WO2002027175A1 - Improvement in free piston stirling engines - Google Patents

Improvement in free piston stirling engines Download PDF

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Publication number
WO2002027175A1
WO2002027175A1 PCT/GB2001/004285 GB0104285W WO0227175A1 WO 2002027175 A1 WO2002027175 A1 WO 2002027175A1 GB 0104285 W GB0104285 W GB 0104285W WO 0227175 A1 WO0227175 A1 WO 0227175A1
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WO
WIPO (PCT)
Prior art keywords
displacer piston
cylinder block
spring
stirling engine
abutment
Prior art date
Application number
PCT/GB2001/004285
Other languages
French (fr)
Inventor
Roger Shuttleworth
Rabah Boukhanouf
Original Assignee
Stirling Energy Systems Limited
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Stirling Energy Systems Limited filed Critical Stirling Energy Systems Limited
Priority to AU2001290104A priority Critical patent/AU2001290104A1/en
Publication of WO2002027175A1 publication Critical patent/WO2002027175A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00Hot gas positive-displacement engine plants
    • F02G1/04Hot gas positive-displacement engine plants of closed-cycle type
    • F02G1/043Hot 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00Hot gas positive-displacement engine plants
    • F02G1/04Hot gas positive-displacement engine plants of closed-cycle type
    • F02G1/043Hot 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
    • F02G1/053Component parts or details

