LABYRINTH PISTON COMPRESSOR

Abstract

The labyrinth piston compressor comprises a cylinder, a piston disposed in the cylinder, and a piston rod, wherein the piston rod extends in a longitudinal direction (L) and is connected to the piston, and wherein the piston is reciprocally movable in the longitudinal direction (L) within the cylinder, wherein the cylinder comprises a first cylinder cover, wherein an inlet valve and an outlet valve are arranged in the first cylinder cover, and wherein the inlet valve and the outlet valve are arranged symmetrically with respect to a plane of symmetry (S) extending in the longitudinal direction (L) along the piston rod.

Claims

1. A labyrinth piston compressor comprising a cylinder, a piston disposed in the cylinder, and a piston rod, wherein the piston rod extends in a longitudinal direction (L) and is connected to the piston, and wherein the piston is reciprocally movable within the cylinder in the longitudinal direction (L), wherein the cylinder comprises a first cylinder cover, wherein an inlet valve and an outlet valve are arranged in the first cylinder cover, and wherein the inlet valve and the outlet valve are arranged symmetrically with respect to a plane of symmetry (S) extending in the longitudinal direction (L) along the piston rod, wherein the inlet valve and the outlet valve are arranged in the cylinder cover so as to extend inclinedly with respect to the plane of symmetry (S).

2. Labyrinth piston compressor according to claim 1, wherein the cylinder comprises a second cylinder cover, wherein also in the second cylinder cover an inlet valve as well as an outlet valve are arranged symmetrically with respect to the plane of symmetry (S), and wherein the cylinder and the piston are thus designed double-acting.

3. Labyrinth piston compressor according to claim 1, wherein at least one of the cylinder and/or the piston is made of a metal with a thermal conductivity in the range between 100 and 300 (W/m.Math.K).

4. Labyrinth piston compressor according to claim 1, wherein the second cylinder cover is connected to a carrier housing via a spacer and is held at a distance from the carrier housing by the spacer, and wherein the spacer comprises at least two support arms which are arranged symmetrically with respect to the plane of symmetry (S), run in the longitudinal direction (L) and are connected to the second cylinder cover.

5. Labyrinth piston compressor according to claim 4, wherein the second cylinder cover has attachment points arranged on its outer edge, to which the support arms are fastened, and wherein the attachment points are arranged symmetrically with respect to the plane of symmetry (S).

6. Labyrinth piston compressor according to claim 5, wherein the spacer is U-shaped, with two support arms extending in the longitudinal direction (L), and the second cylinder cover has two attachment points.

7. Labyrinth piston compressor according to claim 5, wherein each attachment point has a width (C) in the circumferential direction of the second cylinder cover in the range between 10° and 30°.

8. Labyrinth piston compressor according to claim 1, wherein a flange leading to the outside is arranged in the fluid flow direction (F) of a conveyed fluid directly before the inlet valve or in the fluid flow direction (F) directly after the outlet valve, in order to feed the fluid to the cylinder from the outside or in order to discharge the fluid from the cylinder to the outside.

9. Labyrinth piston compressor according to claim 1, wherein the cylinder comprises at least three parts, the first cylinder cover, the second cylinder cover and a cylinder jacket, the cylinder jacket being arranged between the first cylinder cover and the second cylinder cover.

10. Labyrinth piston compressor according to claim 1, wherein the piston-comprises at least three parts, a first piston cover, a second piston cover and a piston skirt arranged between the first and second piston covers, the piston skirt having at least partially a labyrinth-shaped outer surface.

11. Labyrinth piston compressor according to claim 10, wherein at least one of the two piston covers has a piston end face, which projects towards the associated cylinder cover, and wherein the associated cylinder cover has a correspondingly projecting cylinder cover outer side or a correspondingly receding cylinder cover inner side with respect to the piston end face.

12. Labyrinth piston compressor according to claim 1, wherein the second cylinder cover has in its center a passage opening extending in the longitudinal direction (L), along which the piston rod extends, at least one gland chamber being arranged in the longitudinal direction (L) downstream of the passage opening, outside the cylinder cover.

13. Labyrinth piston compressor according to claim 1, wherein at least one of the inlet valve, the outlet valve and the flange rests only partially on the first or second cylinder cover in order to increase the thermal resistance between the inlet valve, the outlet valve, the flange and the first or second cylinder cover.

