Applied Energy 86 (2009) 68 73
Contents lists available at ScienceDirect
Applied Energy
journal homepage: www.elsevier.com/locate/apenergy
An experimental study on the development of a b-type Stirling engine
for low and moderate temperature heat sources
a,* a a b
Halit Karabulut , Hüseyin Serdar Yücesu , Can Ç1nar , Fatih Aksoy
a
Department of Mechanical Technology, Faculty of Technical Education, Gazi University, 06500 Teknikokullar, Ankara, Turkey
b
Department of Mechanical Technology, Faculty of Technical Education, Afyon Kocatepe University, 03100 Afyon, Turkey
a r t i c l e i n f o a b s t r a c t
Article history:
In this study, a b-type Stirling engine was designed and manufactured which works at relatively lower
Received 30 October 2007
temperatures. To increase the heat transfer area, the inner surface of the displacer cylinder was aug-
Received in revised form 4 April 2008
mented by means of growing spanwise slots. To perform a better approach to the theoretical Stirling
Accepted 5 April 2008
cycle, the motion of displacer was governed by a lever. The engine block was used as pressurized working
Available online 27 May 2008
fluid reservoir. The escape of working fluid, through the end-pin bearing of crankshaft, was prevented by
means of adapting an oil pool around the end-pin. Experimental results presented in this paper were
Keywords:
obtained by testing the engine with air as working fluid. The hot end of the displacer cylinder was heated
Beta type Stirling engine
with a LPG flame and kept about 200 °C constant temperature throughout the testing period. The other
Hot-air engine
end of the displacer cylinder was cooled with a water circulation having 27 °C temperature. Starting from
Engine performance
ambient pressure, the engine was tested at several charge pressures up to 4.6 bars. Maximum power out-
put was obtained at 2.8 bars charge pressure as 51.93 W at 453 rpm engine speed. The maximum torque
was obtained as 1.17 Nm at 2.8 bars charge pressure. By comparing experimental work with theoretical
work calculated by nodal analysis, the convective heat transfer coefficient at working fluid side of the dis-
placer cylinder was predicted as 447 W/m2 K for air. At maximum shaft power, the internal thermal effi-
ciency of the engine was predicted as 15%.
Ó 2008 Elsevier Ltd. All rights reserved.
1. Introduction harmless and thermally more efficient however, still there are
some problems to solve. In the last few decades, Stirling engines
For the current situation, fossil fuels meet most of the world s operating under low temperature difference, especially solar pow-
energy demand, but because of the rapid depletion of fossil fuels ered low temperature difference Stirling engines, gained so much
and environmental considerations, the interest in alternative en- importance. These engines can be run with very small differences
ergy sources and effective energy conversion systems has signifi- in temperature between the hot and cold sides of the displacer cyl-
cantly increased [1 3]. The energy conversion from solar inder and are able to use low grade, cheap and waste heat sources
radiation or any heat energy to mechanical energy can be per- including solar energy [9 12].
formed via Stirling engines with high thermal efficiency. The Stir- Since 1816, many studies on Stirling engines have been con-
ling engine is a mechanical device working with a closed cycle. ducted. The era of modern Stirling engine development was started
In the theoretical cycle of the Stirling engine, the working fluid is in 1937 by the Philips Company of The Netherlands. Philips devel-
compressed at constant temperature, heated at constant volume, oped a number of Stirling engines of various sizes up to 336 kW
expanded at constant temperature and cooled at constant volume [12,13].
[4 6]. Since the Stirling engine is externally heated and the heat In 1983, Kolin [11] demonstrated the first low temperature dif-
addition is continuous, many energy sources, such as solar radia- ference Stirling engine. Senft [11,14] developed the Ringbom en-
tion, combustible materials, radioisotope energy, all kind of fuels gine using the ideas introduced by Kolin. Iwamoto et al. [15]
so on, can be used. Stirling engines have less pollutant emissions compared the performance of a high temperature difference Stir-
in comparison with internal combustion engines [4,7 9]. ling engine with a low temperature difference Stirling engine. They
The Stirling engine was first patented in 1816 by Robert Stirling. concluded that at the same working conditions the thermal effi-
Stirling engines built in 19th century were huge in volume and ciency of the low temperature difference Stirling engines will not
small in power. Modern Stirling engines are environmentally reach that of high temperature difference Stirling engines.