Definitions

  • the present invention relates to improvements in free piston Stirling engines and more particularly to a spring mounting system for the displacer piston of such an engine.
  • Stirling engines are well known in the prior art and normally comprise two reciprocating pistons, one called a displacer piston and one called a power or working piston which are coupled together by means of a crankshaft from which the power output is drawn.
  • the significant feature of a Stirling engine is that it receives heat through the wall of the cylinder (rather than internally as in an internal combustion engine) and heat is removed from the cooler of the engine. As a consequence of the resulting temperature difference between the heater and cooler, some of the thermal energy is converted into mechanical energy by the engine, appearing as output shaft rotational energy, and can be applied to a mechanical load.
  • Stirling engines comprise a two piston arrangement of a displacer piston and a working piston and Stirling engines are commonly arranged such that the displacer piston has a relatively long stroke, the stroke being larger than the diameter of the piston. This is the accepted practice for Stirling engines.
  • the Harwell Laboratories in the United Kingdom produced a Stirling engine which replaced the working piston of a normal Stirling engine with a steel diaphragm member which flexes instead of reciprocating .
  • the two pistons are not connected to any crank mechanism, but are instead typically supported from the outer casing of the engine each by a spring system.
  • the engine casing also is mounted on a spring
  • JUBST ⁇ UET ⁇ SHEET (RULE 2 ⁇ ) system typically supported by a solid base. Oscillations of the two pistons and casing occur when thermal energy is passed through the engine, producing a temperature drop between the heater and cooler of the engine as it does so.
  • the oscillations of these three components are sinusoidal and at the same frequency but are not in phase. The frequency of oscillation is determined by many factors, but is mainly a function of the displacer piston's natural frequency of operation (this in turn is a function of its mass, supporting spring stiffness and the effect of any damping forces) .
  • the frequency of oscillation and working stroke of the reciprocating power take off shaft are important as the magnitude of these parameters inversely determines the size, and hence cost, of the generator.
  • the spring support system of the displacer piston is a crucial engine component.
  • One or more spring systems may be used depending upon the design of engine, but it is usual to have three or four spring support systems for the displacer piston.
  • Each spring system must be compact to minimise dead spaces within the engine, and it is also advantageous if the spring system is cheap, simple to construct and reliable.
  • HEET RULE 6 The use of standard spiral springs offers advantages in these respects. However standard spiral springs are designed to work only in either compression or extension, but not both. In operation, the displacer piston moves in two directions (up and down the cylinder) and thus a single support spring would need to work in both compression and extension modes. Operating a standard spiral wound spring in the mode for which it is not designed will result in a varying spring stiffness (which will affect displacer piston frequency and its stroke) and may also reduce the spring's life. In addition there are difficulties associated with attachments to the end of the spring when using a standard spiral spring out of its normal operating mode.
  • the invention therefore provides a Stirling engine having a cylinder block defining a cylinder, a displacer piston located in said cylinder having a heated end and a cooled end, and at least one spring mounting means provided to mount and centre the displacer piston in the cylinder such that the displacer piston is free to oscillate in the cylinder, the spring mounting means being located at the cooled
  • SUBSTs y fc S * ki LI f-Li end of the cylinder between the cylinder and piston comprise at least two spring members arranged to bias the displacer piston towards a resting position with respect to the cylinder block, wherein the spring members are arranged such that the biassing force of one spring member counters the biassing force of the other spring member.
  • the spring members are preferably arranged in series.
  • the spring members are preferably arranged co- ⁇ axially.
  • the spring members are compression springs.
  • the cylinder block is preferably provided with at least one abutment member for at least one of the spring members and the displacer piston is provided with at least one abutment member for at least one of the spring members, wherein one of the cylinder block and displacer piston abutment members provides opposing abutment surfaces for two spring members, and in which " one spring member extends between the cylinder block and displacer piston abutment members.
  • the at least one abutment member of the displacer piston may comprise flange means extending radially outwards from the displacer piston.
  • the at least one abutment member of the displacer piston may comprise a portion of a radially extending wall of the displacer piston.
  • the at least one abutment member of the displacer piston is preferably a member projecting from a radially extending wall of the displacer piston.
  • the at least one abutment member of the displacer piston is preferably provided by a cup member having an outwardly extending radial lip providing one abutment surface and having a base defining an opposing abutment surface.