14. Labyrinth piston compressor according to claim 4, wherein a plurality of cylinders with pistons arranged therein are arranged on a common carrier housing and are driven by a common crankshaft arranged in the carrier housing.

15. Labyrinth piston according to claim 3, wherein the metal is aluminum or an aluminum alloy.

16. Labyrinth piston according to claim 5, wherein the attachment points are arranged substantially perpendicular to the plane of symmetry (S).

17. Labyrinth piston according to claim 9, wherein the cylinder jacket is tubular.

18. Labyrinth piston according to claim 11, wherein the piston end face is convex.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The drawings used to explain the embodiments show:

[0018] FIG. 1 a longitudinal section through a reciprocating compressor along section line A-A;

[0019] FIG. 2 a detailed view of the piston compressor according to FIG. 1, in particular the cylinder and the piston;

[0020] FIG. 3 a detailed view of the arrangement of the valve in the cylinder;

[0021] FIG. 4 a side view of the cylinder with spacer;

[0022] FIG. 5 another side view of the cylinder with spacer;

[0023] FIG. 6 a longitudinal section through the cylinder with piston along section line A-A;

[0024] FIG. 7 another longitudinal section through the cylinder with piston along section line B-B;

[0025] FIG. 8 a side view of the reciprocating compressor;

[0026] FIG. 9 the reciprocating compressor in an application configuration.

[0027] In principle, the same parts are given the same reference signs in the drawings.

DETAILED DESCRIPTION

[0028] FIG. 1 shows a longitudinal section through a reciprocating compressor 1 comprising a cylinder 10 and a piston 20 arranged therein, comprising a carrier housing 60 with a crosshead 63 arranged therein with bearing part 63a, the crosshead 63 being drivable via a crankshaft 61 and a connecting rod 62, and comprising a spacer 40 with support section 41, the spacer 40 connecting the cylinder 10 to the carrier housing 60 and, as shown in FIG. 1, supporting the cylinder 10 when the reciprocating compressor 1 is arranged upright. The reciprocating compressor 1 includes a piston rod 24 that connects the crosshead 63 to the piston 20 and drives the piston 20. The reciprocating compressor 1 has a longitudinal axis L which extends along the center of the piston rod 24. The cylinder 10 includes a first cylinder cover 11, a second cylinder cover 12, and a cylinder jacket 13 disposed therebetween. The first cylinder cover 11 includes an intake valve receiving opening 11a and an exhaust valve receiving opening 11b, in which an intake valve 90 and an exhaust valve 91 are disposed, respectively. In addition, a flange 14 is connected to each of the openings 11a, 11b, the flange 14 being used to supply or remove a fluid between outside the cylinder 10 and an interior 10a of the cylinder 10. Fluids can be supplied or removed, for example, via a hose 15 connected to the respective flange 14. The second cylinder cover 12 also comprises an intake valve receiving opening 12a and an exhaust valve receiving opening 12b with intake valve 90 and exhaust valve 91 arranged therein, respectively. The second cylinder cover 12 comprises a central portion 12h having a passage opening 12g in which the piston rod 24 is arranged movably in the direction L of its travel. The cylinder 10 or the piston 20 is double-acting, in which the piston 20 defines a first cylinder interior 10a and a second cylinder interior 10b. In another embodiment, the cylinder jacket 13 could be dispensed with by making the first and second cylinder covers 11, 12 longer in the longitudinal direction L.

[0029] In the longitudinal direction L, a first, a second and a third stuffing box chamber 50, 51. 52 are arranged downstream of the center section 12h. The first, second and third stuffing box chamber 50, 51. 52 are arranged downstream of the center section 12. The spacer 40 has a spacer interior 40a in which an oil scraper packing 55, shown only schematically, is arranged, preferably comprising a guide which encloses the piston rod 24. In addition, an oil screen 54 is arranged on the piston rod 24. The support housing 60 includes a bore 60a that forms a sliding surface for the crosshead 63 so that the crosshead 63, the piston rod 24 connected to the crosshead 63, and the piston 20 connected to the piston rod 24 can reciprocate in the longitudinal direction L. Preferably, the sliding surface for the crosshead is lubricated, preferably with oil, although this lubrication is not shown in detail.