Kongragool and Wongwises [16] manufactured and tested twin
power pistons and four power pistons, gamma-configuration low
* Corresponding author. Tel.: +90 312 2028639; fax: +90 312 2120059.
E-mail address: halitk@gazi.edu.tr (H. Karabulut). temperature difference Stirling engines. Engines were tested with
0306-2619/$ - see front matter Ó 2008 Elsevier Ltd. All rights reserved.
doi:10.1016/j.apenergy.2008.04.003
H. Karabulut et al. / Applied Energy 86 (2009) 68 73 69
Nomenclature
sc length of cold volume (m) Ti nodal values of working fluid temperature (K)
sh length of hot volume (m) Uc length from cylinder top to the fixing pin center (m)
Hp
distance between piston top and piston pin (m) Dd angle made by displacer rod with cylinder axis (rad)
2
Hd displacer length (m) bp angle made by piston rod with cylinder axis (rad)
ld length of displacer rod (m) c angle made by slotted arm of lever with cylinder axis
lm distance of fixing pin and crank pin (m) (rad)
p
lR length of displacer rod (m) ð2 uÞ Conjunction angle of lever arms (rad)
lp length of piston rod (m)
SL length of lever arm connected to displacer rod (m)
various heat inputs using a domestic gas burner. Power of engines
measured were far-off any industrial application.
Cinar and Karabulut [9] designed and manufactured a gamma
type Stirling engine. The engine was tested with air and helium.
Maximum output power was obtained as 128.3 W. Karabulut
et al. [17] investigated the thermodynamic performance character-
istics of a novel mechanical arrangement of concentric Stirling en-
gine using nodal analysis. In an experimental study, carried out by
Cinar et al. [18], a b-type prototype Stirling engine was manufac-
tured and tests were conducted at atmospheric pressure. The en-
gine provided maximum 5.98 W brake power at 208 rpm.
A Stirling radioisotope generator having 110 W power output is
currently being developed by the Department of Energy, Lockheed
Martin and the NASA Glenn Research Center to use in space inves-
tigations. This generator promises higher efficiency, specific power
and reduced mass compared to alternatives [19].
This study aims to develop a Stirling engine for low and moder-
ate temperature energy sources having 200 500 °C heating range.
The power output of the engine was designed as 500 W. As work-
ing fluid ambient air and helium was considered. The speed of the
engine was designed as 1200 rpm. The prime objective of the en-
gine to be developed is solar power generation at domestic scale.
The engine should be eligible to couple with a parabolic collector
and to reflect solar rays directly onto the hot end of displacer
cylinder.
In most of solar energy applications of Stirling engine, the solar
rays are concentrated by a parabolic dish and focused on a heat
pipe. The solar energy received by the heat pipe is converted to
heat and conveyed to the heater or hot end of the Stirling engine.
The heat pipe is used to reduce the energy losses by thermal radi-
ation and reflection as well as satisfying the uniform heating. A
Stirling engine working at 200 250 °C hot end temperature is not
exposed to high thermal stresses. The energy loss by thermal radi-
ation is also not too much. Therefore, in a domestic scale solar en-
ergy conversion system the use of a Stirling engine working at
200 250 °C hot end temperatures may exclude the heat pipe and
simplify the system as well as reducing the cost of construction.
The engine being developed is also considered for water pumping
in greenhouses.
Fig. 1. Schematic illustration of the test engine.
2. Mechanical arrangement
ner surface of the piston liner was finished by honing. The external
In Fig. 1 and Table 1, the mechanical arrangement of the man- surface of the piston liner is cooled by water circulation. The piston
ufactured b-type Stirling engine and its specifications are shown. was made of aluminum alloy because of its light weight and
The cylinder of the engine consists of two sections connected to machining simplicity. The surface of the piston was machined at
each other end-to-end. The first part functions as piston liner and super-finish quality. Appropriate value of clearance between pis-
made of oil hardening steel. The second part functions as displacer ton and piston liner was determined experimentally.
