GB2118635A - Module for forming a modular Stirling engine assembly - Google Patents
Module for forming a modular Stirling engine assembly Download PDFInfo
- Publication number
- GB2118635A GB2118635A GB08210930A GB8210930A GB2118635A GB 2118635 A GB2118635 A GB 2118635A GB 08210930 A GB08210930 A GB 08210930A GB 8210930 A GB8210930 A GB 8210930A GB 2118635 A GB2118635 A GB 2118635A
- Authority
- GB
- United Kingdom
- Prior art keywords
- module
- cooler
- cylinder
- engine
- heater
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000010438 heat treatment Methods 0.000 claims abstract description 12
- 238000010276 construction Methods 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 9
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 229910052708 sodium Inorganic materials 0.000 description 4
- 239000011734 sodium Substances 0.000 description 4
- 239000007788 liquid Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000000429 assembly Methods 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 2
- 239000000498 cooling water Substances 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012812 general test Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000011551 heat transfer agent Substances 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000006262 metallic foam Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases
- F02F7/0021—Construction
- F02F7/0031—Construction kit principle (modular engines)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B1/00—Reciprocating-piston machines or engines characterised by number or relative disposition of cylinders or by being built-up from separate cylinder-crankcase elements
- F01B1/12—Separate cylinder-crankcase elements coupled together to form a unit
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
- F02G1/00—Hot gas positive-displacement engine plants
- F02G1/04—Hot gas positive-displacement engine plants of closed-cycle type
- F02G1/043—Hot gas positive-displacement engine plants of closed-cycle type the engine being operated by expansion and contraction of a mass of working gas which is heated and cooled in one of a plurality of constantly communicating expansible chambers, e.g. Stirling cycle type engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
- F02G2244/00—Machines having two pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
- F02G2244/00—Machines having two pistons
- F02G2244/50—Double acting piston machines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
The module is composed of a cylinder head 12, Fig. 3, a heater 22, a regenerator 32, a cooler 42 and a cold duct 39. A plurality of such modules are assembled to construct a multi- cylinder double acting Stirling engine of the indirect heating type, Fig. 5 (not shown). The heater tubes 6 are enclosed in a housing which rigidly connects the cylinder head and the regenerator of the module, and the cold duct 39 is connected to the base of a cylinder which corresponds to an adjacent module. <IMAGE>
Description
SPECIFICATION
Heat exchanger module for stirling engines
It is known that Stirling engines are heat engines of the external heating, piston type, in which the working gas, which is helium or hydrogen, circulates alternately from one cylinder to another, passing through a tubular heat exchanger in which it is heated, a porous metallic matrix known as a regenerator, in which it receives or gives up heat, and another tubular heat exchanger in which it is cooled. The two heat exchangers also enable it to retain its temperature when it is compressed or expanded in the cylinders.
A two-cylinder engine of this type is illustrated diagrammatically in Figure 1. A kinematic connection comprising connecting rods and a crankshaft is provided between the two pistons in such a manner that the movement of the piston of the "cold" cylinder B is offset 900 in relation to that of the "hot" cylinder A. When the crankshaft
F turns about one sixth of a turn in the direction indicated by the arrow, starting from the position shown in Figure 1, the piston of cylinder A moves very little, while the piston of cylinder B compresses the gas which is kept cold by the cooler C. When the next sixth of a revolution is made, the gas is transferred from cylinder B to cylinder A while being heated by the regenerator D and the heater E.During the next sixth of a revolution, the piston of cylinder B moves very little, while the piston of cylinder A allows the gas kept hot by the heater E to expand. In the next half-revolution the gas is transferred from cylinder
A to cylinder B while being cooled by the regenerator D and the cooler C, and a new cycle starts. In the course of this complete cycle, as in any heat engine, heat is supplied at high temperature (in the heater), heat is given up at low temperature (in the cooler), and work is done (on the crankshaft). Heating in the heater E is generally effected by passing through it combustion gases from various materials, and cooling is effected in the cooler C by means of a current of cold water.
