plate of the releasing mechanism. The upper shell can be configured to contain a first fire extinguishing material, and the lower shell can include a membrane configured to contain a second fire-extinguishing material. The bladder can be coupled to the internal plate and to the upper and lower shells, such that the bladder is positioned within the capsule in a first position when the capsule is prepared for use and in a second position when the capsule has been activated.

A safety device configured to fire projectiles. The safety device includes a firing mechanism, a y-axis frame, an x-axis frame, a first control unit, a camera, and a monitoring control unit. The y-axis frame having a first actuator and the x-axis frame having a second actuator. The monitoring unit having a second control unit, wherein the second control unit is in communication with the first control unit. The safety device capturing imaging and transmitting imaging to the monitoring unit. The monitoring unit generating a display. The second control unit tracking a target on the display and calculating angle coordinates. The second control unit communicating the angle coordinates to the first control unit. The first control unit generating firing coordinates and transmitting the firing coordinates to the first actuator and the second actuator. The first actuator and the second actuator adjusting the firing mechanism position to correspond to the firing coordinates.

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.

A fire suppression device may be launched from a hand-held, stand alone, or object- or vehicle-mounted device. The fire suppression device may be propelled by a first accelerant ejected out of a proximal end of the fire suppression device. The fire suppression device may be ruptured by a second accelerant after a predetermined amount of time. A fire suppressant may be dispersed on a fire when the fire suppression device is ruptured.

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.

A control mechanism of a vehicle-mounted system for electromagnetic launch of fire extinguishing bombs for high-rise buildings is provided. A stress wave amplifier is fixedly connected to a secondary coil, a primary coil is fixedly connected to a coil base, a guide shaft passes through a central hole in the primary coil and the coil base, and a head of the guide shaft is fixedly connected to the secondary coil. A step-up transformer TM1 boosts a 380-V alternating current and changes it to direct current to charge a pulse capacitor C1 and store energy in the pulse capacitor C1. A discharge thyristor M3 is triggered, and the pulse capacitor C1 releases the energy instantaneously. A stress wave is generated between the primary coil and the secondary coil. The stress wave is transmitted to a fire extinguishing bomb through the stress wave amplifier, to launch the fire extinguishing bomb.

A control mechanism of a vehicle-mounted system for electromagnetic launch of fire extinguishing bombs for high-rise buildings is provided. A stress wave amplifier is fixedly connected to a secondary coil, a primary coil is fixedly connected to a coil base, a guide shaft passes through a central hole in the primary coil and the coil base, and a head of the guide shaft is fixedly connected to the secondary coil. A step-up transformer TM1 boosts a 380-V alternating current and changes it to direct current to charge a pulse capacitor C1 and store energy in the pulse capacitor C1. A discharge thyristor M3 is triggered, and the pulse capacitor C1 releases the energy instantaneously. A stress wave is generated between the primary coil and the secondary coil. The stress wave is transmitted to a fire extinguishing bomb through the stress wave amplifier, to launch the fire extinguishing bomb.

The present invention discloses a fire extinguishing device to reduce or extinguish a fire in a specific area through a truck. The truck will have air compressor unit to help fire extinguisher ball at the targeted area or remote location

A fire extinguishing bomb and a launching system thereof are provided. The fire extinguishing bomb includes a fire extinguishing part and a propelling part connected to each other; the propelling part includes a storage bunker filled with liquid or fire extinguishing agent; the liquid or fire extinguishing agent is driven by compressing the volume of the storage bunker or compressing the volume of the liquid or the fire extinguishing agent and thus is sprayed out of the propelling part through a spray nozzle of the storage bunker, so that the fire extinguishing bomb obtains forward propulsion. The propelling part further includes an expansion part, and the expansion part comprises a power source component and a piston. The fire extinguishing part includes a fuze. The fire extinguishing bomb is ignited in the air after falling due to gravity, which minimizes the impact and interference to unmanned aircraft vehicle.

The present invention discloses a fire extinguishing device to reduce or extinguish a fire in a specific area through a helicopter. The main structure of fire extinguisher ball plate is of steel boxes with a separator in-between. The operator will use computer monitor and cameras to import wireless cameras pictures and area temperature in helicopter before dropping fire extinguisher ball in the specific area and can drop balls after evaluating the fire volume in the area from different cells of plate