Support ring made of compressed carbon fiber reinforced composite material
Compression molding of carbon fiber-reinforced composite chips with 3 to 20 mm fibers addresses the limitations of conventional materials by enhancing strength, airtightness, and thermal stability in sealing elements and support rings for reciprocating compressors.
Patent Information
- Application Number
- JP2022514764
- Authority / Receiving Office
- JP · JP
- Patent Type
- Patents
- Current Assignee / Owner
- Priority Date
- 2019-09-06
- Filing Date
- 2020-09-06
- Publication Date
- 2025-09-25
- Estimated Expiration
- 2040-09-06
AI Technical Summary
Sealing elements and support rings made from conventional carbon fiber-reinforced plastics exhibit strength drawbacks, low airtightness, and uneven thermal expansion, limiting their suitability for high-pressure applications in reciprocating compressors.
Manufacturing sealing elements and support rings by compression molding carbon fiber-reinforced composite chips with carbon fibers ranging from 3 to 20 mm long, resulting in a random fiber orientation for isotropic properties, enhancing strength, airtightness, and uniform thermal expansion.
The solution provides sealing elements and support rings with increased strength, high airtightness, and uniform thermal expansion, reducing the risk of jamming and friction, and ensuring precise fit and impact resistance in reciprocating compressors.
Abstract
Description
[Technical Field]
[0001] The present invention relates to a sealing element and / or support ring, in particular for a reciprocating compressor, manufactured by compression molding of a mixture of chips of carbon fiber reinforced composite material, to a method for manufacturing such a sealing element and / or support ring, and to a reciprocating compressor including at least one such sealing element and / or support ring. [Background technology]
[0002] Sealing elements such as piston rings or packing rings, guide rings such as piston guide rings, and guide seals such as piston guide rings must meet a wide range of requirements to perform their functions. In particular, they must have adequate hardness, sufficiently high tensile strength, sufficiently high elongation at break, good shape conformance, high aging resistance, low pressure creep and cold flow tendencies, excellent chemical resistance, excellent heat resistance, and (depending on the application) possibly high ozone resistance. For example, good shape conformance is necessary to ensure that the sealing elements remain functional even when moved. Furthermore, low pressure creep and cold flow tendencies are essential to prevent irreversible plastic deformation at low temperatures under load, even after long periods of operation.
[0003] Due to their superior properties, sealing elements are often made from polytetrafluoroethylene (PTFE)-based compositions. PTFE is characterized by, for example, a very wide thermal range, nearly universal chemical resistance, and excellent resistance to light, weather, and hot steam. Furthermore, PTFE is characterized by excellent sliding properties, excellent adhesion resistance, excellent electrical properties, and excellent dielectric properties. However, to reduce cold flow and improve mechanical properties, PTFE is usually not used in its pure form but is reinforced with fillers. For example, carbon, graphite, molybdenum disulfide, or bronze particles are used as fillers. Recently, fiber-reinforced composites using a PTFE matrix with embedded fibers, such as glass fiber, carbon fiber, or aramid fiber, have become increasingly popular for this purpose. However, due to their limited mechanical stability, such PTFE-based materials are limited to applications in sealing elements or support rings at lower pressure ranges. For high-pressure applications, corresponding materials based on high-performance polymers such as polyimide, polyaryletherketone, polyphenylene sulfide, polyetheretherketone (PEEK), etc. Carbon fiber reinforced plastics (CFRP), such as those with a matrix of PEEK with 10% by weight of embedded carbon fibers, are used for this purpose.