  • the at least one abutment member of the cylinder block comprises flange means extending radially inwards from the cylinder block.
  • a further abutment member is attached to a shaft, which shaft extends slidingly through one of the displacer piston or cylinder block abutment members, in which a second spring member extends between either the displacer piston abutment member or the cylinder block abutment member and the shaft abutment member to bias them apart, wherein the shaft abutment member is constrained from moving more than a predetermined distance from either the cylinder block or the displacer piston abutment member.
  • the spring member may alternatively be extension springs .
  • One spring member preferably extends between attachment means on the displacer piston and attachment means on the cylinder block, and a second spring member extends between either of said attachment means on the cylinder block or on the displacer piston and secondary attachment means on either the displacer piston or the cylinder block respectively.
  • attachment means on the displacer piston are located on a portion of a radially extending wall of the displacer piston.
  • the attachment means and/or the secondary attachment means on the displacer piston may comprise a flange member extending radially outwards from the displacer piston.
  • the attachment means on the cylinder block may be located on a flange member extending radially inwards from the cylinder block.
  • the secondary attachment means on the cylinder block are preferably located on a flange member extending radially inwards from the cylinder block.
  • Fig. 1 is a schematic cross-sectional side elevation of a Stirling engine having a free displacer piston
  • Fig. 2 is an enlarged view of the spring mounting area of Fig. 1 showing a spring mounting according to the present invention
  • Figs. 3 to 5 are alternative embodiments of the spring mounting arrangement of Fig. 2;
  • Figs. 6 and 7 are alternative embodiments of the spring mounting arrangement of Fig. 2, utilising extension instead of compression springs.
  • the Stirling engine comprises a cylindrical cylinder block 10 defining a cylinder 11.
  • a free displacer piston 12 is provided to move reciprocally in the cylinder 11.
  • a cylinder head closes off the top of the cylinder 11 and defines, with the cylinder block 10 and an upper plate of the displacer piston 12, a variable valve chamber A.
  • the cylinder head abuts a heat exchanger block 13, which is heated by means of heater tubes 14.
  • a diaphragm 16 Attached to the cylinder block 10 is a diaphragm 16, which is made of a material which is able to flex or is fully flexible
  • the diaphragm 16 defines, with the cylinder block 10 and a bottom plate of the displacer piston 12, a variable volume chamber B.
  • Coolant inlet and outlet tubes 15 are provided to enable heat removal from the cylinder and the working fluid in the manner described in GB-A-2298903.
  • a plunger is connected to the diaphragm to move with the diaphragm.
  • the plunger is connected to a linear alternator, which is located in a housing defining a bounce chamber.
  • FIG. 2 shows an enlargement of the displacer piston mounting area 17 (left hand side) .
  • the bottom plate 18 of the displacer piston 12 has a smaller diameter than that of the side walls 19.
  • the bottom plate 18 and the side wall 19 are connected by an inwardly stepped portion 20 being L-shaped in cross-section.
  • This stepped portion 20 defines, with the side walls of the cylinder block 10 defining the cylinder 11, a small annular chamber 21 in which one or more of the spring mounting systems are located.
  • the number of spring mounting systems used depends upon the design of the engine. It is preferred to have three or four spring mounting systems for each displacer piston 12.
  • a flange 22 extends from the displacer piston 12. In this embodiment the flange 22 extends radially from a first wall 20a of
  • l RULE28 the stepped portion, said first wall extending to a parallel to the displacer piston side wall 19.
  • Passing through the flange 22 is a first orifice 23, which is bordered by a lip 24 on each side of the flange 22.
  • a shaft 25, which passes through the first orifice 23, is of a diameter to allow the flange 22 to slide freely up and down the shaft 25.
  • At one end the shaft 25 is provided with an abutment flange 26, and a first compression spring 27 is located around the outside of the shaft 25 between the abutment flange 26 and the flange 22 extending from the displacer piston biassing the flanges 22, 26 apart.
  • a further flange 28 Extending radially inwards from the cylinder block 10 is a further flange 28 which, for convenience, may be stepped as shown in Fig. 2.
  • the cylinder block flange 28 is also provided with a second orifice 29 which is bordered by an annular lip 30.
  • the other end of the shaft 25 extends through this second orifice 29 and a nut 31, or other similar component, is attached to the end of the shaft 25 to prevent it from being pulled out of the second orifice 29.
  • a second compression spring 32 extends between the displacer piston flange 22 and the cylinder block flange 28, so as to bias the flanges 22, 28 away from each other.
  • each spring 27, 32 is precompressed by the action of the other and thus biassing forces, which would otherwise deflect the displacer piston 12 from its central position when at rest, are eliminated.
  • the displacer piston 12 is able to oscillate about its central position due to further compression of each springs 27, 32 alternately.