A known arrangement of this kind can be modified as shown in Figure 2. The variable cold volume is disposed not above, but below the piston of cylinder B, on the kinematic connection side. The operating principle of the engine is not changed, provided that the movement of the piston of cylinder B is 900 ahead in phase in relation to that of cylinder A, as is shown in this
Figure.
The diagram given in Figure 2 makes it possible to conceive the connection in series of a plurality of engine units of the kind shown in Figure 2 as is suggested by the pipe outlets shown on cylinders
A and B. A double-acting piston engine is then obtained in which each of the pistons works on both its faces, and the power of which is substantially doubled for a given cylinder capacity.
Furthermore, the devices sealing the engine in relation to the outside are situated under the cold variable volumes of the cylinders, so that their construction is less difficult. The various engine units, which are generally from three to six in number, preferably form a closed chain in an arangement due to RINIA. This principle has been adopted for almost all existing Stirling engines.
For good thermodynamic functioning it is necessary in practice that the hot ducts between A and E in Figure 2 and the cold ducts between B and C, constituting dead volumes and causing pressure drops, should be shortened as much as possible; in order to reduce deformation, play and friction, it is also necessary that the kinematic connection between the various piston rods should simplified as far as possible. Finally, when heating is effected by combustion gases, it is necessary for the tubes of the heater E to be grouped to form a single heating head permitting uniform distribution of the heat.
A very compact engine complying with the conditions set forth above is obtained by disposing four cylinders in a square. The piston rods may be parallel and may operate an inclined plate (swash plate or wobble plate) or a double crankshaft (H type engine); they may also be inclined in V form and drive d single crankshaft (double V type engine). These various arrangements are those most generally adopted in present Stirling engines.
As a setoff to compactness, these Stirling engines lose the modular character which it would have been possible to obtain by connecting a plurality of engine units in series in accordance with the diagram shown in Figure 2. They are composed of a single engine assembly in which only small components, such as regenerators, coolers or pistons, are manufactured as sets ot identical parts.
The object of the present invention is a heat exchanger module for Stirling engines, which comprises in known manner a tubular heater, a regenerator and a tubular cooler, together with at least one cylinder part, the regenerator and the cooler forming an assembly of generally cylindrical shaped, whose axis is parallel to the axis of the cylinder head, and this module being designed to permit the construction of a double acting Stirling engine by mounting a plurality of identical modules on an engine assembly equipped with inline pistons connected to a crankshaft, while the cooler of each module of the engine is connected by a cold duct to the base of the cylinder which corresponds to an adjacent module.In a module of this kind, according to the invention, the heater is of the indirect heating type and its tubes are enclosed in a housing which rigidly connects the cylinder head and the regenerator housing.
The modular design according to the invention offers numerous advantages. The various engine units making up the engine are strictly identical, including the hot and cold ducts connecting the heat exchangers to the engine assembly, so that the operation of the engine is perfectly regular.
Designing and -adjustment tests are simplified because of the existence of identical units in the engine. The cost of manufacture of parts and assembly of units for general tests, construction of engines and supply of spares is reduced because of the increased number of identical components.
Maintenance requires a smaller stock of parts.
Engines differing in respect of shape or number of cylinders can easily be constructed from the same modules.
The tubes of the cooler are preferably rectilinear and directed parallel to the axis of the cooler, while its outside wall is made of a flexible materal so that it is capabie of absorbing, with concomitant deformation of these tubes in S shape, the effects of thermal expansions of the heater in relation to the engine assembly as the result of the considerable differences in temperature which occur between these eiements in the course of operation.