cylinder and made of ASTM steel. The displacer and the displacer As shown in Fig. 1, the crankshaft has only one pin for the con-
cylinder wall were used as a regenerator. Two different displacer nection of piston rod and lever arm. The motion of the displacer is
cylinders were manufactured and tested. One of them has a governed by a lever. The lever-controlled mechanism and the
smooth inner surface and the other has augmented inner surface assembly of piston and displacer are shown in Fig. 2. The lever con-
with rectangular slots having 2 mm width and 3 mm depth. The in- sists of two arms with 70° conjunction angle. One of them holds a
70 H. Karabulut et al. / Applied Energy 86 (2009) 68 73
Table 1
3. Kinematic relations
Technical specification of the test engine
Parameters Specification Thermodynamic analysis was conducted by using the nodal
program presented by Karabulut et al. [17]. The working space of
Engine type b
Power piston Bore stroke (mm) 70 60 the engine was divided into 50 nodal volumes. To calculate nodal
Swept volume (cc) 230
values of hot and cold volumes, kinematic relations
Displacer Bore stroke (mm) 69 79
Hp
Swept volume (cc) 295
Scźldcosbd SLsic uÞþlR lmcosc lpcosbp ; ð1Þ
Working fluid Air
2
Cooling system Water cooled
ShźUc ldcosbd SLsic uÞ lR Hd ð2Þ
Compression ratio 1.65
Total heat transfer area of the 1705
were used. In these equations bp is the angle between piston rod
displacer cylinder (cm2)
and cylinder axis and defined as
Maximum engine power 51.93 W (at 453 rpm)
Rcr
bpźArcsin sin h : ð3Þ
lp
bd, c and lm are; the angle between displacer rod and cylinder
axis, the angle between slotted arm of lever and cylinder axis
and the distance between lever s fixing pin and crank pin, respec-
tively. Mathematical definitions of them depend on the location of
the lever s fixing pin. The point providing the maximum work per
cycle was chosen as the location of fixing pin and determined via
isothermal analysis. With respect to the location of fixing pin; bd,
c and lm were defined as
0:7071þsinh
cźArctan ; ð4Þ
2:5þcosh
SL Rcr
bdźArcsin cosðcuÞ 0:7071 ; ð5Þ
ld ld
Rcrð0:7071þsinhÞ
Lmź : ð6Þ
sinc
p
The conjunction angle of lever arms was defined asð2 uÞand
the optimum value of u was determined as 0.35 rad. Nodal vol-
umes within the regenerator have constant values and take place
around the displacer.
4. Experimental apparatus and testing procedure
A prony type dynamometer with accuracy of 0.003 Nm was
used for loading the engine. The speed of the engine was measured
by a digital tachometer, ENDA ETS1410, with 1 rpm accuracy. Tem-
peratures were measured with a non-contact infrared thermome-
ter, DT-8859, with Ä…2 °C accuracy. Heat was supplied by a LPG
burner. The charge pressure was measured with a bourdon tube
pressure gauge with 0.1 bar accuracy and 0 10 bars measurement
range. A pressure regulating valve was used for the regulation of
the charge pressure. The schematic view of the experimental appa-
Fig. 2. The lever-controlled mechanism, piston and displacer assembly.
ratus is shown in Fig. 3.
The charge pressure was applied to the block of the engine and
its value was read from the pressure gauge. By means of increasing
slot bearing as the other holds a circular bearing. At the corner of
and decreasing the external load, the speed of the engine was sta-
lever, a third bearing exists. The lever is mounted to the body of en-
bilized at any desired value and then reading of the load; speed and
gine through the bearing at the corner by means of a pin. The slot
temperature were made simultaneously.
bearing at one arm of the lever is connected to the crank pin. The
circular bearing at the other arm of lever is connected to the dis-
placer rod. While the crank pin turns around the crank center, it 5. Results and discussion
drives the lever fort and back around the pin connecting the lever
to the body. The other arm connected to the displacer rod moves The variation of cold volume, hot volume and total volume with
the displacer up and down. Both ends of crankshaft were bedded the crank angle is shown in Fig. 4. In the engine the minimum va-
with ball bearings. Escape of working fluid through the crankshaft lue of cold volume appears about 50° of crank angle and, before
bed was prevented by means of adapting an oil pool around the and after 50° it performs significant variations. This interval of
crank shaft end-pin. As long as the charge pressure was below crank angle corresponds to expansion period of working fluid.
5 bars no air leak was observed. The block of the engine was man- The interval of crankshaft angle from 135° to 225° corresponds
ufactured of two parts and coupled by screws. Between two parts to cooling process at constant volume. In this process the mecha-
of the engine block a plastic seal was set. To lubricate working nism presents a better performance by means of minimizing the
parts of the engine some oil was filled into the engine block and hot volume and maximizing the cold volume without changing
its circulation was satisfied by throwing via the lever arm. the total volume.
