# Determination of Performance Measuring Parameters of an Improved Dual Paraboloid Solar Cooker

Authors: Suhail Zaki Farooqui
Journal: International Journal of Photoenergy
 (2017)

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## Abstract

An experimental investigation into the performance evaluation of an improved dual reflector foldable paraboloid solar cooker has been reported, along with its energy and exergy analysis. The best attribute of this lightweight and low-cost solar cooker is its high performance coupled with the ease of handling. The cooker utilizes two paraboloid reflectors made out of Mylar-coated fiberglass dishes, each having a diameter of 90 cm and focal length of 105 cm. The total intercepted radiation energy is 1.08 kW under standard test conditions. Stagnation temperatures of up to 330°C and cooking temperatures of up to 290°C have been attained with load. Altogether, 9 experiments have been performed with and without load. Loaded tests have been conducted with water and vegetable oil. Results indicate an average cooking power of 485 W, peak exergy gain of 60.53 W, quality factor of 0.077, and a high product of temperature difference gap at half peak power to peak power of 4364.33 W·K. The maximum exergy output power attained was 70 W, while maximum exergy efficiency was 8–10%. All performance measuring parameters indicate that it is a high performance solar cooker for rural and urban communities and is suitable for all types of oil- and water-based cooking.


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## Body

## 1. Introduction

Development of more efficient and user friendly solar cookers is a high priority area, as cooking of food accounts for a substantially large chunk of the total fuel consumption on Earth. In case of the developing countries, this activity accounts to over one-third of the total primary fuel consumption [1, 2]. Conversion of cooking to renewables has the potential of substantially reducing the fuel bills of many energy-deficient countries of the world, as well as reducing the greenhouse gas emissions. Three broad types of solar cookers have been reported in the literature during the last over half a century. Box-type solar cookers utilizing the greenhouse effect to acquire the cooking temperatures are so far the most popular ones, due mainly to their simplicity and lower costs. However, they suffer from the main disadvantage of approaching the maximum temperatures of around 120°C. Therefore, they are suitable only for water-based low temperature cooking [3, 4]. Oil-based high temperature cooking is not possible with these cookers. Parabolic types are the second most common solar cookers. Typically, they utilize a parabolic reflector mounted near the ground, which focuses the reflected solar radiation onto a cooking pan placed at a height. Generally, these cookers acquire high cooking temperatures suitable for cooking all types of food. However, they suffer from a number of issues, including the requirement of frequent solar tracking, lack of maneuverability due to larger sizes and weights, and the splashes of oil and curry falling onto the reflector, requiring frequent cleaning and adversely affecting its reflectivity. The third main type of solar cookers are the vacuum tube-based cookers, as presented by various authors [1, 3–7]. Though these cookers acquire high temperatures and are very efficient, they are complex to operate and expensive to manufacture.Parabolic-type solar cookers have been offered in several versions by a number of authors. Typically, these cookers acquire concentration ratios of up to 50 and temperatures of up to 300°C [8]. With a spherical reflector, the first design was proposed by Stam in 1961 [2]. It was the simplest type of reflector, allowing the cooking vessel to be hung from a tripod at a suitable focal point. However, due to the spherical shape of the reflector, the focus was not very good. A parabolic reflector-type cooker named as SK-14 was invented by Dr. Dieter Seifert [9, 10]. The focus of this cooker was much better and sharper than the previous one. However, it is very sensitive to even a slight change in the position of the sun and hence it requires constant tracking. Due to its deeply curved parabolic reflectors, the focal point lies inside the dish [11, 12]. Further, due to the usage of a single large dish, it occupies more space, making it difficult to carry from one place to the other. Also, the frequent oil and curry splashes spoil the reflector surface, as the cooking utensils are placed above the parabolic reflector. Making this type of cooker requires advanced manufacturing facilities available only to large companies.The Sheffler community solar cooker was invented by Wolfgang Sheffler in 1986 [13, 14]. The Sheffler-type solar cookers utilize large flexible parabolic mirrors to concentrate the solar radiation inside a kitchen on a fixed point through a North-facing window, where high temperatures of up to 1000°C are attainable to cook all types of food. The polar directional controls of the parabolic mirrors are carried out through clockwork rotation at the rate of one revolution per day. The reflector is made to change the shape of its entire surface every few days to adapt itself to the changing declination angles of the sun. For these reasons, its design, manufacturing, and installation are complex. Further, it requires heavy and robust permanent structure for its support and installation needs shadow-free area throughout the year in the south direction. The requirement for capital investment is also high. Some authors have also evaluated the compound parabolic reflectors which do not