[0004] Typically, sealing elements and support rings made of such carbon fiber-reinforced plastics are manufactured by injection molding using short carbon fibers, typically up to 1 mm in length. These short fibers have the advantage of following the contours of the component being manufactured and not protruding from the surface of the component. It is also known to manufacture such components by sintering granules containing short fibers, typically about 0.1 mm in length. The granules are sintered under pressure, and the fibers are internal to the component. However, sealing elements and support rings manufactured in this way have strength drawbacks, and their relatively low airtightness and excessively high and uneven thermal expansion require improvement. Summary of the Invention [Problem to be solved by the invention]
[0005] On this basis, the present invention aims to provide a sealing element or support ring that is characterized by increased strength, higher tightness, improved low and particularly uniform thermal expansion and is particularly suitable for use in reciprocating compressors. [Means for solving the problem]
[0006] According to the invention, this object is solved by a sealing element and / or a support ring, in particular for reciprocating compressors, manufactured by compression molding of a mixture of chips of carbon fiber reinforced composite material, at least part of the chips containing carbon fibers having a length of 3 to 20 mm, preferably the carbon fibers in the sealing element and / or support ring having a random fiber orientation. DETAILED DESCRIPTION OF THE INVENTION
[0007] This solution is based on the surprising discovery that such sealing elements and / or support rings manufactured by compression molding a mixture of carbon fiber-reinforced composite chips, at least some of which contain carbon fibers 3 to 20 mm long, not only exhibit increased strength but also particularly high airtightness and improved low and particularly uniform thermal expansion. In compression molding, carbon fiber-reinforced composite chips are introduced into a mold cavity, which is heated and closed using a plunger. As a result, the molding compound is pressed into the shape of the cavity. When the small chips are poured into the cavity, they are randomly arranged, resulting in a random fiber orientation in the finished component. That is, carbon fibers oriented in all directions are present in the finished component. As a result, sealing elements and support rings are obtained that have at least largely isotropic properties. In particular, sealing elements and support rings according to the present invention are characterized by relatively uniform thermal expansion, with the thermal expansion in the pressing direction being slightly higher than the thermal expansion in the transverse direction. Furthermore, the sealing element and support ring according to the present invention are characterized by very low thermal expansion in the direction transverse to the pressing direction, which is particularly within the range of that of steel. In the pressing direction, the thermal expansion corresponds to that of the plastic forming the matrix of the carbon fiber-reinforced composite material. Due to the low thermal expansion, only small clearances are required between the sealing element or support ring and the sealed or supported component (such as between the piston rod and the support ring), resulting in a constant, narrow gap. This reduces the risk of localized heating during operation and, therefore, the risk of jamming. This material is resistant to expansion when heated, whereas conventional support rings expand upon heating, resulting in contact with the piston rod and causing friction and mutual heating between the support ring and the piston rod. The mechanical properties of the sealing element and support ring according to the present invention are also relatively uniform. Furthermore, the sealing element and support ring according to the present invention are characterized by a higher gas-tightness. Therefore, it is possible to overlap properly manufactured valve plates, resulting in a very precise surface. The plates are also highly impact-resistant, highly heat-resistant, have a low temperature coefficient, and are lightweight.Finally, unexpectedly, despite their relatively long length of 3-20 mm, the carbon fibers do not protrude from the sealing element or support ring and, as a result, do not rub against other components, such as the piston rod. Rather, in the context of the present invention, it has been shown that the carbon fibers break off at their ends when they protrude from the component. For all these reasons, the sealing element or support ring according to the present invention is particularly suitable for use in piston compressors.
[0008] According to the present invention, the carbon fibers in the sealing element and / or support ring have a random fiber orientation in at least two dimensions, and preferably in all three dimensions, i.e., the properties imparted by the fibers are isotropic or mostly isotropic in at least two dimensions, and preferably in all three dimensions.
[0009] According to the present invention, the sealing element or support ring is made from chips of carbon fiber reinforced composite material, at least part of which contains carbon fibers with a length of 3 to 20 mm. If the carbon fiber length is less than 3 mm, the advantages of the present invention, such as increased strength and low, uniform thermal expansion, are no longer achieved to the desired extent. If the carbon fiber is longer than 20 mm, compression molding does not result in a sufficiently high random fiber orientation within the component, and the desired uniformity of properties is not achieved.
[0010] According to the present invention, at least a portion of the chips contain carbon fibers having a length of 3 to 20 mm. In order to achieve the above-mentioned advantages of the present invention to a high degree, in a further development of the present invention, it is proposed that at least 50%, more preferably at least 60% or 70%, particularly preferably at least 80%, and very preferably at least 90% of the chips used in compression molding have carbon fibers having a length of 3 to 20 mm.
[0011] Most preferably, all chips used in the compression molding comprise carbon fibers having a length of 3 to 20 mm. In addition to carbon fibers having a length of 3 to 20 mm, the chips may contain carbon fibers of different lengths. However, in each chip containing carbon fibers having a length of 3 to 20 mm, it is preferred that at least 50%, more preferably at least 60% or 70%, particularly preferably at least 80%, and very preferably at least 90% of the carbon fibers contained therein have a length of 3 to 20 mm. More preferably, all of the carbon fibers in each chip containing carbon fibers having a length of 3 to 20 mm have a length of 3 to 20 mm.
