In-situ efficient elimination system for CO toxic products
By designing a multi-layer annular structure and through-hole design, the in-situ efficient elimination system for CO poisoning products is solved, the problem of unsatisfactory CO elimination effect in the existing technology is solved, and the CO removal efficiency is achieved and the impact resistance is achieved, ensuring that the operators are and environmental security.
Patent Information
- Application Number
- CN202411619549.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-21
- Publication Date
- 2024-12-13
- Estimated Expiration
- 2044-05-21
AI Technical Summary
The existing CO elimination system has poor CO elimination effect, especially during the blasting process, and is not safe enough to operate personnel and the environment.
A system for in-situ efficient elimination of CO toxic products is designed, including a CO elimination mechanism, a movable fixing mechanism and a pressure relief mechanism. Through a combination of CO eliminator particles designed by a multi-layer annular structure and a through-hole design, the multi-layer annular structure is utilized. Cooperation with elastic components can achieve efficient CO removal and impact resistance.
It achieves efficient removal of CO, improves operating efficiency and personnel safety, and can eliminate toxic gases generated during blasting from the source and reduces environmental pollution.
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Figure CN119113750A_ABST
Abstract
Description
Technical Field
[0001] The invention belongs to the technical field of toxic gas purification, and in particular relates to an in-situ high-efficiency elimination system for CO poisoning products. Background Art
[0002] As a toxic and harmful gas, CO has a very adverse effect on the personal health of personnel. CO will be generated in many working processes. For example, a certain amount of toxic gas will be generated during blasting operations. When the CO concentration is high, it is easy to cause poisoning of the workers, and even casualties will occur. The existing elimination system for CO elimination is not ideal for CO elimination, and at the same time, it is not suitable for effectively eliminating CO generated during the blasting process. In order to effectively eliminate CO, at the same time, to ensure the personal safety of the workers. Therefore, it is urgent to provide an elimination system that can be used for CO elimination to effectively eliminate CO. On the basis of ensuring the personal safety of personnel, it can also effectively reduce the degree of pollution of the environment by the generated CO. Summary of the invention
[0003] In view of the problems existing in the above-mentioned prior art, the present invention provides an in-situ efficient elimination system for CO poisoning products. The system has an ideal CO elimination effect and high elimination efficiency. At the same time, it has strong impact resistance and self-protection ability. It can eliminate toxic and harmful gases from the source, which is beneficial to improving work efficiency and ensuring the health and safety of workers.
[0004] In order to achieve the above-mentioned object, the present invention provides an in-situ efficient elimination system for CO poisoning products, comprising a CO elimination mechanism, a movable fixing mechanism and a pressure relief mechanism; The CO elimination mechanism comprises a first loading cylinder, a second loading cylinder and a third loading cylinder; the first loading cylinder is a double-layer closed structure cylinder with an annular accommodating cavity, and a plurality of through holes 1 are arranged all over the cylinder, and the annular accommodating cavity is filled with CO eliminator particles A; the second loading cylinder is a double-layer closed structure cylinder with an annular accommodating cavity, and a plurality of through holes 2 are arranged all over the cylinder, and the annular accommodating cavity is filled with CO eliminator particles B, the aperture of the through hole 2 is larger than the aperture of the through hole 1, and the particle size of the CO eliminator particles B is larger than the particle size of the CO eliminator particles A; the second loading cylinder is uniformly distributed in the circumferential direction. The third charging cylinder is a closed cylinder with a cylindrical accommodating cavity, and a plurality of through holes three are arranged all over the cylinder body, and the cylindrical accommodating cavity is filled with CO eliminator particles C, the aperture of the through hole three is larger than the aperture of the through hole two, and the particle size of the CO eliminator particles C is larger than the particle size of the CO eliminator particles B; the third charging cylinder is coaxially fixedly connected to the inside of the second charging cylinder through a plurality of connecting brackets two uniformly distributed in the circumferential direction, and an inner annular ventilation area is formed between the third charging cylinder and the second charging cylinder; The movable fixing mechanism comprises a movable cylinder, a supporting frame and a fixing assembly; The movable cylinder comprises a main cylinder, a fixed end cover and a movable end cover; the main cylinder is provided with a plurality of through holes 1 throughout the cylinder body, the size of the main cylinder is adapted to the size of the CO elimination mechanism, and is coaxially sleeved on the outside of the CO elimination mechanism; the fixed end cover is fixedly connected to the left open end of the main cylinder, and