In order to give substantially the same length to the cold ducts between the modules of one dnd the same engine, whether these ducts connect two adjacent modules or connect two modules separated by another module, according to the invention provision is made for each module to have at the base of its cooler, for connection to the cold duct, a device able to assume two different configurations offering different connection lengths, so as to compensate for differences in distance between modules.A connection device of this kind may be composed of a thick plate forming the bottom of the cooler and having, in an eccentric position relative to the axis of the cooler, an opening providing communication between the interior of the cooler and a duct formed in the thickness of the said plate, at right angles to the said axis, by way of a bent connector housed in a cavity facing the said opening and dividing the said duct into two portions of unequal lengths, so that connection to the adjacent cylinder can be made either by way of one or the other of these portions depending on the orientation of the bent connector in relation to the said plate.For a cold duct connecting-two contiguous modules, use will thus be made of the "long" configuration, while for a cold duct connecting two modules separated by a third module use will be made of the "short" configuration, in conjunction with an auxiliary pipe. In order to facilitate access to the bent connector, so as to turn it round when it is desired to change over from one configuration to the other, it is expedient for the eccentric opening in question to be made in a detachable auxiliary part fitting into a socket formed in the said plate and in communication with the said cavity.
A module according to the invention may include only the head of the corresponding cylinder, this head being connected leaktightly to the casing of the said cylinder, the casing forming part of the engine assembly. It may however be preferable for the module also to incorporate the cylinder casing, which is then integral with the cylinder head and is leaktightly connected at its base to the body of the engine assembly. This lastmentioned arrangement makes it possible for the seal required for the connection to the engine assembly to be situated in a region where temperature and pressure conditions are less severe, that is to say in the cold part of the cylinder.
The modular design of the heat exchangers according to the invention makes it possible to obtain at one and the same time:
compact engine assemblies with short gas circuits which are equal in length and do not intercross;
a kinematic system for four or six cylinders in line, with a single crankshaft, according to the most usual automobile technique;
sub-assemblies of simple shapes identical to one another;
excellent accessibility of the various components of the engines, thus facilitating dismantling and maintenance.
The description given below, in conjunction with the accompanying drawings which are given by way of examples without constituting limitations, make it possible to understand clearly how the invention may be put into practice.
Figure 3 shows a heat exchanger module according to the invention, in a vertical section on the line Ill-Ill in Figure 5.
Figure 4 shows the bottom of the cooler in the module shown in Figure 3, in another configuration.
Figure 5 is a plan view of a Stirling engine comprising four cylinders in line and formed by combining four modules according to the invention on an engine assembly.
In Figure 3 can be seen the various elements shown diagrammatically in Figure 2, namely a cylinder head 12, a heater 22, a regenerator 32, and a cooler 42, this assembly constituting, together with a cold duct connection device 52, a module according to the invention.
The heater 22, which is of the indirect heating type, comprises a housing 5 and numerous tubes 6 (of which only two have been shown) disposed in its interior and bringing the hot chamber 7 of the cylinder head 12 into communication with the regenerator 32. To the housing 5 is welded the end of a heat duct 62 carrying a heat-transfer agent (sodium, potassium or a eutectic of these two metals) between a heat source (not shown) and the heater 22. The tubes 6, which are several tens in number, have various shapes in such a manner as to have substantially the same length while being very close to one another. When brought to a temperature of the order of 7000C they conduct the working gas (helium or hydrogen), while heating it, at a pressure which may reach 250 bars.
The regenerator 32 is composed of a housing 9 into which the tubes 6 of the heater 22 are led and which encloses a porous cylindrical block 10 composed of a compressed stack of fine wire cloths or of a block of metal foam or porous ceramic material.
The housing 9 of the regenerator 32 and the cylinder head 12 are sufficiently tall and thin for the temperature at their base to be distinctly lower than the temperature imposed at their top by the heater 22. The cross-section of the regenerator 32 constitutes a surface about twice that of the cylinder head 12.
The housing 5 of the heater 22 is rigidly joined, namely by brazing, to the cylinder head 12 and to the housing 9 of the regenerator 32.
During operation the sodium (for example) is made gaseous in an evaporator situated at the other end (not shown) of the heat duct 62, by means of a heating apparatus such as an oven which may burn various fuels, a molten salt storage heater, a solar radiation receiver, and so on. In the heater 22 the sodium is condensed on the tubes 6, heating the gas contained in the latter, and returns in liquid form through the heat duct 62 to the heating apparatus. The transport of the liquid sodium is assisted either by gravity, which explains the slight slope shown in the drawing, or by a porous lining 8 consisting of fine wire cloths in the heat duct, or by a pump, in which case the gas enters and the liquid leaves by way of two different heat ducts.