[0012] Most preferably, all chips used in compression molding contain only carbon fibers having lengths between 3 and 20 mm. For purposes of the present invention, this is understood to mean that each of the carbon fibers contained in the chip has a length between 3 and 20 mm, but the lengths of all fibers do not necessarily have to be the same, so long as each carbon fiber is between 3 and 20 mm long. Thus, a chip containing first carbon fibers, each having a length of 5 mm, second carbon fibers, each having a length of 10 mm, and third carbon fibers, each having a length of 15 mm, is a chip containing only carbon fibers having lengths between 3 and 20 mm.
[0013] In all the above embodiments, it is particularly preferred if the chips containing carbon fibers having a length of 3 to 20 mm contain carbon fibers having a length of 3 to 10 mm. In order to obtain good random orientation when filling a mold used for compression molding, a further development of the idea of the present invention proposes using chips that are not too large. In particular, good results are obtained when using chips that are at least substantially plate-shaped with an at least substantially square or rectangular cross section, and have a length of 3 to 20 mm, a width of 1 to 10 mm, and a thickness of 1 to 5 mm. Therefore, it is preferred that at least 50%, more preferably at least 60% or 70%, particularly preferably at least 80%, most preferably at least 90%, and most preferably all of the chips used in compression molding have a length of 3 to 20 mm, a width of 1 to 10 mm, and a thickness of 1 to 0.5 mm. In particular, it is preferred that the length of the chips is 3 to 10 mm.
[0014] Preferably, the carbon fibers within an individual chip are arranged at least substantially parallel to one another. For purposes of this application, at least substantially parallel arrangement of the carbon fibers in an individual chip means that the longitudinal fiber axes of at least 80% of the carbon fibers do not deviate by more than 20° from the longitudinal fiber axes of all other longitudinal fiber axes of at least 80% of the carbon fibers in the chip. Preferably, this applies to at least 90%, more preferably at least 95%, and most preferably all of the carbon fibers in the chip. Most preferably, the longitudinal axes of the fibers deviate from one another by no more than 10°, even more preferably no more than 5°, particularly preferably no more than 2°, and most preferably no more than 1°. Most preferably, all of the carbon fibers in the chip are parallel to one another.
[0015] Such parallel or at least substantially parallel arrangement of the carbon fibers in the individual chips is preferably achieved by first providing at least one tape of carbon fiber reinforced composite material, the carbon fibers in said at least one tape being arranged parallel or at least substantially parallel, and then cutting said at least one tape transversely to the carbon fiber direction into chips each having a length of 3 to 20 mm, so that the parallelism of the carbon fibers of the tape is maintained in the chips produced therefrom.
[0016] In particular, sealing elements or support rings with good properties are obtained when chips containing carbon fibers with a length of 3 to 20 mm contain 20 to 70% by weight of carbon fibers, preferably 40 to 70% by weight, particularly preferably 60 to 70% by weight of carbon fibers, for example about 65% by weight of carbon fibers, the remainder up to 100% by weight being at least one thermoplastic material.
[0017] The matrix material is selected depending on the required properties. Suitable examples of matrix materials for chips, especially chips containing carbon fibers 3 to 20 mm long, are thermoplastics selected from the group consisting of polyphenylene sulfide, perfluoroalkoxy polymers, polyetheretherketone, polytetrafluoroethylene, polyimides, polyamides, and any mixture of two or more of the aforementioned thermoplastics.
[0018] According to a highly preferred embodiment, the chips comprising carbon fibres of at least 3 to 20 mm in length comprise one or more polyetheretherketones as thermoplastic material. Particularly good results are obtained with chips containing carbon fibers of 3 to 20 mm length, which contain 20 to 70% by weight of carbon fibers, preferably 40 to 70% by weight of carbon fibers, particularly preferably 60% to 70% by weight of carbon fibers, for example about 65% by weight of carbon fibers, the remainder up to 100% by weight being one or more polyetheretherketones.