require solar tracking for a few hours [15, 16]. However, these are not suitable for use with solar cookers due to their bulky size, complex construction, and use of large quantities of thermal fluids, causing delayed heating.In this paper, the design and working scheme of a dual reflector parabolic cooker has been described and experimentally tested with an aim to address the abovementioned deficiencies noted in this class of cookers. A lightweight cooker with two foldable fiberglass parabolic reflectors coated with Mylar sheet has been introduced. These attributes make it convenient to move the cooker from one place to the other, operate at any desired place, and easily store inside the home when not in use. A number of simple controls have been provided to change the inclination of each individual reflector, as well as the collective inclination of both the reflectors, in order to maintain the focused radiation from both the reflectors onto the cooking pan, with changing positions of the sun on the sky. Further, sufficient separation has been provided between the two reflectors to allow any oil and curry splashed from the cooking pan to fall onto the ground, rather than damaging the reflector surfaces. Support for the cooking pan has been kept separate to allow easy maneuverability of the cooker and to prevent shaking of the cooking utensils, while the reflective mirrors are adjusted.Several experiments have been conducted without load and with load of 4 kg of water, as well as vegetable oil to extract the various performance measuring parameters. The experimental results are analyzed in each case for determining the first and second figures of merit, cooking power, energy and exergy efficiencies, and the quality factor of the cooker.The first figure of meritF1 measures the optical efficiency of the cooker per unit heat loss factor. This is measured by dividing the difference of the maximum temperature attained by the unloaded bottom of the cooker with the ambient air temperature to the average solar radiation intensity during experiment. The second figure of merit F2 gives an indication of heat transfer from the absorbing base to the water inside the cooker. It is evaluated in the presence of full load, as the product of heat gained by water and F1 per unit aperture area per unit time per unit temperature. The cooking power is the heat gained by the water inside the cooker per unit time. Energy efficiency of the cooker is evaluated as the heat gained by the water inside the cooker divided by the solar radiation energy intercepted by the cooker collector during a given time. The exergy efficiency measures the potential of the cooker to extract the solar radiation energy. This is obtained by dividing the exergy output of the cooker by the exergy input. The exergy input and output are evaluated by recording the ambient air and water temperatures and solar radiation intensity after periodic intervals of time, while considering the water content, aperture area of the cooker, and the temperature of the surface of the sun, using formulas described in (4) and (5). The quality factor of the cooker is determined by dividing the peak exergy gain of the cooker with the exergy loss (the difference between exergy input and output) at that instant of time. The peak exergy gain is obtained by plotting the exergy output versus the temperature difference of water with the ambient air. The curve is fitted with a second order polynomial, and peak is determined.


## 2. The Optical Scheme of the Dual Paraboloid Reflector

A paraboloid reflector is defined to provide a sharp focus to the rays of light reflected from its surface, when the incident light consists of rays parallel to the axis of the paraboloid. If the incident light is not parallel to the axis of the paraboloid, the reflected light does not make a sharp focus at the focal point, but rather a dispersed focus at a point other than the focal point, as shown in Figure1 [17].Figure 1
Optical scheme of the light reflected from a dual paraboloid reflecting system defining a dispersed focus.Since the cooking pan has finite dimensions, the need for a sharp focus is not quite critical and the cooker can benefit even from a dispersed focus of the incident light reflected from the two paraboloids placed at a distance from each other, without much significant loss of performance. This feature enables the two paraboloids to get folded when not in use, making it handy to allow easy movement and storage of the cooker. Further, it allows the oil and curry splashes to mostly fall on the ground, rather than spoiling the central part of the reflective surface. The paraboloids used in the above scheme have a focal length of 105 cm and a radius of 45 cm. The distance between the rims of the two paraboloids is 20 cm. Therefore, the angle of incidence of the solar radiation to the axis of each paraboloid issin−155/105=31.6°. Further, the altitude angle of the two paraboloids would not, in general, be the same during operation as that of the sun at any instant of time, since the height of the cooking pan is held fixed during operation while the altitude angle of the sun changes. The cooking pan is not placed vertically above the reflectors, as shown in Figure 2. Normally, there would be a difference of nearly 10–20° between the two angles during 9:00 to 15:00 hours, depending upon the season. The total maximum cosine losses due to the difference between the angle of incidence of the solar radiation and the axes of the paraboloids are therefore ≤1−cos31.6°·cos20°=20%.Figure 2
Operational scheme of the dual paraboloid reflector to cater for the changing altitude angle of the sun.