[0030] The cylinder 10 and/or the piston 20, and preferably also the carrier housing 60 and the crosshead 63, are made of a metal having a thermal conductivity in the range of preferably between 100 and 300 (W/m.Math.K), preferably aluminum or an aluminum alloy. Advantageously, the cylinder 10 and the piston 20, and preferably also the carrier housing 60 and the crosshead 63, are made of the same material so that they have the same properties with regard to thermal expansion.

[0031] FIG. 2 shows a detailed view of the piston compressor 1 according to FIG. 1, essentially the cylinder 10, the piston 20, the flanges 14 and the inlet and outlet valves 90, 91. In one possible embodiment, the cylinder 10 and the piston 20 are single-acting in that, for example, only one inlet valve 90 and one outlet valve 91 are arranged in the first cylinder cover 11. Particularly advantageously, however, the cylinder 10 and the piston 20 are of double-acting design, as shown in FIG. 2, with a first cylinder interior 10a, a second cylinder interior 10b and two inlet valves 90 and two outlet valves 91. According to the invention, an inlet valve 90 and an outlet valve 91 are thus arranged at least in the first cylinder cover 11 or in the second cylinder cover 12, and preferably an inlet valve 90 and an outlet valve 91 are arranged in each of the two cylinder covers 11, 12, as shown in FIG. 2. In the respective cylinder cover 11, 12, the inlet valve 90 and the outlet valve 91 are preferably arranged symmetrically with respect to a plane of symmetry S extending in the longitudinal direction L along the piston rod 24. Preferably, both inlet valves 90 and both exhaust valves 91 are arranged on the same side of the cylinder 10 as shown in FIG. 2, i.e. both to the left and both to the right of the plane of symmetry S, respectively, as shown in FIG. 2.

[0032] The reciprocating compressor according to the invention is particularly suitable for compressing a fluid whose inlet fluid FE flowing in via the inlet valve 90 and whose outlet fluid FA flowing out via the outlet valve 91 have a high temperature difference of, for example, between 100° C. to 150° C. For example, the inlet fluid FE, for example exhaust gas of liquefied natural gas, may have a temperature of −160° C., and the outlet fluid FA may have a temperature of −40° C., so that it has a temperature difference of 120° C. The symmetrical arrangement of inlet valve 90 and exhaust valve 91 with respect to the plane of symmetry S has the advantage that the cylinder 10 as well as the piston 20 assume an average temperature during operation in the region of the plane of symmetry S and the longitudinal axis L extending along the piston rod 24, respectively, the temperature of the cylinder 10 and of the piston 20 perpendicular to the longitudinal axis L usually decreasing towards the inlet valve 90 and increasing towards the exhaust valve 91. In the direction of the longitudinal axis L, the cylinder 10 preferably exhibits only small temperature differences. Since the cylinder 10 and the piston 20 have an average temperature in the area of the longitudinal axis L during operation, the cylinder 10, the piston 20 and the piston rod 24 experience no or negligible distortion caused by temperature differences in these parts or changes in length caused by temperature differences. In an advantageous embodiment, the cylinder 10 and/or the piston 20 are made of a material with good thermal conductivity, for example aluminum, which gives the advantage of reducing the temperature differences applied to the cylinder 10 and the piston 20 during operation.

[0033] The piston compressor according to the invention is advantageously operated at ambient temperature. If the reciprocating compressor according to the invention is used to compress exhaust gas from liquid natural gas, the outer surface of the cylinder 10 is heated with air at ambient temperature, which further reduces temperature differences applied to the cylinder 10, especially if the cylinder 10 or at least the cylinder covers 11, 12 are made of a material that conducts heat well.

[0034] In a reciprocating compressor 1, a gas space is understood to be the space between a fluid supply line 15 and the inlet valve 90 or the space between the outlet valve 91 and a fluid discharge line 16. The piston compressor 1 according to the invention advantageously has no or a very small gas space, in that the fluid supply line 15 or a flange 14 is arranged in the fluid flow direction F directly upstream of the inlet valve 90, via which the fluid is supplied to the cylinder 10 from the outside, or in that a fluid discharge line 16 or a flange 14 is arranged in the fluid flow direction F directly downstream of the outlet valve 91, via which the fluid is discharged from the cylinder 10 to the outside. Thus, the pumped fluid is no longer in direct heat-conducting contact with the cylinder 10 until immediately upstream of the inlet valve 90 or immediately downstream of the outlet valve 91. As a result, the cylinder 10 is cooled to a lesser depth.

[0035] In a further advantageous embodiment, at least one of the components inlet valve 90, outlet valve 91 and flange 14 are designed in such a way that they have an increased thermal resistance to the cylinder cover 11, 12 in order to extract heat from the cylinder cover 11, 12 only to a reduced extent due to the cool fluid flowing through the inlet valve 90, the outlet valve 91 and/or the flange 14. FIG. 3 shows a detailed view of an embodiment for increasing the thermal resistance. The exhaust valve 91 is not in full contact with the first cylinder cover 11 but only over part of its surface 91a, which increases the thermal resistance between the exhaust valve 91 and the first cylinder cover 11. In the same way, the inlet valve 90 could also be arranged in the first or second cylinder cover 11, 12. As shown in FIG. 3, another possibility for increasing the thermal resistance is that the flange 14 is also not in full contact with the first cylinder cover 11 but only over part of its surface 14a, which increases the thermal resistance between the flange 14 and the first cylinder cover 11. In the same way, the flange 14 could also be arranged in the second cylinder cover 12. The reciprocating compressor 1 according to the invention is advantageously operated at ambient temperature, so that the cylinder 10 is heated by the ambient air during the conveying and compression of, for example, exhaust steam gas, whereby the increase in thermal resistance described above results in the advantage that the cylinder 10 is cooled to a reduced extent due to the fluid F flowing through it, so that the cylinder 10 has a higher temperature during operation and preferably also a more uniform temperature distribution, which reduces, for example, the risk of warping of the components of the reciprocating compressor 1 due to the temperature differences applied, in particular warping of the cylinder 10, the piston 20, the piston rod 24 or the spacer 40.

[0036] In an advantageous embodiment, the inner surface of the first or second cylinder cover 11, 12 and the outer surface of the first or second piston cover 21, 22 are designed to match each other in such a way that the so-called damage space remains as small as possible.

[0037] As shown in FIGS. 2 and 3, in an advantageous embodiment at least one of the two piston covers 21, 22 has a piston end face 21a, 22a which projects towards the associated cylinder cover 11, 12 and is in particular convex, the associated cylinder cover 11, 12 having a correspondingly projecting cylinder cover outer face 11c, 12c or a cylinder cover inner face 11d, 12d which recedes correspondingly with respect to the piston end face 21a, 22a. In the uppermost position of the piston 20, the first cylinder interior space 10a corresponds to the damage space, which is very small, as shown in FIG. 3.

[0038] In one possible embodiment, the first cylinder cover 11 and/or the second cylinder cover 12 could have an end face extending perpendicular to the longitudinal axis L, in which the inlet valve 90 as well as the outlet valve 91 are arranged. Particularly advantageously, however, the first cylinder cover 11 and/or the second cylinder cover 12 are designed as shown in FIG. 2 in such a way that the inlet valve 90 and the outlet valve 91 are arranged in the cylinder cover 11, 12 so as to be inclined with respect to the plane of symmetry S. The inlet valve 90 and the outlet valve 91 are arranged in the cylinder cover 11, 12 so as to be inclined with respect to the plane of symmetry S. This allows to use valves 90, 91 with larger diameter, which reduces their flow resistance.

[0039] FIGS. 4 and 5 show the same cylinder 10 as in FIG. 2, but in two different side views rather than in a sectional view. The cylinder 10 comprises the first cylinder cover 11, the cylinder jacket 13 and the second cylinder cover 12. Flanges 14 are arranged in the cylinder covers 11, 12. The cylinder 10 is fixedly connected to the carrier housing 60 by a spacer 40 and is spaced with respect to the carrier housing 60. In the illustrated embodiment, the spacer 40 comprises two support arms 42, 43 arranged symmetrically with respect to the plane of symmetry S. and the second cylinder cover 12 comprises two attachment points 12e, 12f, each of which is fixedly connected to a support arm 42, 43. Each of the two attachment points 12e, 12f is preferably identical in the circumferential direction and has a width C in the range of preferably between 10° and 30° in the circumferential direction, as shown in FIG. 4. FIG. 4 also shows the course of the intersection line B-B and the course of the symmetry plane S. FIG. 5 also shows the course of the intersection line A-A and the course of the second symmetry plane S2. The attachment points 12e, 12f preferably run essentially perpendicular to the plane of symmetry S, as shown in FIG. 4 with attachment point 12f, and are arranged to run symmetrically with respect to the plane of symmetry S. The point S3 shows the intersection of the attachment point 12f with the symmetry plane S. The attachment point 12f preferably runs symmetrically with respect to the point S3 or symmetrically with respect to the plane of symmetry S. As already described, the cylinder 10 has an average temperature in the region of the plane of symmetry S or in the region of point S3 during operation of the reciprocating compressor 1. Due to the symmetrical arrangement, the same temperature is present at both attachment points 12e, 12f, or the cylinder 10 has the same temperature, so that the first support arm 42 and the second support arm 43 also have the same temperature at the two attachment points 12e, 12f. The symmetrical design of the cylinder 10 and the flanges 14 attached to the cylinder 10, as well as the symmetrical arrangement of the two attachment points 12e, 12f, and the symmetrically designed support arms 42, 43 of the spacer 40 resulted in the advantage that the support arms 42, 43 have the same temperature at the two attachment points 12e, 12f, so that no mutual thermal distortion occurs at the two support arms 42, 43. As already described, the input fluid FE and the output fluid FA can have a considerable temperature difference, so that the corresponding flanges 14 and also the cylinder 10 and possibly the piston 20 can have a temperature difference in the direction of flow C, which could possibly lead to distortion of the cylinder or distortion of its components, in particular in the direction of flow C. However, such distortion has no or negligible influence on the point S3 or on the support arms 42, 43, so that the cylinder 10 is held in a defined position by the spacer 40 during operation of the reciprocating compressor 1. Particularly important is the aspect that the piston rod 24 also passes through the passage opening 12g of the second valve cover 12 in the region of the plane of symmetry S, a region of the valve cover 12 which also has an average temperature, so that no or only very slight thermally induced distortion should also occur between the passage opening 12g and the piston rod 24.

[0040] In FIG. 5, the spacer 40 is U-shaped, comprising a first support arm 42 and a second support arm 43. However, the spacer 40 could also have more support arms, for example four, six or eight, which are connected to the second cylinder cover 12, and which are preferably arranged symmetrically with respect to the symmetry plane S. For better illustration, the second stuffing box chamber 51 and the third stuffing box chamber 52 are not shown in FIG. 5.

[0041] FIG. 6 shows substantially the cylinder 10 and the piston 20 without the flanges 14 in a section along section line A-A. FIG. 7 shows substantially the cylinder 10 and the piston 20 without the flanges 14 in a section along the line of intersection B-B.

[0042] The cylinder 10 comprises at least three parts, the first cylinder cover 11, the second cylinder cover 12 and a preferably tubular cylinder jacket 13, wherein the cylinder jacket 13 is arranged between the first cylinder cover 11 and the second cylinder cover 13.

[0043] The piston 20 includes at least three parts, a first piston cap 21, a second piston cap 22, and a piston skirt 23 disposed between the first and second piston caps 21, 22. This layered structure of cylinder and/or piston allows a particularly favorable maintenance, because on the occasion of the maintenance only those parts have to be replaced, which could show a considerable wear, for example the cylinder jacket 13 and the piston jacket 23. Advantageously the piston jacket 23 has at least partly a labyrinth-shaped outer surface 23a, so that the piston compressor 1 is designed as a labyrinth piston compressor. In a further advantageous embodiment, instead of the labyrinthine outer surface 23a, at least one sealing ring is arranged on the piston skirt 23, the piston skirt 23 preferably having at least one circumferential groove in which the sealing ring is arranged, so that the piston compressor 1 is designed as a ring-sealed piston compressor 1.

[0044] The second cylinder cover 12 has attachment points 12e, 12f, preferably arranged on its outer edge 12i, to which the support arms 42, 43 are fastened by a fastening means not shown, preferably a screw. The attachment points 12e, 12f are preferably mutually symmetrical with respect to the plane of symmetry S.

[0045] In an advantageous embodiment, at least one of the two piston covers 21, 22 has a piston end face 21a, 22a which projects towards the associated cylinder cover 11, 12 and is convex in particular, the associated cylinder cover 11, 12 having a correspondingly projecting cylinder cover outer face 11c, 12c or a cylinder cover inner face 11d, 12d which recedes correspondingly with respect to the piston end face 21a, 22a, as shown for example in FIG. 2.