The heat duct 62, the heater 22, the regenerator 32, and the top of the cylinder head 12 are enclosed in a thick covering (not shown) effecting their thermal insulation.
The cooler 42 is composed of a bundle of several hundred very thin tubes 15, which are rectilinear and parallel to the axis 1 6 on which the regenerator 32 and the cooler 42 are aligned, this axis being in turn parallel to the axis 48 of the cylinder head 32. These tubes are leaktightly brazed to two perforated plates 17, 1 8 connected together by a cylindrical sleeve 1 9. The top perforated plate 1 7 is fastened to the base of the housing 9 of the regenerator 32 by means of a double-screwthread ring 20, with the interposition of an O-ring 25. The bottom perforated plate 1 8 has an inlet aperture (not visible in Figure 3) and an outlet aperture 26 for the cooling water.The water, which is introduced into a bottom chamber 27, passes into the space surrounding the tubes 1 5 and bounded by a cylindrical sleeve 28 by way of a hole 29 formed centrally in a transverse metal plate 30, rises along the tubes 15, and then flows back down into the annular space between the sleeve 28 and the sleeve 19, passing out through the outlet pipe 26.
Under the bottom perforated plate 18 is fastened, by means of screws 35, a thick base 36 of circular contour, in the top face of which is formed centrally a circular recess receiving a member 37 provided, parallel to the axis 16, with an eccentric opening 38 leading into a funnelshaped inlet space 59. Below this recess there are formed in the base 36 a diametrical duct 39 and also a cavity dividing the duct 39 into two segments of unequal lengths and containing a hollow member 40 forming a connection bend between the eccentric opening 38 and the.duct 39.Depending on the orientation of the member 40 in the cavity receiving it, the length, inside the base 36, of the outlet duct of the cooler 42 may be given two different values, depending on whether the long segment of the duct 39 (Figure 3) or the short segment (Figure 4) is used.
In order to ensure that the outlet aperture 45a or 45b of whichever segment of the duct 39 is used remains on the same side, the base 36 is appropriately oriented under the cooler 42, as shown in Figures 3 and 4, while the aperture 45b or 45a of the unused segment is closed by a stopper 46. The outlet aperture is connected by a rigid connection assembly (flange, nuts and seal) to the base of the cylinder corresponding to an adjacent module, either directly or with the aid of an intermediate pipe 47 (see Figure 5), the base of the cooler 42 being adjusted as required to the "long" configuration or to the "short" configuration in such a manner that the total length of the cold ducts is substantially constant.
When a module is in operation, its heater 22 is brought to a temperature of about 7000 and the housing 5 of the heater undergoes elongation of 1 to 2 mm more than the engine assembly. In order to avoid excessive thermal stresses, the module is made slightly flexible at the level of the cooler 42, in which the tubes can be deformed in S-shape, with a corresponding sag. In order to give the cooler the desired flexibility while carrying the cooling water, the cylindrical sleeve 19 is composed of a flexible skin of elastomer or of a metal bellows.
In Figure 3 two forms of construction of the portion of the cylinder which is associated with the module have been shown, one on each side of the axis 48 of the cylinder. In the arrangement shown on the left, the casing 49 of the cylinder forms part of the engine assembly and is connected to the cylinder head 1 2 with the interposition of a seal 50. Since this seal is subjected to severe stressing due to the pressure and temperature, which at this point may reach the respective values of 250 bars and 250"C, it may be preferable to use the arrangement shown on the right in which the cylinder head 12 and the casing 49a are in one piece and connected to the engine assembly 55 with an interposed seal 50a.
The seal is thus transferred to the well cooled base of the casing, so that its life is lengthened.