## 3. The Dual Paraboloid Reflector Solar Cooker

The complete dual parabolic reflector solar cooker has been constructed in five pieces. Four of them are connected together to make one piece, while the fifth piece is kept separate to make the handling of the cooker easier. Two identical paraboloids made out of fiberglass having diameter of 90 cm and focal length of 105 cm each have been used. The inner surfaces of the paraboloids have been coated with highly reflective Mylar sheet. The sheet has a reflectivity of 94% and can withstand temperatures of up to 200°C [18]. Two pipe frames A and B are constructed as shown in Figure 3. Two steel pipes are bent in circles of diameter 75 cm each. Two small pieces of pipes “a1” are welded with frame A on one side, while another 17.5 cm long pipe “a2” is perpendicularly welded to them on the other side. A small rod passing through a small piece of pipe attached to an eye is welded between the small pieces of pipes, so that the pipe containing the eye can easily rotate with respect to the rod. The eye contains a threaded nut that allows a bolt to pass through. The bolt pressing against a closed ended U-channel on another frame provides a simple control for changing the orientation of the parabolic reflector, while in operation. The frame B is also similarly constructed with different distance between the pipes “b1.” Whole scheme is illustrated in Figure 3.Figure 3
Schematic diagram of the dual parabolic reflector support system with dimensions.The parabolic reflector frames A and B are then mounted on another frame through a rotational axis rod, as shown in Figure4. The rotational axis rod passes through the pipes “a2” and “b2” of frames “A” and “B” and allows both frames to rotate with respect to it. This allows both reflectors to be adjusted, such that the reflected solar radiation gets focused below the coking pan, within an area equal to the diameter of the pan.Figure 4
Schematic diagram of the frame allowing the orientation control of the parabolic reflectors along the altitude.The frame shown in Figure4 consists of a 78 cm long rectangular pipe, cross welded with another piece of 48 cm long pipe and a 22 cm long closed end U-channel. The 48 cm long pipe contains one strut with an eye hole at each end. The whole frame can rotate with respect to a rod passing through these struts. The rear end of this frame is connected to an altitude adjustment wheel, which can drive a high-pitch screw into a similarly pitched 30 cm long bolt. The next end of this bolt is connected to another frame, such that rotating the altitude adjustment wheel allows the whole frame to change its orientation with respect to the rod passing through the abovementioned two struts. This rod is welded onto the frame shown in Figure 5.Figure 5
Schematic diagram of the Y-shaped support frame, placed on a level surface.The Y-shaped frame shown in Figure5 is made out of four rectangular pipe sections. Five wheels are connected at the ends of the frame. The frame in Figure 4 is connected to this frame through the 53 cm long welded rod and a hook, as shown. This frame supports the entire structure of the cooker and can be easily moved across over a flat surface. The total weight of the entire structure with fiberglass dishes is 12 kg.The last part of the cooker is the cooking pan holder. The holder frame made out of angle iron, shown in Figure6, is 125 cm high, 60 cm long, and 37.5 cm wide and provides a structurally stable support for the cooking pan. The bottom of this frame is slipped between the two front wheels of the frame shown in Figure 5, such that any movement of the reflector frame does not cause any vibrations onto the cooking frame.Figure 6
Cooking pan holding frame.The complete dual parabolic reflector cooker in operation is shown in Figure7.Figure 7
The dual parabolic reflector solar cooker in operation.