H. Karabulut et al. / Applied Energy 86 (2009) 68 73 71
Fig. 3. Schematic illustration of the test equipment.
At initial testing conducted with ambient pressure and displac- are illustrated in Fig. 5 and 6, respectively. Data used in Figs. 5
er cylinder having smooth inner surface, the engine started to run and 6 were obtained about 200 °C hot-end temperature and at dif-
at a 93 °C hot-end temperature. Cooling water temperature was ferent values of charge pressure. Up to a certain level of speed, the
measured as 27 °C. At the other tests conducted with different power increases with speed and then declines. Decrease of the
charge pressures, running temperature of the engine varied up to power output after a certain speed is estimated due to inadequate
125 °C. When the heating was ceased, the engine continues to heat transfer caused by limited heating and cooling time. Flow and
run until the hot-end temperature drops to 75 °C. mechanical frictions may also have effects on decreasing of power.
For the displacer cylinder having augmented inner surface, the As shown in Fig. 5, the power output obtained at 3.5 and 4.6 bars
variations of power output and brake torque with engine speed are lower than at 2.8 bars. At 200 °C hot-end temperature, the opti-
mum charge pressure is estimated as 2.8 bars. Maximum power
output obtained at 2.8 bars charge pressure is 51.93 W and appears
at 453 rpm engine speed. As seen in Fig. 6, the brake torque has
450
also a maximum value at a certain value of speed. At higher and
Cold volume
400
Hot volume lower values of speed, the reasons causing the power output to de-
Total volume
crease causes also the brake torque to decrease. The maximum val-
350
ues of power and torque correspond almost to the same speed.
300
In the nodal program developed by Karabulut et al. [17], by
250
using 2.8 bars charge pressure, 200 °C hot-end temperature, 27 °C
200
cold-end temperature and 453 rpm engine speed, the convective
heat transfer coefficient at working fluid side of cylinder was deter-
150
mined as 447 W/m2 K by trial and error corresponding to 51.93 W
100
shaft power or 6.88 J shaft work per cycle. The p V diagram of the
50
engine obtained for these conditions was illustrated in Fig. 7. In the
0
same figure, the p V diagram obtained by isothermal analysis,
0 90 180 270 360
which corresponds to an infinite heat transfer coefficient, was also
Crank Angle (Degree)
illustrated. In order to check whether the heat transfer coefficient
Fig. 4. Variation of cold volume, hot volume and total volume with crank angle. of 447 W/m2 K is valid for the other cases or not, the nodal pro-
3
Volume (cm )
72 H. Karabulut et al. / Applied Energy 86 (2009) 68 73
60 60 1.2
Atm.
1.4 Bar
50
50 1
2.8 Bar
40
3.5 Bar
40 0.8
4.6 Bar
30
30 0.6
20
20 0.4
10
Engine torque
10 0.2
Engine power
0
200 250 300 350 400 450 500 550 600
0 0
Engine Speed (rpm)
0 1 2 3 4 5
Charge Pressure (Bar)
Fig. 5. Variation of brake power with engine speed.
Fig. 8. Variation of brake power and engine torque with charge pressure.
1.4
Atm.
By means of equating Nusselt numbers of air and helium to
1.2
1.4 Bar
each other, the heat transfer coefficient of helium was calculated
2.8 Bar
1
3.5 Bar as 2392 W/m2 K. If we consider that Nusselt number increases as
4.6 Bar
flow velocity increases, the heat transfer coefficient of 2392 W/
0.8
m2 K is a safe value to predict the power of the engine with helium
0.6 as working fluid. By means of introducing 2.8 bars charge pressure,
500 °C hot-end temperature, 27 °C cold-end temperature,
0.4
1200 rpm engine speed and 2392 W/m2 K heat transfer coefficient
to the nodal program, the power of the engine was predicted as
0.2
493 W. In addition this, if we consider the increase of charge pres-
0
sure with hot-end temperature, the engine should provide a higher
250 300 350 400 450 500 550 600
power than the above predicted.
Engine Speed (rpm)
Fig. 8 illustrates the variation of the power output and brake
torque with charge pressure ranging from 0 to 4.6 bars. As the
Fig. 6. Variation of engine torque with engine speed.
charge pressure increases, the output power and brake torque in-
crease as well, and reaches to a maximum. Further increase of
400
charge pressure over the optimum value causes output power
h=447 W/m2K
380
and brake torque to decrease. It was also noted that, increasing
Isothermal
the charge pressure resulted in increase of vibration.