a plurality of through holes 2 are provided on the surface thereof; the movable end cover is detachably covered on the right open end of the main cylinder, and a plurality of through holes 3 are provided on the surface thereof; the left end of the movable end cover is fixedly connected to a right limiting ring at a position outside the main cylinder; The support frame includes a first support plate, a second support plate and a support rod; the outer contour of the first support plate is circular, and its outer diameter is larger than the outer diameter of the movable cylinder; the first support plate is coaxially arranged on the left side of the movable cylinder, a circular hole 1 is opened in the center of the first support plate, and a plurality of mounting holes 1 are evenly opened in the circumferential direction of the edge portion of the first support plate, and a plurality of through holes 4 are opened in the area between the circular hole 1 and the plurality of mounting holes 1, and a connecting screw sleeve is coaxially fixedly connected to one of the circular holes on the right side of the first support plate; the outer contour of the second support plate is circular, and its outer diameter is the same as the outer diameter of the first support plate, and a circular hole 2 is opened in the center corresponding to the movable cylinder , a plurality of mounting holes 2 are opened in its edge portion corresponding to the plurality of mounting holes 1; the right end of the second support plate is fixedly connected with a left limiting ring on the outside of the circular hole 2; the left limiting ring and the right limiting ring are mutually limited and matched; the second support plate can be slidably mounted on the outside of the movable cylinder through the circular hole 2; the number of the support rods is the same as the number of the plurality of mounting holes 1 and the plurality of mounting holes 2, the plurality of support rods are evenly distributed on the outside of the movable cylinder in the circumferential direction, and the left end of each support rod is inserted in the corresponding mounting hole 1, and the right end thereof is inserted in the corresponding mounting hole 2, and a plurality of through holes are evenly opened in the length direction of each support rod; The fixing assembly comprises an articulated block, a fixing pin and a limit baffle; multiple groups of articulated blocks, multiple groups of fixing pins, multiple groups of limit baffles and multiple support rods are arranged one by one; wherein, multiple articulated blocks in each group of articulated blocks are evenly fixedly connected to the outer surface of the main cylinder body along the axial direction, and at the same time, multiple articulated blocks correspond one by one to multiple through holes on the corresponding support rods; multiple fixing pins in each group of fixing pins are respectively slidably inserted into the multiple through holes on the corresponding support rods, and at the same time, the inner ends of the multiple fixing pins are respectively movably connected to the corresponding multiple articulated blocks, and the outer ends of the multiple fixing pins are all pointed cone structures; multiple limit baffles in each group of limit baffles are respectively fixedly connected to the corresponding support rods, and at the same time, multiple limit baffles are respectively located on the right sides of the multiple through holes; The pressure relief mechanism comprises a connecting cover, a first elastic component, a front end plate, a second elastic component, a rear end plate and a third elastic component; The outer contour of the connecting cover is circular, which is located on the inner side of the plurality of support rods and is coaxially arranged between the first support plate and the movable cylinder; a circular hole three is opened in the center of the connecting cover, and a plurality of through holes five are opened in the area outside the circular hole three; a connecting stud is coaxially fixedly connected to the circular hole three on the left side of the connecting cover, and the connecting stud is inserted into the connecting screw sleeve through threaded matching; A plurality of first elastic components are evenly distributed in an annular direction between the connection cover and the movable cylinder, with the left ends thereof being connected to the connection cover and the right ends thereof being connected to the fixed end cover; The front end plate has a circular outer contour, and is evenly provided with a plurality of through holes 6, which are coaxially arranged on the left side of the first support plate; A plurality of second elastic components are evenly distributed in an annular direction between the front end plate and the first support plate, with the left ends thereof being connected to the front end plate and the right ends thereof being connected to the first support plate; The outer contour of the rear end plate is circular, and a plurality of through holes 7 are formed thereon and are coaxially arranged on the right side of the movable end cover; A plurality of third elastic components are evenly distributed in an annular direction between the movable end cover and the rear end plate, with the left end thereof being connected to the movable end cover and the right end thereof being connected to the rear end plate; When the first elastic component, the second elastic component and the third elastic component are in a normal state, the outer ends of the plurality of fixing pins in each group of fixing pins are in a state of being tilted to the left.