## 4. Performance Measuring Experiments

Several experiments had been performed on carefully selected calm and clear days at 33.73° N latitude and 73.09° E longitude test location (Islamabad, Pakistan), during the months of April and May 2016, to assess the performance measuring parameters of the dual parabolic reflector solar cooker, described in the previous section. Three experiments were performed on different days without load to determine the maximum plate stagnation temperature and the first figure of meritF1. Three more experiments were performed with 4 kg of water load each, to determine the energy and exergy efficiencies of the cooker, the second figure of merit F2, cooking power, and the quality factor of the cooker. Further, three experiments were performed with cooking oil load to determine the maximum achievable temperatures with load, as shown in Table 1. The recorded data included the ambient temperature Ta, plate temperature Tp, load temperature Tl, and the solar radiation intensity Ih on the horizontal surface. The maximum available power to the cooker through two reflectors (diameter 90 cm each) under standard solar insolation conditions of 1000 W/m2, while taking into account the cosine losses, is 1.08 kW. The cooking pot had a diameter of 25 cm and could accommodate up to 7 liters of liquid load. It was surrounded from all sides with a 5 cm thick glass wool insulation. The lid at the top was also covered with a 5 cm thick layer of glass wool. The insulation-free bottom of the pot was exposed to the ambient air and was sprayed with dull black deco paint. Nine experiments had been performed with corresponding conditions as outlined in Table 1.Table 1
Test conditions of nine experiments.
Exp. number
Date of experiment
Experiment start solar time (H:M)
Experiment end solar time (H:M)
Load (gm)
Max. temp. attained (°C)
1
April 13, 2016
09:40
10:30
Nil
233
2
April 13, 2016
12:18
12:46
Nil
258
3
April 22, 2016
11:26
12:18
Nil
331
4
April 14, 2016
13:46
14:14
4000 (water)
100
5
May 02, 2016
12:16
13:04
4000 (water)
100
6
May 18, 2016
12:24
12:58
4000 (water)
100
7
April 22, 2016
12:06
12:44
850 (oil)
294
8
April 27, 2016
10:56
12:00
850 (oil)
262
9
April 29, 2016
11:04
12:00
850 (oil)
285The first set of experiments was performed without load on the cooker. The base plate temperature of the cooker, the ambient temperature, and the solar radiation intensity on a horizontal surface were measured and recorded every two minutes, while cooker tracking adjustments were performed every five minutes. Digital thermometers UT33 series, prepared by Uni-Trend Group Ltd., China, were used for temperature measurement, while Apogee SP110 pyranometer was used for the measurement of solar radiation intensity. The data plotted in Figures8, 9, and 10 indicates the stagnation temperatures attained in each case.Figure 8
Plot of temperature (blue) and solar radiation intensity (red) versus time for the first unloaded experiment. Radiation intensity is divided by 10 to fit the scale.Figure 9
Plot of temperature (blue) and solar radiation intensity (red) versus time for the second unloaded experiment. Radiation intensity is divided by 10 to fit the scale.Figure 10
Plot of temperature (blue) and solar radiation intensity (red) versus time for the third unloaded experiment. Radiation intensity is divided by 10 to fit the scale.The blue curves in Figures8, 9, and 10 show that the maximum temperatures attained during the three unloaded experiments were 233°C, 258°C, and 331°C, respectively. A comparison of these figures shows that the maximum plate temperature depends heavily on the existing intensity of the solar radiation.The second set of experiments was conducted with a load of 4 kg of water each time, on April 14, May 2, and May 18, 2016, as per the recommended test load for solar cookers per unit aperture area per unit concentration ratio [19]. As shown in Figures 11, 12, and 13, 4 kg of water load was brought to a boil in 28 minutes, 48 minutes, and 34 minutes from starting temperatures of 42°C, 39°C, and 36°C, respectively.Figure 11
Plot of temperature (blue) and solar radiation intensity (red) versus time for the first experiment with 4 kg of water load. Radiation intensity is divided by 10 to fit the scale.Figure 12
Plot of temperature (blue) and solar radiation intensity (red) versus time for the second experiment with 4 kg of water load. Radiation intensity is divided by 10 to fit the scale.Figure 13
Plot of temperature (blue) and solar radiation intensity (red) versus time for the third experiment with 4 kg of water load. Radiation intensity is divided by 10 to fit the scale.The last set of experiments was conducted with one liter (850 gm) of vegetable oil load each time, on April 22, 27, and 29, 2016. As shown in Figures14, 15, and 16, the vegetable oil attained maximum temperatures of 294°C, 262°C, and 285°C in 38 minutes, 64 minutes, and 56 minutes from starting temperatures of 101°C, 60°C, and 53°C, respectively.Figure 14
Plot of temperature (blue) and solar radiation intensity (red) versus time for the first experiment with 850 gm of vegetable oil load. Radiation intensity is divided by 10 to fit the scale.Figure 15
Plot of temperature (blue) and solar radiation intensity (red) versus time for the second experiment with 850 gm of vegetable oil load. Radiation intensity is divided by 10 to fit the scale.Figure 16
Plot of temperature (blue) and solar radiation intensity (red) versus time for the third experiment with 850 gm of vegetable oil load. Radiation intensity is divided by 10 to fit the scale.Results of three sets of three experiments each have been shown in the foregoing, with dual parabolic reflector soar cooker, during the months of April and May 2016. The experiments with no load on the cooker indicate that under clear sky conditions, maximum plate temperatures as high as 330°C may be attained in 30 to 40 minutes duration. Experiments with 4 kg of water load indicate that starting from the ambient temperatures, it boils in 28 to 48 minutes, depending upon the radiation intensity. The last set of experiments with vegetable oil load indicates the maximum attainable cooking temperatures with load. Temperatures as high as 294°C have been attained this way, with the average attained temperature of about 280°C in 53 minutes. All these results indicate that the cooker presented in this paper is most suitable for fulfilling the oil-based high-temperature cooking needs of the public, while being user friendly, lightweight, and low cost.The detailed performance measuring parameters of the cooker have been evaluated in the following sections.