For the purpose of forming a Stirling engine, a plurality of modules of the type just described are assembled and mounted (by means of fastening screws 58) on the engine assembly 55 (Figure 5); four such modules are used in the present example. These modules 1.2, 3, 4 are placed side by side, altemately in one direction and in the other, the cylinders being aligned along the axis 56 of a single crankshaft driving an output shaft 57. In this Figure can be seen the cylinder heads 11,12,14, the heaters 21,23,24, the regenerator 31, the coolers 41,42,43, the connection device 54, and the four heat ducts 61, 62, 63, 64.The base of the cooler 42 of the module 2, mounted in the "long" configuration shown in Figure 3, is connected directly to the base of the cylinder corresponding to the head 11 of the module 1; the base of the cooler 43 of the module 3 is similarly connected to the base of
the cylinder corresponding to the head 14 of the
module 4. A similar connection, but with the
interposition of a pipe 47, is made between
the base of the coolers 41 and 44 (in the "short"
configuration shown in Figure 4) and the base of
the cylinders corresponding to the heads 1 3 and
12 respectively. It can clearly be seen in Figure 5
that ali the cold ducts are approximately of the
same length and consequently have the same
volume.The modules thus operate in the order 1-2-4-3. The movements of the pistons in
the cylinders are offset 900 in the same order, in
accordance with the diagram shown in Figure 2,
the engine crankshaft being shaped accordingly.
The invention is also applicable to the case of a
Stirling engine having six cylinders in line. The
heat exchanger modules then operate in the order 1-2-4-6-5-3. The movements of the
pistons in the cylinders are offset 1200 in the
same order, the engine crankshaft being shaped
accordingly. This has the consequence that the
variations of the cold volume in the engine units
according to the diagram shown in Figure 2 are
offset 600 in relation to those of the hot volumes
(instead of 900 in the case of the four-cylinder
engine). The cold connections between the
coolers of the modules 2 and 5 and the cylinders
corresponding to the modules 1 and 6 respectively
are made by direct screw connection of the cooler
bases (in the configuration shown in Figure 3), while the cold connections between the coolers of
modules 4,1,6 and 3 and the cylinders
corresponding to modules 2, 3, 4 and 5
respectively require the interposition of
intermediate pipes 47, the bases of the coolers of
these modules being in the configuration shown in
Figure 4.
The heat ducts 61,62,63,64 welded tithe various heat exchanger modules 1, 2, 3, 4 are not
in general all identical, as would appear from
Figure 5. Their shape is adapted to the
connections to be made to the heat source or
sources of the engine.
Claims (8)
1. A heat exchanger module for Stirling
engines, which comprises a tubular heater, a
regenerator and a tubular cooler, together with at
least one cylinder part, the regenerator and the
cooler forming an assembly of generally cylindrical
shape, whose axis is parallel to the axis of the
cylinder head, and this module being designed to
permit the construction of a double acting Stirling engine by mounting a plurality of identical modules on an engine assembly equipped with inline pistons connected to a crankshaft, while the cooler of each module of the engine is connected by a cold duct to the base of the cylinder which corresponds to an adjacent module, wherein the said heater is of the indirect heating type and its tubes are enclosed in a housing which rigidly connects the cylinder head and the regenerator housing.
2. A module as claimed in Claim 1, wherein the tubes of the cooler are rectilinear and directed parallel to the axis of the cooler, and its outside wall is made of a flexible material and is capable of absorbing, with concomitant deformation of these tubes in S shape, the effects of thermal expansions of the heater in relation to the engine assembly.
3. A module as claimed in Claim 1 or 2 which is provided at the base of the cooler with a device for connection to the cold duct, this device being able to assume two different configurations offering different connection lengths.
4. A module as claimed in Claim 3, wherein the connection device is composed of a thick plate forming the base of the cooler and having an opening which is situated eccentrically relative to the axis of the cooler and brings the interior of the latter into communication with a duct formed in the thickness of the said plate perpendicularly to the said axis, by way of a bent connector housed in a cavity facing the said opening and dividing the said duct into two portions of unequal lengths, the connection to the adjacent cylinder being made either by one or by the other of these portions depending on the orientation of the bent connector relative to the said plate.
5. A module as claimed in Claim 4, wherein the eccentric opening is formed in a detachable member fitting into a recess formed in the said plate and communicating with the said cavity.
6. A module as claimed in any one of the
Claims 1 to 5, wherein the cylinder head is connected leaktightly to the casing of the corresponding cylinder, this casing forming part of the engine assembly.
