Patent Application
20150263354
The present invention relates to an electrochemical battery, for the propulsion of underwater craft, with a centrifugal pump regulating the incoming water flow.
There are known electric batteries for the propulsion of craft (such as torpedoes for example) operating in an underwater environment that comprise:
Batteries of the above-described type use means of controlled water admission capable of regulating the flow of water fed to the chamber as a function the external pressure acting on the craft and therefore as a function of the depth reached by the craft.
In fact, torpedoes are normally launched from submarines and this can happen at any navigation depth of the submarine. The operating depths of conventional submarines are approximately between 200 and 300 metres, while nuclear submarines can reach and go below 500 metres.
In consequence, the external water pressure can have values ranging from 1 bar to several tens of bars, while the pressure inside the chamber is initially similar to atmospheric pressure.
Without a flow-rate regulator device, the filling speed of the chamber would be highly variable, depending to the launch depth: low for launches near the surface of the sea and high at the deepest launch depths. For correct operation of the system, it is necessary that the filling speed and, in consequence, the inlet flow rate be confined between two well-defined values.
A water flow rate that is too low (for example, following a torpedo launch close to the sea surface), would slow the formation of the electrolyte and delay the availability of power from the main battery. If this delay was excessive, the start-up battery might drain before main one is ready; in this case the torpedo would cut out, be uncontrollable and not complete the mission.
A water flow rate that is very high (for example, following a launch at considerable depth) might damage the various components in the mixing chamber (electrochemical cells, gas separator, valves, etc.), with their consequent breakage. In this case as well, the torpedo's mission would not be completed.
Known type of flow-rate regulator devices carry out a check by measuring the pressure outside the craft in order to adjust the position of a moveable member that chokes the flow fed from outside the torpedo to the mixing chamber.
These flow-rate regulator devices, which envisage an electromechanical structure and an electronic control unit, are quite complex, both from the physical viewpoint and with regard to the control electronics.
In addition, flow-rate regulators are mechanically complex because they must adapt to the various launch conditions of the torpedo and must be able to support large dynamic forces during the transitory phase of water intake into the mixing chamber.
Finally, known types of flow-rate regulators also require auxiliary systems to prepare the regulator for the particular launch conditions.
Essentially, known types of flow-rate regulators are complicated, expensive and heavy, and intrinsically have a high probability of malfunction, severely reducing the reliability of the entire system to which they are applied. Failure of the regulator generally results in significantly impaired operation of the electrochemical battery, thereby making the torpedo's mission impossible.
The object of the present invention is to provide an electrochemical battery of the aforementioned type that enables achieving the controlled intake of water into the mixing chamber by means of a device already present in the electrochemical battery and intrinsically robust and efficient.
The foregoing object is achieved by the present invention in so far as it relates to an electrochemical battery for the propulsion of an underwater craft, in particular a torpedo, comprising: a main electric battery of the electrochemical type, in which a mixing chamber is configured to house an anhydrous electrolyte and is provided with an intake member for admitting a flow of water from the aquatic environment to the chamber, where the admitted water is mixed with the anhydrous electrolyte, thereby forming a liquid electrolyte; a recirculation system for the fluid electrolyte using a centrifugal electric pump and communicating with a plurality of electrochemical cells housed within the chamber (5); and an auxiliary electric battery that can be activated by remote control for powering the centrifugal electric pump, characterized in that the water intake member is configured to establish a direct connection, when open, between the exterior of the craft and the inlet of the centrifugal pump, which has an outlet communicating with the mixing chamber; said centrifugal pump is dimensionally configured to act as a flow limiting device when the pressure at the pump inlet is higher than the pressure at the pump outlet, thereby supplying the mixing chamber with a substantially constant flow that complies with the design limits of the electrochemical battery.
Advantageously, the electric pump is of the axial suction and radial delivery type, and comprises a casing that internally delimits a toroidal volute, which houses an impeller that is angularly movable about an axis under the propelling force of an electric motor; a discharge conduit runs from the volute, thereby forming the pump delivery line; at the connection zone with the volute, the exhaust conduit section has an area AREATHROAT that is sized according to the following expression:
AREATHROAT=(QMAX/QR−q)/m
where:
The invention will now be described with particular reference to the accompanying drawings, which represent a preferred embodiment, in which:
In
The electrochemical battery 1 comprises:
The electrochemical battery 1 is also provided with a recirculation system, shown schematically, in which a mode valve 101 receives the liquid coming from a phase separator 22 and, depending on the operating state of the system, can send it to a discharge device 24 or to the inlet of the pump 12 for recirculation. A thermostatic valve 23 then receives, as input, the pressurized fluid coming from the chamber 5 and the return line 100 of a heat exchanger, and is able to feed the electrochemical cells 15 with liquid electrolyte having a substantially constant temperature. The phase separator 22 (shown schematically) is designed to extract the gaseous component that forms in the liquid electrolyte during the electrochemical reaction inside the cells 15 and send it to the discharge device 24.
