Carbon compression mechanism of ship gas turbine carbon capture equipment
By designing the carbon compression mechanism of the marine gas turbine carbon capture equipment, and utilizing the contact rod limit and buffer components to absorb vibration, the problems of complex installation and vibration of traditional carbon dioxide compressors are solved, enabling rapid disassembly and assembly and stable operation, thus extending the equipment's lifespan.
Patent Information
- Application Number
- CN202520547016.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-26
- Publication Date
- 2026-01-23
- Estimated Expiration
- 2035-03-26
AI Technical Summary
Traditional carbon dioxide compressors have complex installation structures, require a lot of manpower and time, and lack effective vibration damping mechanisms, which leads to equipment loosening and wear, affecting capture efficiency and reliability, and making it difficult to achieve convenient disassembly and buffer maintenance.
Design a carbon compression mechanism for a marine gas turbine carbon capture device. The mechanism uses an abutment rod limit mounting base and a buffer assembly. Quick installation is achieved through a toggle block, and the buffer assembly absorbs high-frequency vibrations to improve the stability of the device.
This enables rapid replacement and convenient maintenance of carbon dioxide compressors, improving the overall stability and service life of the equipment and reducing maintenance costs.
Smart Images

Figure CN223825208U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the technical field of carbon capture equipment for marine gas turbines, and in particular to a carbon compression mechanism for carbon capture equipment for marine gas turbines. Background Technology
[0002] With increasing global awareness of environmental protection, reducing greenhouse gas emissions, especially carbon dioxide emissions, has become an international consensus. In the shipping industry, ships, as important means of transportation, emit a significant amount of carbon dioxide from their gas engines.
[0003] In practical use, traditional carbon dioxide compressors have complex installation structures, usually using a large number of bolts and nuts for fixing. This requires a lot of time and manpower for disassembly and installation, which not only increases maintenance costs but also reduces the availability of the equipment. In addition, traditional installation structures often lack effective vibration damping mechanisms, leading to problems such as loosening and wear after long-term operation, which in turn affects the capture efficiency and reliability. Improvements are urgently needed, as well as the inconvenience of convenient disassembly and maintenance of the equipment.
[0004] Therefore, to address the aforementioned issues of inconvenience in facilitating easy disassembly and maintenance of the equipment, a carbon compression mechanism for marine gas turbine carbon capture equipment can be designed. During the use of the marine gas turbine carbon capture equipment, the abutment rods limit and abut against the mounting base from all sides above. Furthermore, the buffer components can effectively absorb and offset these high-frequency vibrations, not only enabling rapid replacement and convenient maintenance of the carbon dioxide compressor, but also improving the overall stability and service life of the equipment through an effective vibration offsetting mechanism. Utility Model Content
[0005] To address the challenges of using the carbon compression mechanism in a marine gas turbine carbon capture device, it is crucial to improve the traditional carbon dioxide compressor installation structure. Traditional compressors often require numerous bolts and nuts for fastening, consuming significant time and manpower for disassembly and installation. This increases maintenance costs and reduces equipment availability. Furthermore, traditional installation structures often lack effective vibration damping mechanisms, leading to loosening and wear after long-term operation, thus affecting capture efficiency and reliability. This necessitates improvements to facilitate convenient disassembly, assembly, and maintenance.
[0006] A carbon compression mechanism for a marine gas turbine carbon capture device includes a fixed base, a bottom groove, a mounting base, a carbon dioxide compressor body, an adjusting groove, an adjusting rod, an adjusting block, an abutment rod, a toggle block, a buffer assembly, a support assembly, and a reset assembly. The fixed base has a bottom groove inside, and multiple sets of buffer assemblies are arranged on both sides of the bottom groove. A support assembly is arranged above the buffer assemblies, and a mounting base is arranged inside the support assembly. The carbon dioxide compressor body is arranged above the mounting base. Multiple sets of adjusting grooves are opened on both sides of the upper part of the support assembly. An adjusting rod is arranged inside the adjusting groove, and an adjusting block is arranged on the side wall of the adjusting rod. A reset assembly is arranged outside the adjusting rod. Two sets of abutment rods are arranged on both sides of the upper part of the support base, and a toggle block is arranged above the abutment rod.
