None.
(1) Field of the Invention
The present invention relates to a water propulsion apparatus, and more particularly to a two phase water jet propulsion apparatus.
(2) Description of the Prior Art
In a typical water propulsion system, the system employs a pump connected to a nozzle. The pump, usually a high speed centrifugal water pump, is driven by an engine such as a two stroke gasoline engine, four stroke gasoline engine, or a diesel engine. The system produces thrust by first increasing velocity of the water flow, and subsequently expanding the water flow.
The engine used to pump the water in the water propulsion system generates exhaust gas and sound waves. The exhaust and sound waves are directed away from the engine compartment by an exhaust system or passageway that is connected to an exhaust port of the engine. The exhaust system is then either extended to open into the water or into the air/atmosphere. In the exhaust systems where the exhaust gas is discharged into the atmosphere, the exhaust noise creates a problem.
In the propulsion systems where the exhaust is introduced into the water, the exhaust is introduced in a low-pressure region or after the water begins to expand. While introducing the exhaust gas into the low-pressure region (after the water has expanded) reduces the sounds waves (noise level), this does not increase the efficiency of the water propulsion system or increase thrust of the water propulsion system.
Accordingly, a need exists for a water propulsion apparatus that reduces the noise level generated by the engine. The apparatus should also increase the thrust produced by the propulsion apparatus. Moreover, the apparatus should increase the overall efficiency of the propulsion apparatus.
A water propulsion apparatus is disclosed which includes a nozzle and a passageway communicating with an exhaust gas source. The nozzle includes a first region that increases the water flow velocity and a second region that subsequently expands the water, thereby producing a thrust. The passageway is connected to the nozzle at a point in the first nozzle region while the water flow velocity is being increased and prior to the second nozzle region wherein the water being expanded. In a preferred embodiment, the exhaust gas source is an engine. The engine can be a diesel engine, a gasoline engine, or a hot gas piston expander.
In a further embodiment, the present invention includes a method of increasing the thrust of a water propulsion apparatus. The method includes the steps of providing an engine that produces an exhaust gas, providing a nozzle having a first region which increases the water flow velocity and a second region which subsequently expands the water, and introducing the exhaust gas at a point in the first nozzle region while the water flow velocity is being increased and prior to the second nozzle region wherein the water is being expanded.
These and other features and advantages of the present invention will be better understood in view of the following description of the invention taken together with the drawing wherein:
Referring now to
The engine 12 drives a pump 16, typically a high-speed centrifugal pump, via a drive means 17 (such as, but not limited to, a drive shaft, transmission, drive belt, etc.) that displaces water through a water intake 18 from a water source (not shown), through the pump 16, and into the nozzle 14. As the speed of the pump 16 is increased, the amount of water displaced, the mass flow rate “M”, is increased. For a given pump speed, the pump 16 will substantially have a constant mass flow rate M.
The nozzle 14 is fluidly connected to the pump 16, and can be any nozzle known to those skilled in the art. In general, the nozzle 14 is a converging passageway wherein the nozzle diameter at region R1 is larger than the nozzle diameter at region R2. For a given mass flow rate M, the decrease in the diameter from R1 to R2 increases a velocity “V” of the water, and consequently increases the momentum of the water. As the accelerated water exits the nozzle 14 at a nozzle outlet 20, the increased momentum translates into thrust. The thrust produced by the nozzle 14 is approximated by the difference in the momentum of the water jet:
Thrust=MVJet−MV (1)
where M is the mass flow rate through the system, V is the velocity of the vehicle, and VJet is the velocity at the nozzle which is nominally:
V
Jet=(2(PPump−POcean)/ρOcean)1/2 (2)
where PPump is pressure of the pump, POcean is the pressure of the ocean, and ρOcean is the density of the water. This principle is well understood and known by those skilled in the art.
A result of decreasing the diameter of the passageway, and consequently increasing the water velocity, is that the pressure within the nozzle 14 at region R1 is greater than the pressure at region R2. This effect is reflected by Bernoulli's Equation.
In the past, most engines operate efficiently at lower exhaust back-pressures. Exhaust back-pressure is a measurement of the resistance to the flow of exhaust encountered by the engine. By and large, as engine exhaust back-pressure increases, the engine 12 requires more power to remove the exhaust gasses 15 from a combustion chamber of the engine, thus reducing the performance and efficiency. New engine designs, however, actually operate more efficiently at higher Net Mean Effective Pressure (NMEP). NMEP can be derived/defined from an expander's or engine's net power, shaft speed, and volume displaced, and is approximated by:
The variable “RPC” (output shaft revolutions per cycle) is one for hot gas piston expanders, one for a two stroke internal combustion engine, and two for a four stroke internal combustion engine. Table 1 summarizes the maximum power for several engines.
A gas passageway 22, according to the present invention, is connected to the nozzle 14 at a region R3 where the velocity of the water flow is being increased, yet prior to the water being expanded. This region R3 is in a high-pressure region of the nozzle 14. The resulting thrust can be approximated by:
Thrust=(M+MExhaust)VN−MV (4)
where:
V
N=(2(PPump−POcean)/ρMixture)1/2 (5)
This results in the exhaust 15 being mixed with water in the nozzle 14. Consequently, the density, ρMixture, is decreased, the total mass flow rate, (M+MExhaust), is increased, and the thrust is increased. When the water propulsion apparatus 10 is used in combination with the engine (gas source) 12 which operates most efficiently at an increased NMEP, the result is a water propulsion apparatus having increased thrust, increased efficiency, and decreased noise levels.
The water propulsion apparatus 10 may be used in on personal watercraft (or “Jet Ski”) or high speed underwater vehicles (such as torpedoes) or high speed surface craft.
It will be understood that many additional changes in the details, materials, steps and arrangement of parts, which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefore.