1. Field of the Invention
The present invention relates to heat engines, and particularly to a fluid expansion engine that converts heat-driven expansion of a liquid without phase change into mechanical or electrical power.
2. Description of the Related Art
Energy in general and electrical energy in particular are essential for human activities. This energy can be expensive due to the cost of needed fuel and the complexity of required conversion systems. In addition most power-generating systems can have adverse effect on the environment. Providing simple and cost effective methods for energy production can improve the quality of life for less fortunate people. Alternative energy production methods may also improve environmental quality, which currently is under great constraint due to high energy demand.
Thus, a fluid expansion engine solving the aforementioned problems is desired.
The fluid expansion engine uses a liquid working fluid contained by primary pressurized cylinders. A heat exchange system alternately cycles hot and cold heat exchanger medium through heat exchanger coils in the primary pressurized cylinders so that the cylinders have opposite temperatures, i.e., when one is hot, the other is cold. As a result, the liquid working fluid in the cylinders reciprocally expands and contracts. The work done by this fluid expansion engine is extracted via exchange of working fluid flow between the cylinders through a fluid motor and gearbox connected to secondary pressurized cylinders attached to the primary pressurized cylinders.
These and other features of the present invention will become readily apparent upon further review of the following specification and drawings.
Similar reference characters denote corresponding features consistently throughout the attached drawings.
The fluid expansion engine uses a liquid working fluid contained by at least one pressurized cylinder. An electric pump drives a heat exchange system in order to provide in the working fluid a four stage fluid expansion engine (FEE) PV cycle.
As shown in the schematic diagram of
Measurements of temperature and pressure may be taken at the primary pressurized vessels 10a, 10b. For example a pressure gauge 30a may be disposed at the heat exchanger inlet end of primary pressurized vessel 10a to measure pressure inside the vessel 10a. A thermometer 40a may be disposed at the heat exchanger end of the cylinder 10a to measure the temperature of the working fluid (e.g., glycerin or mercury) in the cylinder 10a. Similarly, pressure gauge 30b may be disposed at the heat exchanger inlet end of the primary pressurized vessel 10b to measure pressure inside the vessel 10b. A thermometer 40b may be disposed at the heat exchanger end of the cylinder 10b to measure the temperature of the working fluid (e.g., glycerin) in the cylinder 10b. Alternatively, as shown in
The bottom portion of the primary vessel 10a has a conduit that leads to secondary pressurized vessel 120a. Similarly, the bottom portion of the primary vessel 10b has a conduit that leads to another secondary pressurized vessel 120b. The working fluid 140a fills a bottom portion of the secondary pressurized vessel 120a, the remaining portion of the secondary pressurized vessel 120a being filled by hydraulic fluid 130a. Similarly, the working fluid 140b fills a bottom portion of the secondary pressurized vessel 120b, the remaining portion of the secondary pressurized vessel 120b being filled by hydraulic fluid 130b. A conduit 404a extending from the upper portion of the secondary pressurized vessel 120a is connected to an inlet 60a of a fluid motor 50. A conduit 404b extending from upper portion of the secondary pressurized vessel 120b is connected to another outlet 60b of the fluid motor 50. The fluid motor 50 is connected to a gearbox 90 to extract work done by the FEE 400, wherein alternate cyclic expansion/contraction of the working fluid contained by the liquid-containing primary pressurized vessels 10a and 10b causes the working fluid to flow in alternate directions in the lower chambers of the secondary pressurized vessels 120a, 120b, inducing the hydraulic fluid in the upper chambers to flow through the hydraulic pump first in one direction, then in the opposite direction, fluid motor 50 bring coupled to the gearbox 90 to convert rotation of the fluid motor's shaft to useful work. It will be understood that the gearbox 90 may convert the alternate clockwise and counterclockwise rotation of the fluid motor's shaft into unidirectional rotation, either to perform mechanical work or to rotate a generator shaft to generate electricity.
With respect to the heat exchange circuitry (also shown in the schematic diagram of
A heat exchange conduit 408a extends from the bottom heat exchange outlet 20b and is connected to a first port of another four-way valve 80a. Heat exchange conduit 408b extends from a second port of the four way valve 80a and connects to bottom heat exchange outlet 20d of primary pressurized vessel 10b. The input of the electric water pump 110b is connected via a conduit extending from the cold reservoir 70b to a third port of the four-way valve 80a. Conduit 409 connects a fourth port of the four-way valve 80a to an inlet of the hot reservoir 70a.
where V is the volume of the material,
is the rate of change of that volume with temperature, and αV is the volumetric thermal expansion coefficient (constant); and
where Equation (2) expresses the Bulk modulus, P is the pressure, V is the volume, dP/dV denotes the derivative of pressure with respect to volume, and K is a constant. From Equations (1) and (2), the change of pressure with respect to temperature T at constant volume can be derived as follows:
ΔP=αVKΔT. (3)
The heat capacity is defined by:
where Q is the amount of heat and ΔT is the change in temperature.
In step 200a, as the temperature increases from T1 to T2 the pressure will increase from P1 to P2 with a constant volume, as described by Equation (3).
In step 200b, when the pressure within the fluid becomes larger than Pe (at T2), the volume starts to increase while the pressure remains constant, as described by Equation (2).
In step 200c, after approaching the maximum temperature available (T3), the system temperature is reduced. At this stage the fluid pressure starts to decrease at constant volume if the weight replaced on the piston is fixed in position.
In step 200d, when the fluid pressure becomes less than the initial pressure Pe, the fluid volume will contract, moving the piston downward until it reaches its initial volume (V1) at the initial temperature (T1).
Based on the FEE cycle 100, a prototype system has been developed and tested. The environmental setup 300 presented in
The system is operated by raising the temperature of the working fluid in one of the cylinders while reducing the temperature of the working fluid in the other cylinder. This can be done by pumping hot water to the heat exchanger coil in one of the cylinders while pumping cold water to the heat exchanger coil in the other cylinder.
In comparing operation of the system to the FEE cycle, it should be understood that in a first stage, as the temperature rises in cylinder 10a, pressure builds up, generating a force that pushes the fluid through the fluid motor 50. At the same time, reducing the temperature in the cylinder 10b generates negative pressure, which pulls the working fluid from the fluid motor 50 (step 1 in the FEE cycle). In a second stage, when the combined pushing and pulling forces of cylinder 10a and 10b exceed the friction force of the fluid motor 50, the fluid flow causes the fluid motor 50 to rotate (step 2 in the FEE cycle). Each cubic centimeter of liquid passing through the fluid motor 50 generates one revolution of the fluid motor's shaft. In a third stage, when the temperature of the working fluid reaches the temperature of the reservoir, the process will be reversed. At this stage the pressure in cylinder 10a reduces from a positive value to a negative value as the temperature decreases, and the opposite occurs in cylinder 10b (step 200c in the FEE cycle). In a fourth stage, when the combined pulling and pushing forces generated by cylinders 10a and 10b exceed the friction forces of the motor, the fluid passes from cylinder 10b to cylinder 10a, causing the fluid motor 50 to rotate in the opposite direction, as occurred in step 2 (step 200d in the FEE cycle).
The system efficiency can vary significantly based on such factors as physical properties of the working liquid fluid (including an expansion coefficient that determines how much movement the system generates for each degree centigrade increase in temperature), a bulk modulus that determines how much force the system generates for each degree centigrade increase in temperature, and heat capacity, which determines how much energy is required to raise the temperature of the fluid one degree centigrade.
Physical properties of the cylinders housing the working fluids also have an effect on the system efficiency. The cylinder will expand as the working fluid expands, since its temperature will increase in the same rate. Therefore, the volumetric expansion of the cylinder has to be subtracted from the volumetric expansion of the fluid in order to get the system net expansion.
Moreover, the heat exchanger system has an effect on system efficiency. The system power will depend on how fast the energy is transferred to the working fluid (to increase its temperature) and how fast it can be drawn out of the system to cool down the working fluid.
The system efficiency (η) can be defined as the ratio between the work done by the system (Wout) to the energy put into the system (Qin):
η=Wout/Qin. (5)
The work done by the system is the force on the system (
Wout=L×F. (6)
The force is simply the mass placed on the piston (in Kilograms) multiplied by the gravitational acceleration (g=9.8 m/s):
F=m×g. (7)
The displacement L can be obtained by dividing the volumetric expansion (ΔV) by the piston area (A), in case of the example in
L=ΔV/A. (8)
The energy put into the system to perform the required work can be calculated in four stages. In stage one, the temperature increases from T1 to T2, while the pressure increases at constant volume (
F=P×A. (9)
The heat energy required for stage 1 can be calculated as follows:
E1=C×ρ×V×ΔT1 (10)
where C is the heat capacity of the working fluid (Eq. 3), ρ is density of the working fluid, V is volume of working fluid, and ΔT1=T2−T1.