[0019] In furtherance of the invention, it is proposed that the sealing element and / or the support ring are obtainable or are obtainable by a method comprising the following steps: i) providing at least one tape of carbon fiber reinforced composite material, the at least one tape having carbon fibers oriented at least substantially parallel therein; ii) cutting the at least one tape transversely to the carbon fiber direction into chips each having a length of 3 to 20 mm; iii) placing the chip in a mold; iv) heating the chip in the mold; and v) Compressing the chip in the mold.
[0020] Preferably, in step ii), the at least one tape is cut into chips each having a width of 1 to 10 mm, the width of the chip being smaller than its length. In order to obtain sealing elements or support rings with particularly homogeneous properties, it is preferred to introduce the chips into the mould in step iii) with a random orientation.
[0021] Depending on the plastic used, the chips in step iii) are preferably heated to a temperature of 120 to 450°C, particularly preferably to a temperature of 320 to 450°C. In particular, when the chip is compressed at a pressure of 0.1 to 30 MPa in step iv), good results are obtained, especially with regard to thermal expansion and airtightness.
[0022] The sealing element and support ring according to the invention are particularly suitable as support rings of seal packings, as seal rings, as valve rings, as valve plates or as poppets of poppet valves.
[0023] Another object of the invention is a reciprocating compressor including a sealing element such as above and / or a support ring such as above.
Claims
1. 1. A support ring, particularly for a reciprocating compressor, comprising a compressed mixture of chips of a carbon fiber reinforced composite material, at least a portion of the chips containing carbon fibers having a length of 3 to 20 mm, the carbon fibers in said support ring having a random fiber orientation.
2. 2. The support ring according to claim 1, wherein the tip containing carbon fibers having a length of 3 to 20 mm does not contain fibers having a length other than carbon fibers having a length of 3 to 20 mm.
3. 3. A support ring according to claim 1 or 2, characterized in that at least 50%, preferably at least 60% or 70%, particularly preferably at least 80%, most preferably at least 90%, and most preferably all of the tips contain carbon fibers with a length of 3 to 20 mm.
4. Support ring according to any one of claims 1 to 3, characterized in that the carbon fibres within the individual tips are arranged at least substantially parallel to one another.
5. 5. Support ring according to claim 1, characterized in that the carbon fiber-containing chips with a length of 3 to 20 mm contain 20 to 70% by weight of carbon fibers, preferably 40 to 70% by weight of carbon fibers, particularly preferably 60 to 70% by weight of carbon fibers, the remainder up to 100% by weight being at least one thermoplastic material.
6. Support ring according to any one of claims 1 to 5, characterized in that the tip containing carbon fibres of length 3 to 20 mm contains carbon fibres of length 3 to 10 mm.
7. 7. A support ring according to any one of claims 1 to 6, characterized in that the chips containing carbon fibres of 3 to 20 mm in length contain at least one thermoplastic selected from the group consisting of polyphenylene sulfide, perfluoroalkoxy polymer, polyetheretherketone, polytetrafluoroethylene, polyimide, polyamide and any mixture of two or more of the aforementioned thermoplastics.
8. A support ring according to any one of claims 1 to 7, characterized in that the chips containing carbon fibres of length 3 to 20 mm contain one or more polyetheretherketones as thermoplastic material.
9. A method for manufacturing a support ring according to any one of claims 1 to 8, comprising the steps of: i) providing at least one tape of carbon fiber reinforced composite material, the at least one tape having carbon fibers arranged at least substantially parallel therein; ii) cutting said at least one tape transversely to the carbon fiber direction into chips each having a length of 3 to 20 mm; iii) placing the chip in a mold; iv) heating the chip in the mold; and v) Compressing the chip in the mold A method comprising:
10. 10. The method of claim 9, wherein in step ii) the at least one tape is cut into chips each having a width of 1 to 10 mm, the width of the chip being smaller than its length.
11. 11. The method according to claim 9 or 10, characterized in that in step iii) the chips are introduced into the mold in a random orientation.
12. A method according to any one of claims 9 to 11, characterized in that in step iii) the chip is heated to a temperature of 120 to 450°C, preferably to a temperature of 320 to 450°C.
13. 13. The method according to any one of claims 9 to 12, characterized in that in step iv) the chips are compressed at a pressure of 0.1 to 30 MPa.
14. Method according to any one of claims 9 to 13, characterized in that the support ring is a support ring of a seal packing.
15. A piston compressor comprising at least one support ring according to any one of claims 1 to 8.
Citation Information
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