  • the displacer piston flange 22 moves up the shaft 25 causing the first spring 27 to compress against the abutment flange 26 and allowing the second spring 32 to relax.
  • Fig. 3 shows an alternative spring maintaining arrangement using two compression springs. This arrangement differs from Fig. 2 in that the component which oscillates with the movement of the displacer piston 12 is the shaft 25.
  • One end of the shaft 25 is attached to the displacer piston 12, preferably to the second wall 20b of the displacer piston stepped portion 20 which extends radially outwardly from the first wall 20a to the side wall 19.
  • the second spring 32 extends between said second wall 20b and the cylinder " block flange 28.
  • the orifice 23 in which the shaft 25 is slidably located is provided in the -cylinder block flange 28.
  • the abutment flange 26 is provided at the other end of the shaft 25, so the first spring 27 extends between the abutment flange 26 and the cylinder block flange 28.
  • FIG. 4 A further alternative arrangement is illustrated in Fig. 4. This is an arrangement which works in a similar manner to that of Fig. 3, except in that the springs 27, 32 are located coaxially, rather than in series.
  • the cylinder block flange 28 is multi-stepped so as to provide two opposing abutment surfaces 33, 34.
  • the first spring 27 extends between one abutment surface 33 and an abutment flange 26 secured to an end of the shaft 25 by the nut 31.
  • the second spring 32 extends between the other abutment surface 34 and projecting member extending from the stepped portion second wall 20b, from which the shaft 25 extends. Again, as before, each spring is precompressed by the other to eliminate the biassing forces.
  • FIG. 5 yet another alternative arrangement is shown, which is more similar in operation to the system shown in Fig. 2, except in that, again, the springs are co-axially located rather than in series.
  • the cylinder block flange 28 has an orifice 29 for receiving one end of the shaft 25, to which is attached a nut 31.
  • a cylindrical cup member 36 Surrounding the shaft 25 is a cylindrical cup member 36 which has an orifice 37 in its base bordered by an upwardly projecting lip 38.
  • a radially projecting flange 39 Surrounding the shaft 25 is a cylindrical cup member 36 which has an orifice 37 in its base bordered by an upwardly projecting lip 38.
  • a radially projecting flange 39 Around the rim of the cup member 36 is a radially projecting flange 39
  • SUBSTITUTE SHEET (RULE 28 ' which forms an abutment surface for one end of the second spring 32.
  • the other end of the second spring 32 bears against the cylinder block flange 28 biassing the flanges 28, 39 away from each other.
  • the first spring 27 extends between the base of the cup member 36 and an abutment flange 26 extending radially from the other end of the shaft 25.
  • the cup member 36 is secured to the second wall 20b of the displacer piston stepped portion 20 by means of a plurality of studs 40 having a shoulder portion.
  • the studs 40 are secured by means of nuts 41.
  • the first spring 27 is compressed as the displacer piston 12 moves upwardly, whilst the second spring 32 is compressed as it moves downwardly.
  • Fig. 6 differs from those of Figs. 2 to 5 in that extension springs are used instead of compression springs.
  • the cylinder block 10 is provided with a cylinder block flange 28 which projects radially inwardly.
  • the flange 28 preferably has a stepped configuration as shown in Fig. 6 such that a section 42 is located between adjacent ends of the first and second springs 27, 32.
  • the first spring 27 is attached at one end to the cylinder flange 28 and, at the other end, to the displacer piston 17, and preferably to a second wall 20b of the displacer piston stepped portion 20.
  • the displacer piston 17 is thereby biassed towards the cylinder block flange 28.
  • the second spring 32 extends between the cylinder block flange 28 and a flange 22 extending radially inwardly from the displacer piston 12.
  • This displacer piston flange 22 includes means for attaching the other end of the second spring 32 to it.
  • the displacer piston flange 22 is biassed by the second spring 32 towards the cylinder block flange 28.
  • Each spring 27, 32 is pre-extended by the other, thus eliminating the biassing forces which would deflect
  • SUBSTITUTE SHEET (RULE 26 ' the displacer piston 17 from its central position at rest. As the displacer piston 17 moves upwardly the first spring 27 extends and the second spring 32 relaxes. As the piston 17 moves downwardly, the first spring 27 relaxes and the second spring 32 extends.
  • two extension springs 27, 32 are again used.
  • the displacer piston flange 22 is located at a position between the adjacent ends of each spring 27, 32, and one end of each spring 27, 32 is attached thereto.
  • the other end of the first spring 27 is attached to one extension 42a of the cylinder block flange 28, which is located on one side of the spring system (in proximity to the second wall 20b of the displacer piston stepped portion 20) .
  • the cylinder block flange 28 has a second extension 42b, which is located on the other side of the spring system such that the other end of the second spring 32 is attached thereto by appropriate means 43.
  • the other spring relaxes and vice versa.
  • the use of the nuts 31, 43 in the above-mentioned embodiments advantageously allow the adjustment of the displacer piston 12 centre position.
  • the nuts 31, 43 also provide control over the alignment of the displacer piston 12 within the cylinder 11.
  • the ends are ground flat and parallel. These ground ends also help to maintain the alignment of the displacer piston 12 in the cylinder 11.