## 5. Determination of the First and Second Figures of Merit

In order to test the performance of solar cookers, two figures of merit (FOM) are normally recommended. These are defined asF1 and F2 [20, 21]. F1 (measured in m2 K/W) is the ratio of optical efficiency to the heat loss factor by the bottom absorbing plate and is a measure of the differential temperature gained by it at a particular level of solar insolation. F2 gives an indication of heat transfer from the absorbing base to the water inside the cooker.Mathematically, they are defined as(1)F1=Tps−TaHs,where Tps is the plate (tray) stagnation temperature, Hs is the solar insolation on the horizontal surface, and Ta is the ambient temperature.
(2)F2=F1M·CwA·τln1−Twi−Taυ/F1·Haυ1−Twf−Taυ/F1·Haυ,where (M · C)w indicates the mass of the water in the pot multiplied to its heat capacity, A stands for the aperture area of the cooker, τ is the time difference during which water was heated from an initial temperature Twi to the final temperature Twf, Hav is the average solar radiation on a horizontal surface, and Tav is the average ambient temperature during the experiment. F1 is evaluated in the absence of any load on the solar cooker while F2 is evaluated in the presence of full load.The cooking power of a cooker can be calculated as [21]
(3)P=M·CwΔTwΔt,where ΔTw is the temperature difference of water acquired in time ∆t.For the unloaded solar cooker described in this paper, three experiments were conducted on April 13 and April 22, 2016. TheF1 calculation results are summarized in Table 2.Table 2
Calculation of the first figure of merit for the dual parabolic reflector solar cooker during experiment numbers 1, 2, and 3.
Exp. number
T
as (°C)
T
ps (°C)
H
s (W/m2)
F
1 (m2 K/W)
1
29.3
233
885
0.2302
2
30.5
258
900
0.2528
3
30.3
331
1035
0.2905For the fully loaded (4 kg of water load) cooker, data were collected on April 14, May 2, and May 18, 2016. For analysis, data are used for the water temperatures between 60 and 90°C, for each experiment. The results are summarized in Table3.Table 3
Calculation of the second figure of merit and the cooking power for the dual parabolic reflector solar cooker for experiment numbers 4, 5, and 6.
Exp. number
Effective aperture area (m2)
T
wi (°C)
T
wf (°C)
T
av (°C)
H
av (W/m2)
Durationτ (seconds)
(M · C)w (J/K)
F
2
P (W)
4
1.08
60
92
36.6
852.4
960
16,800
0.638
560
5
1.08
60
91
41.8
814.6
1560
16,800
0.453
333.8
6
1.08
65
91
42.8
990.2
780
16,800
0.610
560From the results in Tables2 and 3, it is concluded that the average value of the first figure of merit F1 is 0.2578, while that of the second figure of merit F2 is 0.567. The average cooking power of the solar cooker is 485 W. For comparison, the typical value of F1 is 0.103, F2 is 0.309, and the cooking power is 30 W for typical box-type solar cookers [4], while F1 is 0.395 and F2 is 0.654 for SK-14-type solar cooker with 1.54 m2 aperture area [12]. These parameters indicate that the dual parabolic cooker performance is comparable to that of SK-14 solar cooker.


