US12296207 - Suppression and isolation system

explosionsuppressioncannonpropellant
The patent describes an explosion suppression system featuring a cannon with a barrel and propellant tank, designed to utilize a suppressant cartridge that can be inserted into the barrel and activated by a trigger mechanism. This system includes explosion sensors and a lock-out mechanism to enhance safety and functionality during operation.
Claim 1
- An explosion suppression system, comprising: a cannon comprising a barrel and a propellant tank, wherein the propellant tank contains a propellant; a suppressant cartridge configured to be inserted into the barrel, wherein the suppressant cartridge comprises a first end configured to face the propellant tank, the first end defining a first plane at its ultimate extent; wherein the suppressant cartridge comprises a second end configured to face an outlet of the cannon, the second end defining a second plane at its ultimate extent; wherein no component of a detonator is positioned between the first plane and the second plane; wherein the suppressant cartridge contains a suppressant; wherein the suppressant cartridge is non-pressurized in preparation for propulsion from an outlet of the cannon; and, a trigger configured release propellant from the propellant tank into the barrel and suppressant cartridge when the trigger is triggered, thereby propelling suppressant from the outlet of the cannon. a cannon comprising a barrel and a propellant tank, wherein the propellant tank contains a propellant; wherein the propellant tank contains a propellant; a suppressant cartridge configured to be inserted into the barrel, wherein the suppressant cartridge comprises a first end configured to face the propellant tank, the first end defining a first plane at its ultimate extent; wherein the suppressant cartridge comprises a second end configured to face an outlet of the cannon, the second end defining a second plane at its ultimate extent; wherein no component of a detonator is positioned between the first plane and the second plane; wherein the suppressant cartridge contains a suppressant; wherein the suppressant cartridge is non-pressurized in preparation for propulsion from an outlet of the cannon; and, wherein the suppressant cartridge comprises a first end configured to face the propellant tank, the first end defining a first plane at its ultimate extent; wherein the suppressant cartridge comprises a second end configured to face an outlet of the cannon, the second end defining a second plane at its ultimate extent; wherein no component of a detonator is positioned between the first plane and the second plane; wherein the suppressant cartridge contains a suppressant; wherein the suppressant cartridge is non-pressurized in preparation for propulsion from an outlet of the cannon; and, a trigger configured release propellant from the propellant tank into the barrel and suppressant cartridge when the trigger is triggered, thereby propelling suppressant from the outlet of the cannon.
Google Patents
https://patents.google.com/patent/US12296207
USPTO PDF
https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/12296207