In stage two the temperature increases from T2 to T3. The working fluid expands at constant pressure. The energy (E2) required at this stage can be calculated as follows:
E2=C×ρ×V×ΔT2, (11)
In this stage, the pressure of the working fluid will be reduced as the temperature drops from T3 to T4 (ΔT3) at constant volume. Equations 8, 9 and 10 can be used to calculate the energy (E3). It should be understood that the energy taken out of the system (E3) is ideally equal to the energy put into the system (E1).
Similarly, in stage 4, the temperature of the working fluid drops from T4 to T1 (ΔT4), giving up energy equal to the input energy calculated in stage 1.
The theoretical system produces work with zero energy loss, but in the practical system, as constrained by the first law of thermodynamics, only a limited amount of energy can be recovered from the system in stages 3 and 4. This can be easily determined experimentally by measuring the temperature of the heat exchange fluid supplied to the cylinders. If it is assumed that none of the input energy is recovered from the system, then the efficiency can be calculated using the following equation:
From Equations (1) and (2), the force (F) is:
F=K×αf×ΔT1×A (13)
αf=αv−αc, (14)
where αV is the working fluid volumetric thermal expansion coefficient, αc is the cylinder's volumetric thermal expansion coefficient, and αf is net volumetric thermal expansion coefficient of the working fluid.
From Equations (1), the displacement (L), which occurs at constant pressure in stage two of the cycle, during the increase of temperature from T2 to T3, can be derived as follows:
From Equations (13), (14) and (15), and taking into consideration that the system will generate work during the extraction (stage 4) equal to the work generated during stage 2 of the cycle, the efficiency equation can be rewritten as follows:
The system efficiency depends on how much heat energy can be recovered from the system for recirculation. If all the input heat energy is recovered, then the efficiency could reach 100%. However, this is impossible. On the other hand, if none of the heat energy is recovered, the efficiency can be calculated using Equation (16). The efficiency is a function of the physical properties of working fluids, in this case, glycerin and mercury (presented in Table 1), along with the temperature differential (ΔT) and system specification. Table 2 presents the efficiencies of glycerin and mercury for different ΔT. Glycerin provided slightly higher efficiency. For glycerin, the efficiency varies from 0.043 (4.3%) at 100° C. to 0.21 (21%) at 1500° C. By recovering some of the heat energy drown from the system during stages 2 and 3, and by applying high ΔT, the efficiency could be comparable to the internal combustion engine, which reaches 30%. The working liquid in the cylinders should be air-free. Any air that leaks to the cylinders will lead to a significant reduction in the system efficiency. The other factor that impacts the system efficiency is the force acting on the system (F). This should be predetermined using Equations (13) and (14) so that ΔT1=ΔT2.
It is to be understood that the present invention is not limited to the embodiments described above, but encompasses any and all embodiments within the scope of the following claims.
This application is a continuation-in-part of U.S. patent application Ser. No. 14/667,633, filed Mar. 24, 2015.
Number | Name | Date | Kind |
---|---|---|---|
1717161 | Malone | Jun 1929 | A |
4257231 | Banks | Mar 1981 | A |
4511805 | Boy-Marcotte et al. | Apr 1985 | A |
5579640 | Gray, Jr. | Dec 1996 | A |
5916140 | Hageman | Jun 1999 | A |
20060059912 | Romanelli | Mar 2006 | A1 |
20110061836 | Ingersoll et al. | Mar 2011 | A1 |
20120159942 | Klassen | Jun 2012 | A1 |
20130061590 | Iockheck | Mar 2013 | A1 |
20130152578 | Solem | Jun 2013 | A1 |
Entry |
---|
Greg Swift, Los Alamos National Laboratory, Los Alamos NM, “John Malone and Liquid Thermodynamics” retrieved from the Internet on Sep. 29, 2014. |
Number | Date | Country | |
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Parent | 14667633 | Mar 2015 | US |
Child | 14863395 | US |