7. A module as claimed in any one of the
Claims 1 to 5, wherein-the cylinder head is integral with the casing of the corresponding cylinder and the said casing is connected at its base leaktightly to the body of the engine assembly.
8. A module for Stirling engines substantially as hereinbefore described and with reference to the
Figures 3 to 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08210930A GB2118635B (en) | 1982-04-15 | 1982-04-15 | Module for forming a modular stirling engine assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08210930A GB2118635B (en) | 1982-04-15 | 1982-04-15 | Module for forming a modular stirling engine assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2118635A true GB2118635A (en) | 1983-11-02 |
| GB2118635B GB2118635B (en) | 1985-07-31 |
Family
ID=10529709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08210930A Expired GB2118635B (en) | 1982-04-15 | 1982-04-15 | Module for forming a modular stirling engine assembly |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2118635B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0174504A1 (en) * | 1984-08-11 | 1986-03-19 | Kabushiki Kaisha Toshiba | Stirling engine and stirling engine heater |
| GB2176541A (en) * | 1985-06-13 | 1986-12-31 | Sanden Corp | Stirling cycle engine |
| FR3017212A1 (en) * | 2014-02-04 | 2015-08-07 | Thierry Michel Jean Pierre Raballand | EXPERIMENTAL DEVICE FOR TESTING THE EFFICIENCY OF AN ADDITIONAL REGENERATOR (S) FOR STIRLING CYCLE THERMAL MACHINES |
| EP3364174A1 (en) | 2017-02-15 | 2018-08-22 | Christian Koller | Optical inspection system and method for visual inspection of a specimen |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB728334A (en) * | 1952-04-26 | 1955-04-20 | Philips Nv | Improvements in hot gas engines and refrigerating engines or heat pumps operating onthe reversed hot gas engine cycle |
| GB1304123A (en) * | 1971-08-27 | 1973-01-24 | ||
| GB1472703A (en) * | 1974-01-18 | 1977-05-04 | Motoren Werke Mannheim Ag | Hot gas piston engines |
| GB2051961A (en) * | 1979-06-19 | 1981-01-21 | Cmc Ab | Heater for a double-acting four-cylinder stirling engine |
-
1982
- 1982-04-15 GB GB08210930A patent/GB2118635B/en not_active Expired
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB728334A (en) * | 1952-04-26 | 1955-04-20 | Philips Nv | Improvements in hot gas engines and refrigerating engines or heat pumps operating onthe reversed hot gas engine cycle |
| GB1304123A (en) * | 1971-08-27 | 1973-01-24 | ||
| GB1472703A (en) * | 1974-01-18 | 1977-05-04 | Motoren Werke Mannheim Ag | Hot gas piston engines |
| GB2051961A (en) * | 1979-06-19 | 1981-01-21 | Cmc Ab | Heater for a double-acting four-cylinder stirling engine |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0174504A1 (en) * | 1984-08-11 | 1986-03-19 | Kabushiki Kaisha Toshiba | Stirling engine and stirling engine heater |
| US4719755A (en) * | 1984-08-11 | 1988-01-19 | Kabushiki Kaisha Toshiba | Stirling engine |
| GB2176541A (en) * | 1985-06-13 | 1986-12-31 | Sanden Corp | Stirling cycle engine |
| GB2176541B (en) * | 1985-06-13 | 1989-07-05 | Sanden Corp | Stirling cycle engine |
| FR3017212A1 (en) * | 2014-02-04 | 2015-08-07 | Thierry Michel Jean Pierre Raballand | EXPERIMENTAL DEVICE FOR TESTING THE EFFICIENCY OF AN ADDITIONAL REGENERATOR (S) FOR STIRLING CYCLE THERMAL MACHINES |
| EP3364174A1 (en) | 2017-02-15 | 2018-08-22 | Christian Koller | Optical inspection system and method for visual inspection of a specimen |
| WO2018149877A1 (en) | 2017-02-15 | 2018-08-23 | Christian Koller | Optical inspection system and method for optically inspecting a test object |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2118635B (en) | 1985-07-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |