Patent ID: 8066223
Filing Date: 2011-11-29
Classification: B64D,Y10T

Abstract:
1. A system to be transported by an aircraft, the aircraft including an external wall and having a forward portion and an aft portion, the system comprising: a first pressure device configured to reduce a pressure of a fluid entering into a first portion of the first pressure device from a first pressure to exit a second portion of the first pressure device at a second pressure, the second pressure being smaller than the first pressure; a second pressure device configured to reduce a pressure of a fluid entering into a first portion of the second pressure device from a first pressure to exit a second portion of the second pressure device at a second pressure, the second pressure being smaller than the first pressure; an outlet positioned through the external wall of the aircraft; a plurality of agent tanks configured to hold a material to be released from the aircraft, the agent tanks coupled to the outlet to transfer the material to the outlet, each of the agent tanks positioned in one of a first row and a second row of the plurality of agent tanks, the first row and the second row of agent tanks extending longitudinally along a portion of the aircraft located between the forward portion and the aft portion of the aircraft; a first low pressure propellant tank and a second low pressure propellant tank configured to hold a pressurized gas, the first low pressure propellant tank and the second low pressure propellant tank positioned within the aircraft forward of the plurality of agent tanks, the first low pressure propellant tank coupled to the first row of the plurality of agent tanks to transfer the pressurized gas to the first row of agent tanks and the second low pressure propellant tank coupled to the second row of the plurality of agent tanks to transfer the pressurized gas to the second row of the agent tanks, the first low pressure propellant tank coupled to the second portion of the first pressure device and the second low pressure propellant tank coupled to the second portion of the second pressure device; a first plurality of high pressure propellant tanks configured to hold the pressurized gas, the first plurality of high pressure propellant tanks positioned within the aircraft aft of the plurality of agent tanks and coupled to the first portion of the first pressure device to transfer the pressurized gas at the first pressure to the first low pressure propellant tank at the second pressure through the first pressure device, the second pressure being sufficient to propel a portion of the material from the first row of agent tanks through the outlet; and a second plurality of high pressure propellant tanks configured to hold the pressurized gas, the second plurality of high pressure propellant tanks positioned within the aircraft aft of the plurality of agent tanks and coupled to the first portion of the second pressure device to transfer the pressurized gas at the first pressure to the second low pressure propellant tank at the second pressure through the second pressure device, the second pressure being sufficient to propel a portion of the material from the second row of agent tanks through the outlet.