## 6. Determination of Exergy Efficiency and Quality Factor

Exergy efficiency is often measured and reported for a given solar energy device as a measure of its potential for extracting heat from its surrounding environment [19, 22]. As per definition, the exergy approaches zero as the device approaches an equilibrium state with the environment. Exergy of the solar radiation describes the exergy input to the solar energy device and is determined by measuring the solar radiation flux (I°AΔt) during the experiment and using the relation [23, 24]:
(4)EXi=I°AΔt1+TaTs413−43TaTs,where Ta and Ts, respectively, indicate the ambient air temperature during the experiment and the surface temperature of the sun, I° represents the measured solar radiation intensity perpendicular to the collector at a given instant, Δt is the time interval between two readings, and A indicates the aperture area of the solar collector under investigation. The exergy output power of the device can be evaluated as [23]
(5)Exo=Eout−M·C·TalnTwfTwi,where Twi is the initial and Twf is the final temperature of water (or any other material) placed inside the device. M and C, respectively, represent the mass and the specific heat capacity of the material.The exergy efficiency may therefore be evaluated as(6)ψ=M·C·Twf−Twi−TalnTwf/Twi/ΔtI°1+1/3Ta/Ts4−4/3Ta/TsA.Another important parameter is the exergy loss coefficient, which is determined by measuring the difference between exergy input and output and the temperature differenceδT between the water and the ambient air, defined as
(7)EXloss=Exi−ExoA·Δt·δTW/m2K.A plot of the exergy loss (Exi − Exo) versus δT can provide the overall heat loss coefficient of the cooker. Further, it has been proposed that a plot between the exergy output power and δT, fitted with a second order polynomial, can be used to infer the peak exergy power of the device during a particular experiment [25]. The plot may also be used to infer the temperature difference gap between the temperatures corresponding to half exergy power points, on either side of the peak power point.The exergy input power during the three experiments, as derived from (4), is shown in Figure 17.Figure 17
Exergy input power during the three experiments with 4 kg of water load. Curves are labeled according to the experiment number.The exergy output power during the three experiments, as extracted using5 and fitted to a least-squares curve to show the trend with time, is shown in Figure 18, while the exergy efficiency is plotted in Figure 19.Figure 18
Exergy output power during the three experiments with 4 kg of water load. Blue points correspond to experiment number 4, red to experiment number 5, and green to experiment number 6.Figure 19
Efficiency of the exergy output power during the three experiments with 4 kg water load. Blue points correspond to experiment number 4, red to experiment number 5, and green to experiment number 6.The exergy loss data (EXi − Exo) is plotted versus the temperature difference δT in Figure 20, corresponding to experiment numbers 4, 5, and 6. The data are fitted with linear curves. Heat loss coefficient (W/K m2) of the cooker is extracted by dividing the slopes of these curves by the aperture area of the cooker, while the specific heat loss coefficient (W/K kg m2) is obtained by further division by the amount of water. The quality factor of the solar cooker may be evaluated by dividing the peak exergy gained to the exergy lost at that instant [25].Figure 20
Least-squares fit to the exergy loss data for experiment numbers 4, 5, and 6.Figure21 shows the graphs between the output exergy power Exo and the temperature difference δT. The data are fitted to a second order polynomial, for all three experiments. The peak value of the exergy power and the temperature difference gaps corresponding to half peak power points have been extracted in each case.Figure 21