360
Figs. 9 and 10 show the performance comparison of smooth and
340
slotted displacer cylinders in terms of engine power and brake tor-
320
que. Both cylinders were tested at 200 °C hot-end temperatures
300
and several values of charge pressure. The slotted cylinder having
Charge pressure = 2.8 bars
280
214% larger inner surface than smooth cylinder provides about 50%
higher power which is lower than our expectations. The reason
260
limiting the power and torque is guessed as inadequacy of hot-
240
end temperature and decrease of compression ratio. To get larger
220
power outputs, the hot-end temperature should be increased or
Work of isothermal analysis = 13.57 J/cycle
200
Work of nodal analysis = 6.88 J/cycle the augmentation of inner surface of the displacer cylinder should
180
be made without permeating the compression ratio to decrease at
350 400 450 500 550 600
a significant rate.
Volume (cm3)
Fig. 7. p V diagrams obtained with isothermal and nodal analysis.
60
1.4 Bar (slotted)
gram was run with 325 rpm engine speed, 1 bar charge pressure
2.8 Bar (slotted)
and 447 W/m2 K heat transfer coefficient. As the result 4.068 J
50 3.5 Bar (slotted)
4.6 Bar (slotted)
work was obtained. For the same conditions, the experimental va-
1.4 Bar (smooth)
40
lue of work is 3.32 J which can be deduced from Fig. 5. The differ- 2.8 Bar (smooth)
3.5 Bar (smooth)
ence between these experimental and theoretical works may be
30
caused by mechanical frictions which consumes a certain amount
of work produced by working fluid. Obviously while the engine
20
runs at a low power, the ratio of mechanical losses to the produced
work by working fluid becomes larger. Therefore, the convective
10
heat transfer coefficient determined as 447 W/m2 K seems to be
0
valid for different situations caused by engine speed, charge pres-
200 250 300 350 400 450 500 550 600
sure and compression ratio. Obviously, variation of the slot geom-
Engine Speed (rpm)
etry and the gap between displacer and cylinder will cause the
convective heat transfer coefficient to vary. Fig. 9. Comparison of smooth and slotted cylinders in terms of power.
Engine Power (W)
Engine Power (W)
Engine Torque (Nm)
Engine Torque (Nm)
Pressure (kPa)
Engine Power (W)
H. Karabulut et al. / Applied Energy 86 (2009) 68 73 73
1.4
6. Conclusions
1.4 Bar (slotted)
2.8 Bar (slotted)
1.2
3.5 Bar (slotted)
By means of a lever controlled displacer driving mechanism a
4.6 Bar (slotted)
1.4 Bar (smooth) better approximation to theoretical Stirling cycle was achieved.
1
2.8 Bar (smooth)
By using a LPG burner as heat source, the engine was tested with
3.5 Bar (smooth)
0.8
air up to 4.6 bars charge pressure. At the ambient pressure testing,
the engine started to run at 93 °C hot-end and 27 °C cold-end tem-
0.6
peratures. On the starting temperature the charge pressure made a
0.4 slight effect. Maximum power output was obtained as 51.93 W at
453 rpm engine speed and 2.8 bars charge pressure. The internal
0.2
thermal efficiency corresponding to maximum power was deter-
mined as 15%. When the heat transfer area of the engine was in-
0
200 250 300 350 400 450 500 550 600
creased by augmenting the displacer cylinder inner surface, a
Engine Speed (rpm)
50% increase in output power was obtained. Via an oil pool adapted
to the crankshaft s end-pin bearing, the leak of working fluid was
Fig. 10. Comparison of smooth and slotted cylinders in terms of torque.
perfectly avoided up to 5 bars charge pressure. For 500 °C hot-
end temperature, 27 °C cold-end temperature, 2.8 bars helium
49.5 0.4
charge pressure and 1200 rpm engine speed, the power of the en-
Heat per cycle
gine was predicted as 493 W via the nodal program.
49
0.35
Experimental efficiency
Efficiency calculated bynodal analysis
48.5
Acknowledgments
0.3
48
0.25
This study was supported by The Scientific and Technological
47.5
Research Council of Turkey (TUBITAK) in frame of the Project code
0.2
of 105M256. As researchers, we thank The Scientific and Techno-
47
logical Research Council of Turkey.
0.15
46.5
0.1 References
46
0.05 [1] Dincer I. Renewable energy and sustainable development: a crucial review.