Abstract

The present invention relates to improvements in free piston Stirling engines and more particularly to a spring mounting system for the displace piston (12) of such an engine. A Stirling engine having a cylinder block (10) defining a cylinder (11) a displacer piston (12) located in said cylinder (11) having a heated end and a cooled end, and at least one spring mounting means provided to mount and centre the displacer piston (12) in the cylinder such that the displacer piston (12) is free to oscillate in the cylinder in response to a pressure differential across the displacer piston (12), or other perturbing force, the spring mounting means (17) being located at the cooled end of the cylinder (11) between the cylinder (11) and the piston (12) comprise at least two spring members arranged.

Description

IMPROVEMENT IN FREE PISTON STIRLING ENGINES
The present invention relates to improvements in free piston Stirling engines and more particularly to a spring mounting system for the displacer piston of such an engine.
Stirling engines are well known in the prior art and normally comprise two reciprocating pistons, one called a displacer piston and one called a power or working piston which are coupled together by means of a crankshaft from which the power output is drawn. The significant feature of a Stirling engine is that it receives heat through the wall of the cylinder (rather than internally as in an internal combustion engine) and heat is removed from the cooler of the engine. As a consequence of the resulting temperature difference between the heater and cooler, some of the thermal energy is converted into mechanical energy by the engine, appearing as output shaft rotational energy, and can be applied to a mechanical load.
The majority of Stirling engines comprise a two piston arrangement of a displacer piston and a working piston and Stirling engines are commonly arranged such that the displacer piston has a relatively long stroke, the stroke being larger than the diameter of the piston. This is the accepted practice for Stirling engines.
The Harwell Laboratories in the United Kingdom produced a Stirling engine which replaced the working piston of a normal Stirling engine with a steel diaphragm member which flexes instead of reciprocating .
In a Harwell type of free piston Stirling engine the two pistons are not connected to any crank mechanism, but are instead typically supported from the outer casing of the engine each by a spring system. The engine casing also is mounted on a spring
JUBSTΠUETΞ SHEET (RULE 2β) system typically supported by a solid base. Oscillations of the two pistons and casing occur when thermal energy is passed through the engine, producing a temperature drop between the heater and cooler of the engine as it does so. The oscillations of these three components are sinusoidal and at the same frequency but are not in phase. The frequency of oscillation is determined by many factors, but is mainly a function of the displacer piston's natural frequency of operation (this in turn is a function of its mass, supporting spring stiffness and the effect of any damping forces) .
Mechanical energy can be directly drawn from either of the pistons, or the casing. However, the mechanical energy is in the form of reciprocating motion. Furthermore as the power output of the engine changes so the amplitude of the reciprocating motion changes. Because it is difficult to efficiently convert variable amplitude reciprocating shaft movement to a rotational form, the reciprocating power take off shaft is usually arranged to drive a linear generator directly.
The frequency of oscillation and working stroke of the reciprocating power take off shaft are important as the magnitude of these parameters inversely determines the size, and hence cost, of the generator. Thus it is usual to take the shaft power from the power piston, which is designed to have the largest stroke of the three components. The spring support system of the displacer piston is a crucial engine component. One or more spring systems may be used depending upon the design of engine, but it is usual to have three or four spring support systems for the displacer piston. Each spring system must be compact to minimise dead spaces within the engine, and it is also advantageous if the spring system is cheap, simple to construct and reliable.
HEET RULE 6 The use of standard spiral springs offers advantages in these respects. However standard spiral springs are designed to work only in either compression or extension, but not both. In operation, the displacer piston moves in two directions (up and down the cylinder) and thus a single support spring would need to work in both compression and extension modes. Operating a standard spiral wound spring in the mode for which it is not designed will result in a varying spring stiffness (which will affect displacer piston frequency and its stroke) and may also reduce the spring's life. In addition there are difficulties associated with attachments to the end of the spring when using a standard spiral spring out of its normal operating mode.
For this reason if standard spiral wound springs are to be used they must be prestressed so that they only operate in the mode for which they are specified. Thus if extension springs are used, they must be prestressed by extending them a pre-determined amount, sufficient that the maximum movement of the displacer piston does not allow them to reach their free unextended length. Similarly, if compression springs are used they must be sufficiently precompressed so that full movement of the displacer piston does not cause them to reach their free length.
It is an object of the present invention therefore to provide a spring mounting system for the displacer piston to overcome these problems. The invention therefore provides a Stirling engine having a cylinder block defining a cylinder, a displacer piston located in said cylinder having a heated end and a cooled end, and at least one spring mounting means provided to mount and centre the displacer piston in the cylinder such that the displacer piston is free to oscillate in the cylinder, the spring mounting means being located at the cooled
SUBSTs y fc S *ki LI f-Li end of the cylinder between the cylinder and piston comprise at least two spring members arranged to bias the displacer piston towards a resting position with respect to the cylinder block, wherein the spring members are arranged such that the biassing force of one spring member counters the biassing force of the other spring member.
The spring members are preferably arranged in series.
The spring members are preferably arranged co- ϊ axially.
In a preferred embodiment the spring members are compression springs.
The cylinder block is preferably provided with at least one abutment member for at least one of the spring members and the displacer piston is provided with at least one abutment member for at least one of the spring members, wherein one of the cylinder block and displacer piston abutment members provides opposing abutment surfaces for two spring members, and in which "one spring member extends between the cylinder block and displacer piston abutment members.