[0005] Furthermore, in order to effectively ensure the elimination effect of CO while reducing the airflow resistance, the aperture of the through hole one is greater than 0 and less than 0.05 mm, the aperture of the through hole two is greater than or equal to 0.05 mm and less than 0.3 mm, and the aperture of the through hole three is greater than or equal to 0.3 mm and less than 0.7 mm; the diameter of the CO eliminator particles A is 0.05-0.1 mm, the particle diameter of the CO eliminator particles B is 0.3-0.6 mm, and the particle diameter of the CO eliminator particles C is 0.7-1 mm.
[0006] Furthermore, in order to facilitate connection, the left end surface of the first support plate outside the circular hole 1 is evenly and circumferentially fixed with a plurality of connecting ear plates, the plurality of connecting ear plates are arranged one-to-one correspondingly to the plurality of second elastic components, and the right ends of the plurality of second elastic components are connected to the first support plate through the plurality of connecting ear plates.
[0007] Furthermore, in order to ensure good impact resistance and deformation resistance, the CO elimination mechanism, the movable fixing mechanism and the pressure relief mechanism are all made of metal materials with high temperature resistance and strong pressure resistance; the thickness of the front end plate and the rear end plate are both 1 to 3 mm; the thickness of the first support plate and the second support plate are both 1 to 2 mm; the thickness of the main cylinder is 1 to 1.5 mm; the thickness of the connecting cover, the fixed end cover and the movable end cover are all 1 to 2 mm.
[0008] Preferably, the number of the support rods is 4 to 12, and the number of holes on each support rod is 2 to 6; the number of the fixing pins is 8 to 72.
[0009] Furthermore, in order to ensure that the elastic component has good elastic properties and at the same time has good load-bearing capacity, the first elastic component, the second elastic component and the third elastic component are all combination springs of stainless steel corrugated springs and coil springs, the number of the first elastic components is 2 to 4, and the number of the second elastic components and the third elastic components are both 4 to 8.
[0010] In the present invention, the CO elimination mechanism is a multi-layer annular structure composed of a first charging barrel, a second charging barrel and a third charging barrel. At the same time, an outer annular ventilation area is formed between the first charging barrel and the second charging barrel, and an inner annular ventilation area is formed between the second charging barrel and the third charging barrel, so that the detonation gas can pass through the CO elimination mechanism smoothly through the outer annular ventilation area and the inner annular ventilation area. Since the first, second and third charging barrels are respectively filled with CO eliminator particles A, B and C, and at the same time, through holes are arranged on the barrel of each charging barrel, in this way, during the process of the detonation gas passing through the CO elimination mechanism, it can fully contact with the CO eliminator particles in the three charging barrels, so that the CO gas contained in the gas can be effectively eliminated by using the CO eliminator particles, and the purpose of quickly and efficiently removing toxic and harmful gases is achieved. The movable end cover is detachably covered on the right open end of the main barrel, which can facilitate opening or closing the movable barrel, and then it can facilitate loading or removing the CO elimination mechanism into or out of the movable barrel. The movable cylinder is provided with a plurality of through holes, so that the detonation gas can pass through the movable cylinder and enter the CO elimination mechanism smoothly. The second support plate is axially slidably mounted on the outer side of the movable cylinder through the circular hole in the center thereof. At the same time, a plurality of support rods surrounding the outer periphery of the movable cylinder are used to connect the second support plate and the first support plate located on the left side of the movable cylinder, so that a protection frame can be formed on the outer periphery of the movable cylinder. In this way, not only the movable cylinder can be protected, but also the movable cylinder can slide relative to the protection frame in the axial direction. The connecting screw sleeve is connected to the right side of the first support plate, and the connecting stud is connected to the left side of the connecting cover. It is convenient to