[0046] The second cylinder cover 12 has in its center a passage opening 12g extending in longitudinal direction L, along which the piston rod 24 extends, wherein preferably in longitudinal direction L downstream of the passage opening 12g, outside the cylinder cover 12, at least one stuffing box chamber 50 is arranged and preferably a plurality of stuffing box chambers are arranged.

[0047] In an advantageous embodiment of the reciprocating compressor, at least one of inlet valve 90, outlet valve 91 and flange 14 is not in contact with the first or second cylinder cover 11, 12 with the entire possible surface area, but is only in contact with the first or second cylinder cover 11, 12 with a partial surface area, i.e. with a part of the possible total surface area, in order to increase the thermal resistance between inlet valve 90, outlet valve 91, flange 14 and first or second cylinder cover 11, 12.

[0048] FIG. 8 shows a side view of piston compressor 1. This comprises two cylinders 10 with pistons 20 disposed therein, each piston 20 being connected to the carrier housing 60 by a spacer 40, and each piston rod 24 being driven by a common crankshaft 61. An oil collection pan 64 is located below the carrier housing 60. In further advantageous embodiments, the reciprocating compressor 1 may also comprise only a single cylinder 10 with piston 20, or a plurality of cylinders 10 with corresponding piston 20, for example between three to ten cylinders 10.

[0049] FIG. 9 shows a compressor unit 80 comprising a reciprocating compressor 1, an electric motor 81, a supply manifold 85 connected to the fluid supply line 15, and a discharge manifold 86 connected to the fluid discharge line 16. The fluid supply line 15 as well as the fluid discharge line 16 are preferably designed to be elastic in order to compensate for temperature-related expansions, whereby these lines 15, 16 consist of a metal mesh, for example.

[0050] In an advantageous embodiment, the reciprocating compressor 1 comprises a cylinder 10 and a piston 20 disposed therein, a carrier housing 60 having a crosshead 63 mounted in the carrier housing 60, a spacer 40 connecting the cylinder 10 to the carrier housing 60, and a piston rod 24 extending in a longitudinal direction L and connecting the crosshead 63 to the piston 20, the spacer 40 comprising a plurality of support arms 42, 43, the support arms 42, 43 being connected to and supporting the cylinder 10. Advantageously, the cylinder 10 comprises a plurality of attachment points 12e, 12f mutually symmetrically arranged with respect to the longitudinal axis L, to which the support arms 42, 43 are fastened. The piston compressor has a plane of symmetry S extending in the longitudinal direction L along the piston rod 24, the attachment points 12e, 12f and the support arms 42, 43 being arranged symmetrically with respect to the plane of symmetry S. Advantageously, the spacer 40 is U-shaped, with two support arms 42, 43 extending in the longitudinal direction L, the cylinder 10 having two attachment points 12e, 12f to which the support arms 42, 43 are attached. Advantageously, each attachment point 12e, 12f has a width C in the range between 10° and 30° in the circumferential direction of the cylinder 10. Advantageously, the cylinder 10 comprises an inlet valve 90 and an outlet valve 91, the inlet valve 90 and the outlet valve 91 being mutually symmetrical with respect to the plane of symmetry S. Advantageously, the cylinder 10 comprises a first cylinder cover 11 as well as a second cylinder cover 12, wherein both the first and the second cylinder cover 11, 12 comprise an inlet valve 90 as well as an outlet valve 91, so that the cylinder 10 and the piston 20 are double-acting. Advantageously, a plurality of cylinders 10 with pistons 20 arranged therein are mutually spaced on the carrier housing 60 and are each connected to the carrier housing 60 via a separate spacer 40. Advantageously, a piston rod 24 is assigned to each piston 20, the carrier housing 60 being designed as a monoblock, and the monoblock having a number of bores corresponding to the number of piston rods 45, in each of which a crosshead 63 is displaceably mounted, each piston 20 being connected to the assigned crosshead 63 via a piston rod 20. Advantageously, the monoblock and the crosshead 62 are made of a metal with a thermal conductivity in the range between 100 and 300 (W/m.Math.K), preferably aluminum or an aluminum alloy. Preferably, the cylinder 10 and/or the piston 20 is made of a metal having a thermal conductivity in the range between 100 and 300 (W/m.Math.K), preferably aluminum or an aluminum alloy.