Exergy output power versus the temperature difference. Data are fitted with second order polynomials. Curves are labeled according to the experiment number.The top three lines in the left of Figure21 show the equations of the polynomial fits to the data for the three experiments. The bottom set of three lines shows the peak exergy power attained during each of the three experiments at a specific temperature difference. The third set of three lines at the right top of Figure 21 provides the temperature difference gaps at half peak exergy power points. The temperature difference gaps are 68.96, 102.43, and 44.93 K, respectively.The average value of the peak exergy power for the three experiments is 60.53 W, while the average temperature difference gap at half peak power is 72.1 K. The product of the peak power with the temperature difference gap is therefore 4364.33 W·K. This value is by far the highest reported in literature, for any solar cooker. Table4 summarizes the various exergy-based performance measuring parameters for these experiments and provides comparison of these parameters with those of other types of solar cookers [1, 3, 4, 25].Table 4
Various exergy-based performance measuring parameters for three types of solar cookers.
Cooker parameter
Dual parabolic
SK-14
Sheffler type
Box type
Vacuum tube type
Slope of exergy loss curve (W/K)
1.828
5.407
19.485
0.577
2.63
Aperture area (m2)
0.049
1.47
8.21
0.4326
0.107
Heat loss coefficient (W/K m2)
37.31
40.35
54.125
1.334
24.58
Specific heat loss coefficient (W/K kg m2)
9.326
8.07
2.706
0.417
4.916
Peak exergy gain (W)
60.53
18.21
55.75
48.39
55.6
Exergy lost at peak exergy gain (W)
805.87
171.79
560.606
377.90
1323.8
Quality factor
0.077
0.106
0.099
0.1281
0.042
Temperature difference at peak power (K)
50.48
30.33
29.165
31.64
55.2
Temperature difference gap at half power (K)
72.1
40.374
39.62
41.76
38.75
Product of temperature difference gap at half power to peak power (W·K)
4364.33
735.3
2208.815
2020.77
2154.5From Table4, it may be concluded that the specific heat loss coefficient for parabolic-type solar cooker is comparable to that of SK-14. The quality factor of this cooker is higher than that of vacuum tube-type cooker and comparable to those of Scheffler and SK-14 types. However, the peak exergy gain, which determines the actual useful energy, is quite high, as compared to other types of solar cookers. Further, the temperature difference gap at half peak power and its product with the peak exergy gain are substantially higher compared to any other solar cooker reported so far. The average energy efficiency during the three experiments was 46.3%, 39.9%, and 49.38%, respectively. Due to design improvements in the present cooker, the maximum energy (49.38%) and exergy (8–10% from Figure 19) efficiencies have substantially improved compared to the results reported for a single parabolic trough cooker, where maximum energy efficiency was 15.7% and maximum exergy efficiency was 1.25% [23]. Similarly, these parameters are substantial improvements over SK-14 and Sheffler-type parabolic solar cookers [25].


## 7. Conclusions

This paper presents the results of an experimental investigation of an improved dual parabolic reflector solar cooker along with its construction details. The cooker has been explicitly designed from the point of view of a common user in terms of its usefulness and ease of transportation and handling, while addressing several other issues prevalent with such cookers. The cooker has been extensively tested under different load conditions and without load. All test results support it as a substantial improvement over other solar cookers in terms of its capacity of cooking all types of food as well as faster cooking with a view to its portability and lightweightiness. The various standard performance measuring parameters have been evaluated at a test load of 4 kg of water. The average cooking power of the cooker has been found to be 485 W, while the maximum attainable temperatures with load approached 290°C. Many cooking experiments like frying of eggs and French fries and making of bread have been conducted several times with great ease. The cooker has high exergy gain of up to 70 W, with 8–10% maximum efficiency, while the thermal efficiency of the cooker is up to 49.4%. The product of peak exergy power to the temperature difference gap, which is an important parameter for comparing the performance of solar cookers, has been found to be 4364.33 W·K, which is by far the highest reported in the literature, for any solar cooker. The cooker is low cost (around US$ 100) and easy to manufacture. It is quite ready for large scale dissemination.



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