fix the connecting cover between the first support plate and the movable cylinder through threaded matching, and then the movable cylinder is connected to the connecting cover by using a plurality of first elastic connecting components. While the supporting frame is used to protect the movable cylinder, a buffer force is provided for the axial movement process of the movable cylinder through the plurality of first elastic components, thereby improving the protection effect of the movable cylinder. The front end plate and the rear end plate are relatively arranged at the leftmost and rightmost positions, and a plurality of second elastic components are used to connect the front end plate and the first support plate, and a plurality of third elastic components are used to connect the rear end plate and the second support plate. The second elastic components and the third elastic components can cooperate to provide elastic forces for the movable cylinder and the support frame, thereby effectively buffering the impact force during the blasting process, thereby effectively protecting the CO elimination mechanism and the movable fixing mechanism.The outer ends of the plurality of fixing pins are all of a pointed cone structure, and at the same time, the inner ends of the fixing pins are movably connected to the main cylinder body through a hinge block, and the fixing pins of the elastic components are in an inclined state under normal conditions. In this way, when the elimination system is pushed toward the bottom of the blasthole, it can be ensured that the fixing pins can extend outward by a certain length, and can be smoothly inserted into the wall of the rock under the limiting effect of the limiting baffle, which is conducive to fixing the elimination system inside the blasthole. Combined with the buffering protection effect of the plurality of elastic components, the elimination system can be equipped with the ability to resist the blasting pressure and shock wave of the explosive. At the same time, by using a plurality of first elastic components evenly distributed in the annular direction to connect the connection cover and the movable cylinder body, by using a plurality of second elastic components evenly distributed in the annular direction to connect the front end plate and the connection cover, and by using a plurality of third elastic components evenly distributed in the annular direction to connect the movable end cover and the rear end plate, the load-bearing capacity can be effectively enhanced by a parallel connection method, and at the same time, a good pressure relief and buffering effect can be achieved, which is conducive to multiple protections for the elimination system, and the elimination system has the ability to be reused. Furthermore, when the elimination system is fixed inside the blast hole, it can also help prevent the occurrence of punching, which helps to improve the blasting effect to a certain extent. In addition, during the blasting process, the CO elimination mechanism placed in the blast hole can effectively remove CO from the gas, achieving the effect of eliminating CO from the source.
[0011] The system has an ideal CO elimination effect and high elimination efficiency. At the same time, it has strong impact resistance and self-protection ability. It can eliminate the CO generated during the operation from the source, which is beneficial to improving operation efficiency and ensuring the health and safety of workers. BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Figure 1 It is a structural schematic diagram of the present invention; Figure 2 It is a structural schematic diagram of the front end plate in the present invention; Figure 3 It is a structural schematic diagram of the rear end plate in the present invention; Figure 4 is a schematic structural diagram of the first support plate in the present invention; Figure 5 is a schematic structural diagram of the second support plate in the present invention; Figure 6 It is a structural schematic diagram of the connecting cover in the present invention; Figure 7 It is a structural schematic diagram of the movable end cover in the present invention; Figure 8 It is a cross-sectional structural diagram of the CO elimination mechanism in the present invention; Fig. 9 A schematic diagram of the change of the fixing pin from an unfixed state to a fixed state in the present invention; Fig.10It is a schematic diagram of the assembly of the elimination system in the present invention; Fig.11 It is a schematic diagram of the state of the elimination system in the blast hole in the present invention; Fig.12 for Fig.11 Schematic diagram of the cross section along the AA direction.