[0007] Preferably, during the use of the marine gas turbine carbon capture equipment, firstly, by pulling the actuating block outward, this action causes the abutment rod to expand in the opposite direction. The abutment rod then pushes the adjusting block to slide on the adjusting rod. Subsequently, the carbon dioxide compressor body and its mounting base are placed inside the support assembly. After releasing the actuating block, the reset assembly, utilizing its elastic characteristics, pushes the adjusting block and the abutment rod back to their original positions. The abutment rod then limits and abuts the mounting base from all sides and above, thereby achieving rapid installation and fixation of the carbon dioxide compressor, facilitating subsequent replacement and maintenance. During operation, the high-frequency vibrations generated by the carbon dioxide compressor are transmitted to the buffer assembly below through the support assembly. Due to the elasticity of the buffer assembly, these high-frequency vibrations can be effectively absorbed and offset. In summary, this utility model, through its ingeniously designed adjustment and buffer mechanism, not only achieves rapid replacement and convenient maintenance of the carbon dioxide compressor, but also improves the overall stability and service life of the equipment through an effective vibration offsetting mechanism.
[0008] Preferably, the adjusting block and the adjusting rod are slidably connected, both ends of the abutting rod are fixedly connected to the side walls of the two adjusting blocks, and the inner wall of the abutting rod is in contact with the mounting base.
[0009] Preferably, the buffer assembly includes a buffer side plate, a fixed side plate, and a fixed support column. Multiple sets of fixed side plates are provided on both inner walls of the bottom groove, and a fixed support column is provided between two sets of fixed side plates. A buffer side plate is provided on the side wall of the fixed support column.
[0010] Preferably, the buffer assembly also includes a buffer spring and a buffer base plate, the buffer side plate is slidably connected to the fixed support, the bottom groove is provided with a buffer base plate, and two sets of buffer springs are provided on the upper and lower sides of the buffer side plate.
[0011] Preferably, the buffer side plate is disposed on the side wall of the buffer base plate, one end of the buffer spring is fixedly connected to the inner wall of the buffer side plate, and the other end of the buffer spring is fixedly connected to the inner wall of the fixed side plate.
[0012] Preferably, the support assembly includes a support base and a mounting groove. The support base is provided above the buffer base plate, the side wall of the support base is slidably connected to the inner wall of the fixed base, and the mounting groove is provided above the support base.
[0013] Preferably, the reset assembly includes a reset spring, with the reset spring located on the outside of the adjusting rod. One end of the reset spring is fixedly connected to the inner wall of the adjusting groove, and the other end of the reset spring is fixedly connected to the inner wall of the adjusting block.
[0014] When the carbon capture equipment for marine gas turbines is in use, firstly, by pulling the actuating block outward, this action causes the abutment rod to expand in the opposite direction. The abutment rod then pushes the adjusting block to slide on the adjusting rod. Subsequently, the carbon dioxide compressor body and its mounting base are placed inside the support assembly. After releasing the actuating block, the reset assembly, utilizing its elastic characteristics, pushes the adjusting block and the abutment rod back to their original positions. The abutment rod then limits and abuts the mounting base from all sides and above, thus achieving rapid installation and fixation of the carbon dioxide compressor, facilitating subsequent replacement and maintenance. During operation, the high-frequency vibrations generated by the carbon dioxide compressor are transmitted to the buffer assembly below through the support assembly. Due to the elasticity of the buffer assembly, these high-frequency vibrations can be effectively absorbed and offset. In summary, this utility model, through its ingeniously designed adjustment and buffer mechanism, not only achieves rapid replacement and convenient maintenance of the carbon dioxide compressor, but also improves the overall stability and service life of the equipment through an effective vibration offsetting mechanism. Attached Figure Description
[0015] Figure 1 The diagram shown is a first three-dimensional structural schematic of the carbon compression mechanism of a marine gas turbine carbon capture device according to this utility model.
[0016] Figure 2 The diagram shown is a partial three-dimensional structural schematic of the carbon compression mechanism of a marine gas turbine carbon capture device according to this utility model.
[0017] Figure 3 The diagram shown is a partial three-dimensional structural schematic of the carbon compression mechanism of a marine gas turbine carbon capture device according to this utility model.
[0018] Figure 4 The diagram shown is a three-dimensional structural schematic of the third part of the carbon compression mechanism of a marine gas turbine carbon capture device according to this utility model.
[0019] Figure 5 The diagram shown is a three-dimensional structural schematic of the fourth part of the carbon compression mechanism of a marine gas turbine carbon capture device according to this utility model.
[0020] Explanation of reference numerals in the attached drawings: 1. Fixed seat; 2. Bottom groove; 3. Mounting seat; 4. Carbon dioxide compressor body; 5. Adjustment groove; 6. Adjustment rod; 7. Adjustment block; 8. Abutment rod; 9. Actuating block; 101. Buffer side plate; 102. Fixed side plate; 103. Fixed support column; 104. Buffer spring; 105. Buffer base plate; 201. Support seat; 202. Mounting groove; 301. Return spring. Detailed Implementation
[0021] The present invention will be further described below with reference to the accompanying drawings and embodiments.