The structure of the electrochemical battery 1 is however of known type and will not be further described.
According to the present invention, the water intake member 8 (for example, an on-off valve positioned on the body of the torpedo) is configured to establish a direct connection, when open, between the exterior of the torpedo 2 and the inlet of the centrifugal electric pump 12), which has an outlet communicating directly with the mixing chamber; the centrifugal pump 12 is dimensionally configured to act as a flow limiting device when the pressure at the pump inlet is higher than the pressure at the pump outlet, thereby supplying the mixing chamber 5 with a substantially constant flow that complies with the design limits of the electrochemical battery 1.
In this way, an electrochemical battery 1 is produced in which the sole centrifugal pump 12 is capable of limiting the flow rate and can be used for this purpose without introducing flow-rate limiting devices of the type described according to the known art. In this way, the electrochemical battery intrinsically has a structure less subject to malfunction as, with respect to the known art, the flow-rate regulator, which is a critical component as shown above, has been eliminated. In addition, the design of the battery 1 is simplified and there is also a reduction in costs and weight.
The electric pump 12 is of the axial suction and radial delivery type, and comprises (
In particular, AREATHROAT, expressed in mm2, takes the following value (obtained experimentally):
AREATHROAT=(QMAX/Qr−q)/m (Formula 1)
where:
In detail, m is expressed by the following relation (obtained experimentally):
m=−2.00E−06*ΔP2+1.16E−04*ΔP+9.00E−04 (Formula 2)
According to one advantageous embodiment, parameter q is expressed by the following relation (obtained experimentally):
q=6.124E−04*ΔP2+4.796E−03*ΔP+1.433E+00 (Formula 3)
In Formula 1 and Formula 2, ΔP is expressed in bar.
In greater detail, it is noted that QMAX is the maximum capacity allowable in input to the electrochemical battery 1 without generating damages to the battery 1 itself. Thus, the value QMAX depends on the electrochemical battery 1 used, and may be obtained experimentally by increasing the capacity in input to the battery 1 and verifying its damaging point. The value QMAX is therefore the value immediately preceding the damaging value of the electrochemical battery 1.
When the input valve of the electrochemical battery 1 is opened, the pressure inside the battery 1 has the same order of magnitude of the atmospheric pressure, while the external pressure may be very high due to the fact that it depends on the altitude at which the electrochemical battery is in that time instant (e.g., the battery 1 is located on a torpedo); in the absence of an element which regulates the capacity at input to the electrochemical battery 1, such a condition would generate a very high flow rate, even higher than the maximum acceptable value (QMAX). According to an aspect of the present disclosure, the element which regulates the input capacity is the recirculating pump of the electrolyte, which, in the presence of an upstream pressure higher than that downstream, shows a turbine-like behavior and, correctly dimensioned, limits the maximum input capacity to values lower than QMAX. After having made these preliminary remarks, the maximum value of ΔP represents the difference between the pressure upstream of the pump, when the input valve of the battery is opened at the maximum deepness foreseen at the design stage and the pressure present downstream of the pump at the same instant. The pump may carry out a regulation of the capacity is adequately dimensioned; in particular, the present Applicant has verified that the vortex which takes place in the vicinity of the throat section self-limits the capacity as a function of the throat section area AREATHROAT if the throat area satisfies the aforementioned Formula 1. Formula 1, which links the throat area to the parameters QMAX, QR, q ed m, has been obtained and verified by the present Applicant based on theory and experimental results. Also the relations (formulae 2 and 3) which express the parameters m and q have been obtained experimentally and based on practical experiments.
By sizing the pump according to Formula 1, for the most severe operating conditions, the pump works in work zone Q1 where the curve shown has a steep slope, i.e. where change in the flow rate (X-axis) as a function of the change in pressure is negligible. In this way, the aforementioned flow-rate limiting is performed without using a flow-rate limiter.
If, following its launching, the torpedo moves to a shallower depth, the pressure difference between the inlet and outlet may drop and the duty point moves from Q1 to Q2, always in the steep-slope zone.
For example, assuming to have a nominal flow rate QR of 5.5 l/s, if it wished to limit the maximum flow rats QMAX to 20 l/s when launching the torpedo at a depth of 450 m, the throat area AREATHROAT have a value of 368 mm2; sized in this manner, the pump, for a given number of revs, will have decreasing incoming flow rates as the launch depth decreases, until a flow rate of approximately 7.5 l/s is reached at a depth of 10 m.
To conclude, it is noted that the electrochemical generator (battery) according to the present disclosure differs from the known generators for the absence of a regulation device of the input capacity to the electrochemical generator; as a fact, according to the present disclosure, the function of regulating the capacity is carried out by the pump for the recirculation of the electrolyte, which is present in the electrochemical generator itself. Such a solution guarantees a cost reduction, a weight reduction and an increase of reliability.
| Number | Date | Country | Kind |
|---|---|---|---|
| TO2014A000191 | Mar 2014 | IT | national |