45.5
Renew Sustain Energy Rev 2000;4:157 75.
[2] Sorensen B. Renewable energy. 3rd ed. UK: Elsevier Science; 2004.
45 0
[3] Abdullah S, Yousif BF, Sopian K. Design consideration of low temperature
290 340 390 440 490 540
differential double-acting Stirling engine for solar application. Renew Energy
Engine Speed (rpm)
2005;30:1923 41.
[4] Walker G. Stirling engines. Oxford: Clarendon Press; 1981.
Fig. 11. Thermal efficiency and heat given to the working fluid.
[5] Waldes LC. Competitive solar heat engines. Renew Energy 2004;29:1825 42.
[6] Martini WR. Stirling engine design manual. US Department of Energy; NASA
CR-13518; 1978.
If the variation of internal thermal efficiency of the engine is
[7] Kongtragool B, Wongwises C. Investigation on power output of the gamma-
examined by nodal analysis using the convective heat transfer configuration low temperature differential Stirling engines. Renew Energy
2005;30:465 76.
coefficient of 447 W/m2 K, the charge pressure of 2.8 bars, the
[8] Tsoutsos T, Gekas V, Marketaki K. Technical and economical evaluation of solar
hot end temperature of 200 °C, the cold end temperature of 27 °C
thermal power generation. Renew Energy 2003;28:873 86.
and specific values given in Table 1., a linear variation with engine [9] Cinar C, Karabulut H. Manufacturing and testing of a gamma type Stirling
engine. Renew Energy 2005;30:57 66.
speed is obtained as seen in Fig. 11. The thermal efficiency varies
[10] Walker G, Fauvel OR, Reader G. The literature of Stirling engines. In: Energy
from 12% to 18% as the engine speed varies from 550 rpm to
conversion engineering conference, IECEC-89 proceedings of the 24th
300 rpm. Determination of the heat transferred to the working
intersociety, 6 11 August; 1989. p. 2337 40.
[11] Senft JR. An introduction to low temperature differential Stirling
fluid per cycle was not easy to measure. Therefore the heat was
engines. USA: Moriya Press; 2004.
predicted by nodal analysis by means of introducing experimental
[12] Kongtragool B, Wongwises S. A review of solar-powered Stirling engines and
conditions to the program and results were illustrated in Fig. 11. By
low temperature differential Stirling engines. Renew Sustain Energy Rev
2003;7:131 54.
using the heats predicted by nodal analysis and experimental
[13] Senft JR. An introduction to Stirling engines. USA: Moriya Press; 2004.
works, the thermal efficiency of the engine was determined and
[14] Robson A, Grassie T, Kubie J. Modeling of a low-temperature differential
compared to the theoretical efficiency in Fig. 11. While the exper-
Stirling engine. Proc IMechE Part C J Mech Eng Sci 2007;221:927 43.
[15] Iwamoto I, Toda F, Hirata K, Takeuchi M, Yamamoto T. Comparison of low-and
imental efficiency approaches to the theoretical efficiency at low
high-temperature differential Stirling engines. In: Proceedings of eighth
speeds of the engine, it presents larger diversity at high speeds.
international Stirling engine conference; 1997. p. 29-38.
The difference may be caused by several reasons but mainly inad-
[16] Kongtragool B, Wongwises S. Performance of low-temperature differential
equate heat transfer to and from working fluid. Stirling engines. Renew Energy 2007;32:547 66.
[17] Karabulut H, Yücesu HS, Cinar C. Nodal analysis of a Stirling engine with
While the charge pressure decreases, thermal efficiency of the
concentric piston and displacer. Renew Energy 2006;31:2188 97.
engine increases. For instance, corresponding to 3.32 J shaft work
[18] Cinar C, Yucesu S, Topgul T, Okur M. Beta-type Stirling engine operating at
obtained at ambient pressure testing, the efficiency of the engine atmospheric pressure. Appl Energy 2005;81:351 7.
[19] Schreiber JG, Thieme LG. Final results for the GRC supporting technology
was calculated as 20.6%. At lower charge pressures however, the
development project for the 110-watt Stirling radioisotope generator
ratio of mechanical losses to the work generated by working fluid
(SRG110). NASA Glenn Research Center Technical Reports, NTRS; 2007. p.
will increase and the break thermal efficiency will decrease. 05 25.
Engine Torque (Nm)
Efficiency
Heat (Joule/cycle)
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