The at least one abutment member of the displacer piston may comprise flange means extending radially outwards from the displacer piston.
The at least one abutment member of the displacer piston may comprise a portion of a radially extending wall of the displacer piston.
The at least one abutment member of the displacer piston is preferably a member projecting from a radially extending wall of the displacer piston.
The at least one abutment member of the displacer piston is preferably provided by a cup member having an outwardly extending radial lip providing one abutment surface and having a base defining an opposing abutment surface.
The at least one abutment member of the cylinder block comprises flange means extending radially inwards from the cylinder block.
Preferably a further abutment member is attached to a shaft, which shaft extends slidingly through one of the displacer piston or cylinder block abutment members, in which a second spring member extends between either the displacer piston abutment member or the cylinder block abutment member and the shaft abutment member to bias them apart, wherein the shaft abutment member is constrained from moving more than a predetermined distance from either the cylinder block or the displacer piston abutment member.
The spring member may alternatively be extension springs . "
One spring member preferably extends between attachment means on the displacer piston and attachment means on the cylinder block, and a second spring member extends between either of said attachment means on the cylinder block or on the displacer piston and secondary attachment means on either the displacer piston or the cylinder block respectively.
Preferably the attachment means on the displacer piston are located on a portion of a radially extending wall of the displacer piston.
The attachment means and/or the secondary attachment means on the displacer piston may comprise a flange member extending radially outwards from the displacer piston.
The attachment means on the cylinder block may be located on a flange member extending radially inwards from the cylinder block.
The secondary attachment means on the cylinder block are preferably located on a flange member extending radially inwards from the cylinder block.
The invention will now be described, by way of example only, with reference to the accompanying drawings in which: -
Fig. 1 is a schematic cross-sectional side elevation of a Stirling engine having a free displacer piston;
Fig. 2 is an enlarged view of the spring mounting area of Fig. 1 showing a spring mounting according to the present invention;
Figs. 3 to 5 are alternative embodiments of the spring mounting arrangement of Fig. 2; and
Figs. 6 and 7 are alternative embodiments of the spring mounting arrangement of Fig. 2, utilising extension instead of compression springs.
Referring first to Fig. 1 the Stirling engine comprises a cylindrical cylinder block 10 defining a cylinder 11. A free displacer piston 12 is provided to move reciprocally in the cylinder 11.
A cylinder head closes off the top of the cylinder 11 and defines, with the cylinder block 10 and an upper plate of the displacer piston 12, a variable valve chamber A. The cylinder head abuts a heat exchanger block 13, which is heated by means of heater tubes 14.
Attached to the cylinder block 10 is a diaphragm 16, which is made of a material which is able to flex or is fully flexible The diaphragm 16 defines, with the cylinder block 10 and a bottom plate of the displacer piston 12, a variable volume chamber B.
Coolant inlet and outlet tubes 15 are provided to enable heat removal from the cylinder and the working fluid in the manner described in GB-A-2298903.
A plunger is connected to the diaphragm to move with the diaphragm. The plunger is connected to a linear alternator, which is located in a housing defining a bounce chamber.
Referring now to Fig. 2, this shows an enlargement of the displacer piston mounting area 17 (left hand side) . The bottom plate 18 of the displacer piston 12 has a smaller diameter than that of the side walls 19. The bottom plate 18 and the side wall 19 are connected by an inwardly stepped portion 20 being L-shaped in cross-section. This stepped portion 20 defines, with the side walls of the cylinder block 10 defining the cylinder 11, a small annular chamber 21 in which one or more of the spring mounting systems are located. The number of spring mounting systems used depends upon the design of the engine. It is preferred to have three or four spring mounting systems for each displacer piston 12. For each spring system, a flange 22 extends from the displacer piston 12. In this embodiment the flange 22 extends radially from a first wall 20a of
l RULE28) the stepped portion, said first wall extending to a parallel to the displacer piston side wall 19. Passing through the flange 22 is a first orifice 23, which is bordered by a lip 24 on each side of the flange 22. A shaft 25, which passes through the first orifice 23, is of a diameter to allow the flange 22 to slide freely up and down the shaft 25. At one end the shaft 25 is provided with an abutment flange 26, and a first compression spring 27 is located around the outside of the shaft 25 between the abutment flange 26 and the flange 22 extending from the displacer piston biassing the flanges 22, 26 apart.
Extending radially inwards from the cylinder block 10 is a further flange 28 which, for convenience, may be stepped as shown in Fig. 2. The cylinder block flange 28 is also provided with a second orifice 29 which is bordered by an annular lip 30. The other end of the shaft 25 extends through this second orifice 29 and a nut 31, or other similar component, is attached to the end of the shaft 25 to prevent it from being pulled out of the second orifice 29. A second compression spring 32 extends between the displacer piston flange 22 and the cylinder block flange 28, so as to bias the flanges 22, 28 away from each other.