[0013] In the figure: 1, CO elimination mechanism, 2, movable fixing mechanism, 3, pressure relief mechanism, 4, first charging cylinder, 5, second charging cylinder, 6, third charging cylinder, 7, connecting bracket 1, 8, connecting bracket 2, 9, outer annular ventilation area, 10, inner annular ventilation area, 11, movable cylinder, 12, main cylinder, 13, fixed end cover, 14, movable end cover, 15, support frame, 16, through hole 3, 17, first support plate, 18, second support plate, 19, support rod, 20, round hole 1, 21, connecting screw sleeve, 22, installation Mounting hole one, 23, through hole four, 24, round hole two, 25, mounting hole two, 26, through hole, 27, hinge block, 28, fixing pin, 29, limit baffle, 30, left limit ring, 31, right limit ring, 32, front end plate, 33, connecting cover, 34, rear end plate, 35, first elastic component, 36, second elastic component, 37, round hole three, 38, through hole five, 39, connecting stud, 40, third elastic component, 41, through hole six, 42, through hole seven, 43, connecting ear plate, 44, explosive, 45, blast hole, 46, blockage. DETAILED DESCRIPTION
[0014] The present invention will be further described below.
[0015] like Figures 1 to 12 As shown, the present invention provides an in-situ efficient elimination system for CO poisoning products, comprising a CO elimination mechanism 1, a movable fixing mechanism 2 and a pressure relief mechanism 3; The CO elimination mechanism 1 includes a first loading cylinder 4, a second loading cylinder 5 and a third loading cylinder 6; the first loading cylinder 4 is a double-layer closed structure cylinder with an annular accommodating cavity, and a plurality of through holes 1 are arranged on the cylinder body, and the annular accommodating cavity is filled with CO eliminator particles A, and the through holes 1 are preferably circular holes; as a further preferred embodiment, the end plate at the right end of the first loading cylinder 4 is a detachable structure, so as to facilitate the loading and removal of the CO eliminator particles A; the second loading cylinder 5 is a double-layer closed structure cylinder with an annular accommodating cavity, and a plurality of through holes 2 are arranged on the cylinder body, and the annular accommodating cavity is filled with CO eliminator particles B, and the aperture of the through hole 2 is larger than the aperture of the through hole 1, and the through hole 2 is preferably a circular hole, and the particle size of the CO eliminator particles B is larger than the particle size of the CO eliminator particles A; the second loading cylinder 5 is coaxially fixedly connected to the first loading cylinder 5 through a plurality of connecting brackets 7 uniformly distributed in the circumference. The interior of the material barrel 4, and an outer annular ventilation area 9 is formed between the first loading barrel 4; as a further preference, the end plate at the right end of the second loading barrel 5 is a detachable structure, so as to facilitate the loading and removal of the CO eliminator particles B; the third loading barrel 6 is a closed barrel with a cylindrical accommodating cavity, and a plurality of through holes three are arranged all over the barrel, and the cylindrical accommodating cavity is filled with CO eliminator particles C, the aperture of the through hole three is larger than the aperture of the through hole two, and the through hole three is preferably a circular hole, and the particle size of the CO eliminator particles C is larger than the particle size of the CO eliminator particles B; the third loading barrel 6 is coaxially fixedly connected to the interior of the second loading barrel 5 through a plurality of circumferentially evenly distributed connecting brackets 2 8, and an inner annular ventilation area 10 is formed between the second loading barrel 5; as a further preference, the end plate at the right end of the third loading barrel 6 is a detachable structure, so as to facilitate the loading and removal of the CO eliminator particles C; As a preferred embodiment, the CO eliminator particles A, CO eliminator particles B and CO eliminator particles C are all prepared by a morphology control method using a transition metal oxide or multiple composite metal oxides selected from iron, copper, manganese and cobalt.