[0051] The piston compressor 1 comprising a cylinder 10 and a piston 20 arranged therein, a carrier housing 60 with a crosshead 63 mounted in the carrier housing 60, a spacer 40 which connects the cylinder 10 to the carrier housing 60, and a piston rod 24 extending in a longitudinal direction L and connecting the crosshead 63 to the piston 20, is advantageously operated in such a way that thermal energy, caused by a thermal difference present between the cylinder 10 and the carrier housing 60, is exchanged via a plurality of support arms 42, 43. Advantageously, an inlet fluid FE is supplied to the cylinder 10 via an inlet valve 90, and the fluid located in the cylinder 10 is expelled from the cylinder 10 via an outlet valve 91 as an outlet fluid FA, wherein the inlet valve 90 and the outlet valve 91 are arranged symmetrically with respect to a plane of symmetry S extending along the longitudinal direction L of the piston rod 24, so that the cylinder 10 is heated during the conveyance of the fluid in the region of the plane of symmetry S to a mean temperature which lies between the temperature of the inlet fluid FE and the outlet fluid FA, the support arms 42, 43 being connected to the cylinder 10 in the region of the plane of symmetry S via attachment points 12e, 12f. Advantageously, the two center points S3 between the attachment points 12e, 12f are tempered to essentially the same temperature while the fluid is being conveyed. Advantageously, the piston rod 45 extends in the region of the plane of symmetry S, and this is tempered to substantially the same temperature as the attachment points 12e, 12f while the fluid is being conveyed.

[0052] The piston compressor 1 shown in FIG. 1 comprises a cylinder 10 and a piston 20 arranged therein, a carrier housing 60 with a crosshead 63 mounted in the carrier housing 60, a spacer 40 which connects the cylinder 10 to the carrier housing 60, and a piston rod 24 which extends in a longitudinal direction L and connects the crosshead 63 to the piston 20, the spacer 40 comprising a plurality of support arms 42, 43 extending in the longitudinal direction L, the support arms 42, 43 each being individually connected to the cylinder 10 towards the cylinder 10.

[0053] The cylinder 10 has a plurality of attachment points 12e, 12f, with one support arm 42, 43 attached to each of the attachment points 12e, 12f.

[0054] The attachment points 12e, 12f are arranged symmetrically with respect to each other in the longitudinal direction L.

[0055] The method of operating a reciprocating compressor 1 includes a cylinder 10 and a piston 20 disposed therein, a carrier housing 60 having a crosshead 63 supported in the carrier housing 60, a spacer 40 connecting the cylinder 10 to the carrier housing 60, and a piston rod 24 extending in a longitudinal direction L and connecting the crosshead 63 to the piston 20, wherein the spacer 40 includes a plurality of support arms 42 extending in a longitudinal direction L, 43, wherein the support arms 42, 43 are each individually connected to the cylinder 10 via attachment points 12e, 12f, so that thermal energy, due to a thermal difference present between the attachment points 12e, 12f, is not exchanged directly in the circumferential direction with respect to the longitudinal direction L between the attachment points 12e, 12f, but is exchanged via the support arms 42, 43 extending in the longitudinal direction L.

[0056] In the process, the inlet fluid FE is preferably supplied at a temperature in the range between −162° C. and −40° C., and the outlet fluid FA is preferably heated by a temperature difference in the range between 100° C. and 150° C. due to compression.

[0057] During the process, the attachment points 12e, 12f each have a center point S3 in the region of the plane of symmetry S, which during the

[0058] The temperature of the fluid can be maintained at essentially the same temperature while it is being conveyed.

[0059] In the method, the spacer 40 is U-shaped with a support section 41 and two support arms 42, 43 extending in the longitudinal direction L, wherein thermal energy is exchanged between the cylinder 10 and the carrier housing 60 via the support arms 42, 43 and the support section 41.

[0060] In the method, each attachment point (12e, 12f) has a width C in the circumferential direction of the cylinder 10 in the range between 10° and 30°, each attachment point 12e, 12f being arranged symmetrically with respect to the center point S3 so that thermal energy is transferred in the circumferential direction from the respective support arm 42, 43 along the attachment point 12e, 12f.