The lips 24, 30 act as position locators for the springs 27, 32, although any other locator means may be provided. Appropriate location means are preferably provided on the abutment flange 26 also. In this arrangement each spring 27, 32 is precompressed by the action of the other and thus biassing forces, which would otherwise deflect the displacer piston 12 from its central position when at rest, are eliminated. However when the engine is running the displacer piston 12 is able to oscillate about its central position due to further compression of each springs 27, 32 alternately. As the piston 12 moves upwardly (when the engine is in the orientation of Fig. 1), the displacer piston flange 22 moves up the shaft 25 causing the first spring 27 to compress against the abutment flange 26 and allowing the second spring 32 to relax. As the piston 12 moves downwardly, so does the flange 22, thereby compressing the second spring 32. The shaft 25 may also be reversed so that the nut 31 is at the top, and flange 26 is on the other side of orifice 29. Although the invention is described with reference to oscillation of the displacer piston in response to a pressure differential across the displacer piston, it could be effected by another perturbing force. Fig. 3 shows an alternative spring maintaining arrangement using two compression springs. This arrangement differs from Fig. 2 in that the component which oscillates with the movement of the displacer piston 12 is the shaft 25. One end of the shaft 25 is attached to the displacer piston 12, preferably to the second wall 20b of the displacer piston stepped portion 20 which extends radially outwardly from the first wall 20a to the side wall 19. The second spring 32 extends between said second wall 20b and the cylinder "block flange 28. The orifice 23 in which the shaft 25 is slidably located is provided in the -cylinder block flange 28. The abutment flange 26 is provided at the other end of the shaft 25, so the first spring 27 extends between the abutment flange 26 and the cylinder block flange 28. This arrangement operates in a similar way as that shown in Fig. 2, whereby upward movement of the displacer piston 12 causes the shaft 25 to move upwards thereby causing the first spring 27 to be compressed between abutment flange 26 and cylinder block flange 28, whilst the second spring 32 relaxes. When the piston 12 moves downwardly, the second spring 32 is compressed and the first spring 27 relaxes, maintaining the overall force between the stepped portion second wall 20b and the abutment flange 26.
A further alternative arrangement is illustrated in Fig. 4. This is an arrangement which works in a similar manner to that of Fig. 3, except in that the springs 27, 32 are located coaxially, rather than in series. In this arrangement, the cylinder block flange 28 is multi-stepped so as to provide two opposing abutment surfaces 33, 34. Thus the first spring 27 extends between one abutment surface 33 and an abutment flange 26 secured to an end of the shaft 25 by the nut 31. The second spring 32 extends between the other abutment surface 34 and projecting member extending from the stepped portion second wall 20b, from which the shaft 25 extends. Again, as before, each spring is precompressed by the other to eliminate the biassing forces. As the displacer piston 12 moves upwardly, so does the shaft 25 causing the first spring 27 to be compressed between the abutment flange 26 and the abutment surface 33 of the cylinder block flange 28 whilst the second spring 32 relaxes. When the piston 12 moves downward, the reverse occurs, substantially as described in connection with Fig. 3.
Referring now to Fig. 5, yet another alternative arrangement is shown, which is more similar in operation to the system shown in Fig. 2, except in that, again, the springs are co-axially located rather than in series. In this arrangement, as in Fig. 2, the cylinder block flange 28 has an orifice 29 for receiving one end of the shaft 25, to which is attached a nut 31.
Surrounding the shaft 25 is a cylindrical cup member 36 which has an orifice 37 in its base bordered by an upwardly projecting lip 38. Around the rim of the cup member 36 is a radially projecting flange 39
SUBSTITUTE SHEET (RULE 28' which forms an abutment surface for one end of the second spring 32. The other end of the second spring 32 bears against the cylinder block flange 28 biassing the flanges 28, 39 away from each other. The first spring 27 extends between the base of the cup member 36 and an abutment flange 26 extending radially from the other end of the shaft 25. The cup member 36 is secured to the second wall 20b of the displacer piston stepped portion 20 by means of a plurality of studs 40 having a shoulder portion. The studs 40 are secured by means of nuts 41. Again, the first spring 27 is compressed as the displacer piston 12 moves upwardly, whilst the second spring 32 is compressed as it moves downwardly. The arrangement of Fig. 6 differs from those of Figs. 2 to 5 in that extension springs are used instead of compression springs. In this arrangement, for each spring system, the cylinder block 10 is provided with a cylinder block flange 28 which projects radially inwardly. The flange 28 preferably has a stepped configuration as shown in Fig. 6 such that a section 42 is located between adjacent ends of the first and second springs 27, 32. The first spring 27 is attached at one end to the cylinder flange 28 and, at the other end, to the displacer piston 17, and preferably to a second wall 20b of the displacer piston stepped portion 20. The displacer piston 17 is thereby biassed towards the cylinder block flange 28.- The second spring 32 extends between the cylinder block flange 28 and a flange 22 extending radially inwardly from the displacer piston 12. This displacer piston flange 22 includes means for attaching the other end of the second spring 32 to it. Thus, the displacer piston flange 22 is biassed by the second spring 32 towards the cylinder block flange 28. Each spring 27, 32 is pre-extended by the other, thus eliminating the biassing forces which would deflect
SUBSTITUTE SHEET (RULE 26' the displacer piston 17 from its central position at rest. As the displacer piston 17 moves upwardly the first spring 27 extends and the second spring 32 relaxes. As the piston 17 moves downwardly, the first spring 27 relaxes and the second spring 32 extends.
In an alternative embodiment shown in Fig. 7, two extension springs 27, 32 are again used. However in this case the displacer piston flange 22 is located at a position between the adjacent ends of each spring 27, 32, and one end of each spring 27, 32 is attached thereto. The other end of the first spring 27 is attached to one extension 42a of the cylinder block flange 28, which is located on one side of the spring system (in proximity to the second wall 20b of the displacer piston stepped portion 20) . The cylinder block flange 28 has a second extension 42b, which is located on the other side of the spring system such that the other end of the second spring 32 is attached thereto by appropriate means 43. As before, as one spring extends under movement of the piston 12, the other spring relaxes and vice versa.
Some of the aforegoing configurations advantageously have minimum mass attached to the displacer piston 12, since in practical designs the weight of the displacer piston 12 is minimised.
The use of the nuts 31, 43 in the above-mentioned embodiments advantageously allow the adjustment of the displacer piston 12 centre position. The nuts 31, 43 also provide control over the alignment of the displacer piston 12 within the cylinder 11.
In the embodiments of the invention utilising compression springs, the ends are ground flat and parallel. These ground ends also help to maintain the alignment of the displacer piston 12 in the cylinder 11.