[0022] Please see Figure 1 and Figure 5 This utility model provides an embodiment of a carbon compression mechanism for a marine gas turbine carbon capture device, comprising a fixed base 1, a bottom groove 2, a mounting base 3, a carbon dioxide compressor body 4, an adjusting groove 5, an adjusting rod 6, an adjusting block 7, an abutment rod 8, a toggle block 9, a buffer assembly, a support assembly, and a reset assembly. The fixed base 1 has a bottom groove 2 inside, and multiple sets of buffer assemblies are arranged on both sides of the bottom groove 2. A support assembly is arranged above the buffer assembly, and a mounting base 3 is arranged inside the support assembly. The carbon dioxide compressor body 4 is arranged above the mounting base 3. Multiple sets of adjusting grooves 5 are opened on both sides of the upper part of the support assembly. An adjusting rod 6 is arranged inside the adjusting groove 5, and an adjusting block 7 is arranged on the side wall of the adjusting rod 6. A reset assembly is arranged outside the adjusting rod 6. Two sets of abutment rods 8 are arranged on both sides of the upper part of the support base 201, and a toggle block 9 is arranged above the abutment rod 8.
[0023] Please see Figure 2 and Figure 3 The adjusting block 7 is slidably connected to the adjusting rod 6. Both ends of the abutting rod 8 are fixedly connected to the side walls of the adjusting blocks 7 on both sides. The inner wall of the abutting rod 8 is in contact with the mounting base 3. The abutting rod 8 limits the mounting base 3 from all sides and above, thereby realizing the rapid installation and fixing of the carbon dioxide compressor. The buffer assembly includes a buffer side plate 101, a fixed side plate 102, and a fixed support column 103. Multiple sets of fixed side plates 102 are provided on both sides of the inner wall of the bottom groove 2. A fixed support column 103 is provided between two sets of fixed side plates 102. The fixed support column 103... A buffer side plate 101 is provided on the side wall, and the fixed side plate 102 can be slidably guided by the fixed support column 103. The buffer assembly also includes a buffer spring 104 and a buffer base plate 105. The buffer side plate 101 is slidably connected to the fixed support column 103. The bottom groove 2 is provided with a buffer base plate 105. Two sets of buffer springs 104 are provided on the upper and lower sides of the buffer side plate 101. Due to the elasticity of the buffer springs 104, the buffer side plate 101 can slide and be guided on the fixed support column 103, effectively absorbing and offsetting these high-frequency vibrations.
[0024] Please see Figure 4 and Figure 5 A buffer side plate 101 is disposed on the side wall of a buffer base plate 105. One end of a buffer spring 104 is fixedly connected to the inner wall of the buffer side plate 101, and the other end of the buffer spring 104 is fixedly connected to the inner wall of a fixed side plate 102. Due to the elasticity of the buffer spring 104, the buffer side plate 101 can slide and guide on the fixed support column 103, effectively absorbing and offsetting these high-frequency vibrations. The support assembly includes a support base 201 and a mounting groove 202. The support base 201 is disposed on the top of the buffer base plate 105, and the side wall of the support base 201 is fixedly connected to the inner wall of the fixed support column 102. The inner wall of the seat 1 is slidably connected, and the upper part of the support seat 201 is provided with an installation groove 202. The carbon dioxide compressor body 4 and its mounting seat 3 are placed in the installation groove 202 above the support seat 201. The reset assembly includes a reset spring 301. The external part of the adjusting rod 6 is provided with a reset spring 301. One end of the reset spring 301 is fixedly connected to the inner wall of the adjusting groove 5, and the other end of the reset spring 301 is fixedly connected to the inner wall of the adjusting block 7. After the toggle block 9 is released, the reset spring 301 uses its elastic characteristics to push the adjusting block 7 and the abutment rod 8 to reset.
[0025] When the ship's gas turbine carbon capture equipment is in use, firstly, by pulling the actuating block 9 outward, this action causes the abutment rod 8 to expand in the opposite direction. The abutment rod 8 then pushes the adjusting block 7 to slide on the adjusting rod 6. At this time, the return spring 301 is stretched and deformed. Subsequently, the carbon dioxide compressor body 4 and its mounting base 3 are placed in the mounting groove 202 above the support base 201.
[0026] After the toggle block 9 is released, the return spring 301, utilizing its elastic characteristics, pushes the adjusting block 7 and the abutment rod 8 to reset. The abutment rod 8 then limits and abuts the mounting base 3 from all sides and above, thereby achieving quick installation and fixation of the carbon dioxide compressor, facilitating subsequent replacement and maintenance.
[0027] During operation, the high-frequency vibrations generated by the carbon dioxide compressor are transmitted through the support base 201 to the buffer base plate 105 below and the buffer side plates 101 on its side walls. Due to the elasticity of the buffer spring 104, the buffer side plates 101 can slide and guide on the fixed support column 103, effectively absorbing and canceling these high-frequency vibrations, ensuring stable operation of the equipment and extending its service life.
