Torpedo with external combustion engine having an expansion chamber
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorAnthony W. Duva
Life of this patent
Estimating the term…
Abstract
An external combustion engine having a combustion expansion chamber. The ine includes a combustion chamber for generating a high-pressure, energized gas from a monopropellant fuel, and a cylinder for receiving the energized gas through a rotary valve to perform work on a cylinder disposed therein. A baffle plate is positioned between the combustion area and expansion area for reducing the pressure of the gas. The combustion area and expansion area are separated by a baffle plate having a flow area which is sufficiently large to eliminate the transmission of pressure pulsations from the combustion area to the expansion area while being small enough to provide for substantially complete combustion in the combustion area. The engine is particularly well suited for use in a torpedo.
Claims5
A torpedo having an external combustion expander-type engine, comprising:
- a combustion chamber for combusting a monopropellant fuel to form an energized gas;
- an expansion area for receiving energized gas from the combustion chamber and expanding the energized gas, the expansion area being separated from the combustion chamber by a baffle plate having an effective flow area which is sufficiently large to eliminate the transmission of pressure pulsations to the combustion chamber while being small enough to substantially prevent combustion in the expansion area;
- a cylinder fluidly connected to the expansion area for receiving the energized gas from the expansion area, the cylinder having a piston disposed therein, the energized gas being expanded in the cylinder to move the piston;
- a drive shaft driven by the piston;
- an exhaust passage formed in the drive shaft for removing spent gas from the engine;
- and
- a rotary valve for transferring the energized gas from the expansion area to the cylinder and for transferring the expanded gas from the cylinder to the exhaust passage.
A method for improving the combustion efficiency of an external combustion expander-type torpedo engine comprising a combustion chamber for combusting a monopropellant fuel to form an energized gas, a cylinder for receiving the energized gas, the cylinder having a piston disposed therein, the energized gas being expanded in the cylinder to move the piston, a drive shaft driven by the piston, an exhaust passage operatively cooperating with the reverse stroke of the piston for expelling expanded gas from the engine, and a rotary valve for transferring energized gas into and out of the cylinder, the method comprising:
- transferring the energized gas from the combustion chamber through a perforated baffle plate and into an expansion area in order to reduce the pressure of the energized gas from a monopropellant combustion pressure to a lower pressure, wherein the perforated baffle plate provides for an effective flow area which is sufficiently large to eliminate the transmission of pressure pulsations to the combustion chamber, while being small enough to substantially prevent uncombusted monopropellant from being carried into the expansion area.
A method for reducing the noise generated by an external combustion expander-type torpedo engine comprising a rotatable combustion chamber for combusting a monopropellant fuel to form an energized gas, a cylinder for receiving the energized gas, the cylinder having a piston disposed therein, the energized gas being expanded in the cylinder to move the piston, a drive shaft driven by the piston, an exhaust passage operatively cooperating with the reverse stroke of the piston to expel expanded gas from the engine, and a rotary valve for transferring energized gas into and out of the cylinder, the method comprising:
- transferring the energized gas from the combustion chamber through a perforated baffle plate and into an expansion area in order to reduce the pressure of the energized gas from a monopropellant combustion pressure to a lower pressure, wherein the perforated baffle plate provides for an effective flow area which is sufficiently large to eliminate the transmission of pressure pulsations to the combustion chamber, while being small enough to substantially prevent uncombusted monopropellant from being carried into the expansion area.
Dependencies are inferred from the claim text.