Claims

CLAIMS :
1. A Stirling engine having a cylinder block defining a cylinder a displacer piston located in said cylinder having a heated end and a cooled end, and at least one spring mounting means provided to mount and centre the displacer piston in the cylinder such that the displacer piston is free to oscillate in the cylinder in response to a pressure differential across the displacer piston, or other perturbing force, the spring mounting means being located at the cooled end of the cylinder between the cylinder and the piston comprise at least two spring members arranged to bias the displacer piston towards a resting position centred with respect to the cylinder block, wherein the spring members pre-compressed spring members or pre-extended tension spring mounting arranged such that the biassing force of one spring member counters the biassing force of the other spring member.
2. A Stirling engine as claimed in claim 1 in which the spring members are arranged in series.
3. A Stirling engine as claimed in claim 1 in which the spring members are arranged co-axially.
4. A Stirling engine as claimed in claim 1 in which the spring members are compression springs.
5. A Stirling engine as claimed in claim 4 in which the ends of the compression springs are flat and parallel .
6. A Stirling engine as claimed in any one of the preceding claims in which the cylinder block is provided with at least one abutment member for at least one of the spring members and the displacer piston is provided with at least one abutment member for at least one of the spring members, wherein one of the cylinder block and displacer piston abutment members provides opposing abutment surfaces for two spring members, and in which one sprig member extends between the cylinder block and displacer piston abutment members .
7. A Stirling engine as claimed in any one of the preceding claims in which the at least one abutment member of the displacer piston comprises flange means extending radially outwards from the displacer piston.
8. A Stirling engine as claimed in any one of claims 1 to 6 in which the at least one abutment member of the displacer piston comprises a portion of a radially extending wall of the displacer piston.
9. A Stirling engine as claimed in any one of claims 1 to 6 in which the at least one abutment member of the displacer piston is a member projecting from a radially extending wall of the displacer piston.
10. A Stirling engine as claimed in claim 9 in which the at least one abutment member of the displacer piston is provided by a cup member having an outwardly extending radial lip providing one abutment surface and having a base providing an opposing abutment surface.
11. A Stirling engine as claimed in any one of the preceding claims in which the at least one abutment member of the cylinder block comprises flange means extending radially inwards from the cylinder block.
12. A Stirling engine as claimed in any one of claims 6 to 11 comprising a further abutment member attached to a shaft, which shaft extends slidingly through one of the displacer piston or cylinder block abutment members, in which a second spring member extends between either the displacer piston abutment member or j the cylinder block abutment member and the shaft abutment member to bias them apart, wherein the shaft abutment member is constrained from moving more than a predetermined distance from either the cylinder block or the displacer piston abutment member.
13. A Stirling engine as claimed in claim 1 or claim 2 wherein the spring members are extension springs.
14. A Stirling engine as claimed in claim 13 in which one spring member extends between attachment means on the displacer piston and attachment means on the cylinder block, and a second spring member extends between either of said attachment means on the cylinder block or on the displacer piston and secondary attachment means on either the displacer piston or the cylinder block respectively.
15. A Stirling engine as claimed in claim 14 in which the attachment means on the displacer piston are located o"n a portion of a radially extending wall of the displacer piston.
16. A Stirling engine as claimed in claim 14 or claim 15 in which the attachment means and/or the secondary attachment means on the displacer piston comprise a flange member extending radially outwards from the displacer piston.
17. A Stirling engine as claimed in any one of claims 14 to 16 in which the attachment means on the cylinder block are located on a flange member extending radially inwards from the cylinder block.
18. A Stirling engine as claimed in any one of claims 14 to 17 in which the secondary attachment means on the cylinder block are located on a flange member extending radially inwards from the cylinder block.
19. A Stirling engine as claimed in any one of the preceding claims in which the centre position of the displacer piston is adjustable.
20. A Stirling engine substantially as hereinbefore described with reference to and as shown in the accompanying drawings.
'
PCT/GB2001/004285 2000-09-26 2001-09-26 Improvement in free piston stirling engines WO2002027175A1 (en)

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AU2001290104A AU2001290104A1 (en) 2000-09-26 2001-09-26 Improvement in free piston stirling engines

Applications Claiming Priority (2)

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GB0023579.6 2000-09-26
GB0023579A GB2367335B (en) 2000-09-26 2000-09-26 Improvement in free piston stirling engines

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WO2018200062A1 (en) * 2017-04-24 2018-11-01 Sunpower, Inc. Attachment of cylinders in the housing of free-piston stirling machines
CN112815565A (en) * 2021-01-28 2021-05-18 宁波芯斯特林低温设备有限公司 Stirling refrigerator

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GB0218740D0 (en) * 2002-08-12 2002-09-18 Bg Intellectual Pty Ltd A wall mounted domestic combined heat and power appliance
US20220392657A1 (en) * 2021-06-03 2022-12-08 Battelle Energy Alliance, Llc Energy production devices and associated components, and related heat transfer devices and methods

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US4385615A (en) 1979-10-05 1983-05-31 Fuel Dimensions, Inc. Fuel system for diesel engines
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US5349823A (en) * 1992-02-14 1994-09-27 Intel Corporation Integrated refrigerated computer module
GB2298903A (en) * 1995-03-17 1996-09-18 Auckland David W Stirling engine with sprung displacer and flexible diaphragm
US5813234A (en) * 1995-09-27 1998-09-29 Wighard; Herbert F. Double acting pulse tube electroacoustic system

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US4385615A (en) 1979-10-05 1983-05-31 Fuel Dimensions, Inc. Fuel system for diesel engines
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US5349823A (en) * 1992-02-14 1994-09-27 Intel Corporation Integrated refrigerated computer module
GB2298903A (en) * 1995-03-17 1996-09-18 Auckland David W Stirling engine with sprung displacer and flexible diaphragm
US5813234A (en) * 1995-09-27 1998-09-29 Wighard; Herbert F. Double acting pulse tube electroacoustic system

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018200062A1 (en) * 2017-04-24 2018-11-01 Sunpower, Inc. Attachment of cylinders in the housing of free-piston stirling machines
US10156204B2 (en) 2017-04-24 2018-12-18 Sunpower, Inc. Attachment of cylinders in the housing of free-piston stirling machines
CN112815565A (en) * 2021-01-28 2021-05-18 宁波芯斯特林低温设备有限公司 Stirling refrigerator

Also Published As

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GB2367335A (en) 2002-04-03
GB0023579D0 (en) 2000-11-08
GB2367335B (en) 2002-08-28
AU2001290104A1 (en) 2002-04-08

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