[0028] In summary, this utility model, through its ingeniously designed adjustment and buffer mechanism, not only enables rapid replacement and convenient maintenance of the carbon dioxide compressor, but also improves the overall stability and service life of the equipment through an effective vibration damping mechanism.
[0029] Through the above steps, when the ship's gas turbine carbon capture equipment is in use, firstly, by pulling the actuating block 9 outward, this action causes the abutment rod 8 to expand in the opposite direction. The abutment rod 8 then pushes the adjusting block 7 to slide on the adjusting rod 6. Subsequently, the carbon dioxide compressor body 4 and its mounting base 3 are placed inside the support assembly. After releasing the actuating block 9, the reset assembly, utilizing its elastic characteristics, pushes the adjusting block 7 and the abutment rod 8 to reset. The abutment rod 8 limits and abuts the mounting base 3 from all sides and above, thereby achieving rapid installation and fixation of the carbon dioxide compressor, facilitating subsequent replacement and maintenance. During operation, the high-frequency vibration generated by the carbon dioxide compressor is transmitted to the buffer assembly below through the support assembly. Due to the elasticity of the buffer assembly, these high-frequency vibrations can be effectively absorbed and offset. In summary, this utility model, through its ingeniously designed adjustment and buffer mechanism, not only achieves rapid replacement and convenient maintenance of the carbon dioxide compressor, but also improves the overall stability and service life of the equipment through an effective vibration offsetting mechanism.
[0030] The embodiments of the present invention have been described in detail above with reference to the accompanying drawings. However, the present invention is not limited to the above embodiments. Within the scope of knowledge possessed by those skilled in the art, various changes can be made without departing from the spirit of the present invention.
Claims
1. A carbon compression mechanism for a marine gas turbine carbon capture device, comprising a fixed base (1) and a carbon dioxide compressor body (4), characterized in that: It also includes a bottom groove (2), a mounting base (3), an adjustment groove (5), an adjustment rod (6), an adjustment block (7), a contact rod (8), a toggle block (9), a buffer assembly, a support assembly, and a reset assembly. The fixed base (1) has a bottom groove (2) inside. Multiple sets of buffer assemblies are provided on both sides of the bottom groove (2). A support assembly is provided above the buffer assembly. The mounting base (3) is provided inside the support assembly. The carbon dioxide compressor body (4) is provided above the mounting base (3). Multiple sets of adjustment grooves (5) are provided on both sides above the support assembly. An adjustment rod (6) is provided inside the adjustment groove (5). An adjustment block (7) is provided on the side wall of the adjustment rod (6). A reset assembly is provided outside the adjustment rod (6). Two sets of contact rods (8) are provided on both sides above the support base (201). A toggle block (9) is provided above the contact rods (8).
2. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 1, characterized in that: The adjusting block (7) is slidably connected to the adjusting rod (6), and both ends of the abutting rod (8) are fixedly connected to the side walls of the adjusting blocks (7) on both sides. The inner wall of the abutting rod (8) is abutting against the mounting base (3).
3. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 1, characterized in that: The buffer assembly includes a buffer side plate (101), a fixed side plate (102) and a fixed support column (103). Multiple sets of fixed side plates (102) are provided on both sides of the inner wall of the bottom groove (2). A fixed support column (103) is provided between two sets of fixed side plates (102). A buffer side plate (101) is provided on the side wall of the fixed support column (103).
4. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 3, characterized in that: The buffer assembly also includes a buffer spring (104) and a buffer base plate (105). The buffer side plate (101) is slidably connected to the fixed support column (103). The bottom groove (2) is provided with a buffer base plate (105). Two sets of buffer springs (104) are provided on the upper and lower sides of the buffer side plate (101).
5. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 4, characterized in that: The buffer side plate (101) is set on the side wall of the buffer base plate (105), one end of the buffer spring (104) is fixedly connected to the inner wall of the buffer side plate (101), and the other end of the buffer spring (104) is fixedly connected to the inner wall of the fixed side plate (102).
6. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 4, characterized in that: The support assembly includes a support base (201) and a mounting groove (202). The support base (201) is provided above the buffer base plate (105). The side wall of the support base (201) is slidably connected to the inner wall of the fixed base (1). The mounting groove (202) is provided above the support base (201).
7. The carbon compression mechanism of a marine gas turbine carbon capture device according to claim 4, characterized in that: The reset assembly includes a reset spring (301). The reset spring (301) is provided on the outside of the adjusting rod (6). One end of the reset spring (301) is fixedly connected to the inner wall of the adjusting groove (5), and the other end of the reset spring (301) is fixedly connected to the inner wall of the adjusting block (7).