[0016] The movable fixing mechanism 2 includes a movable cylinder 11, a support frame 15 and a fixing assembly; The movable cylinder 11 includes a main cylinder 12, a fixed end cover 13 and a movable end cover 14; the main cylinder 12 is provided with a plurality of through holes 1 throughout the cylinder body, preferably the through holes 1 are circular holes, the size of the main cylinder 12 is adapted to the size of the CO elimination mechanism 1, and is coaxially sleeved on the outside of the CO elimination mechanism 1; the fixed end cover 13 is fixedly connected to the left open end of the main cylinder 12, and a plurality of through holes 2 are provided throughout the surface thereof, preferably the through holes 2 are circular holes; the movable end cover 14 is detachably covered on the right open end of the main cylinder 12, and a plurality of through holes 3 16 are provided throughout the surface thereof, preferably the through holes 3 16 are circular holes; the left end of the movable end cover 14 is fixedly connected to a right limit ring 31 at a position outside the main cylinder 12; The support frame 15 includes a first support plate 17, a second support plate 18 and a support rod 19; the outer contour of the first support plate 17 is circular, and its outer diameter is larger than the outer diameter of the movable cylinder 11; the first support plate 17 is coaxially arranged on the left side of the movable cylinder 11, and a circular hole 20 is opened in the center thereof, and a plurality of mounting holes 22 are evenly opened in the circumferential direction of the edge portion thereof, and a plurality of through holes 23 are opened in the area between the circular hole 20 and the plurality of mounting holes 22, and the through holes 23 are preferably circular holes, and the right side of the first support plate 17 is coaxially fixedly connected to the circular hole 20 A connecting screw sleeve 21 is connected; the outer contour of the second support plate 18 is circular, and its outer diameter is the same as the outer diameter of the first support plate 17, a second circular hole 24 is opened in the center corresponding to the movable cylinder 11, and a plurality of second mounting holes 25 are opened in the edge portion corresponding to the plurality of mounting holes 1 22; a left limit ring 30 is fixedly connected to the outside of the second circular hole 24 at the right end of the second support plate 18; the left limit ring 30 and the right limit ring 31 are mutually limited and matched; in order to effectively reduce the impact force during the mutual contact process, the left limit ring 30 and the right limit ring 31 are preferably made of rubber material. The second support plate 18 is slidably mounted on the outer side of the movable cylinder 11 through the second circular hole 24; the number of the support rods 19 is the same as the number of the plurality of mounting holes 1 22 and the plurality of mounting holes 25, and the plurality of support rods 19 are evenly distributed on the outer side of the movable cylinder 11 in the circumferential direction, and the left end of each support rod 19 is inserted into the corresponding mounting hole 1 22, and the right end thereof is inserted into the corresponding mounting hole 25, and each support rod 19 is evenly provided with a plurality of through holes 26 in the length direction; The fixing assembly includes an articulated block 27, a fixing pin 28 and a limiting baffle 29; multiple groups of articulated blocks 27, multiple groups of fixing pins 28, multiple groups of limiting baffles 29 and multiple support rods 19 are arranged one by one; wherein, multiple articulated blocks 27 in each group of articulated blocks 27 are evenly fixedly connected to the outer surface of the main cylinder 12 along the axial direction, and at the same time, multiple articulated blocks 27 correspond one by one to multiple through holes 26 on the corresponding support rods 19; multiple fixing pins 28 in each group of fixing pins 28 are respectively slidably inserted into the multiple through holes 26 on the corresponding support rods 19, and at the same time, the inner ends of the multiple fixing pins 28 are respectively movably connected to the corresponding multiple articulated blocks 27, and the outer ends of the multiple fixing pins 28 are all pointed cone structures; multiple limiting baffles 29 in each group of limiting baffles 29 are respectively fixedly connected to the corresponding support rods 19, and at the same time, multiple limiting baffles 29 are respectively located on the right sides of the multiple through holes 26; As a preference, the sum of the lengths of the two radially opposite sets of fixing pins 28 in a vertical state and the outer diameter of the movable cylinder 11 is greater than the diameter of the blast hole 45; The pressure relief mechanism 3 includes a connecting cover 33, a first elastic component 35, a front end plate 32, a second elastic component 36, a rear end plate 34 and a third elastic component 40; The outer contour of the connecting cover 33 is circular, which is located on the inner side of the plurality of support rods 19 and is coaxially arranged between the first support plate 17 and the movable cylinder 11; a circular hole 37 is opened in the center of the connecting cover 33, and a plurality of through holes 5 38 are opened in the area outside the circular hole 37, and the through holes 5 38 are preferably circular holes; a connecting stud 39 is coaxially fixedly connected to the circular hole 37 on the left side of the connecting cover 33, and the connecting stud 39 is inserted into the connecting screw sleeve 21 through threaded matching; A plurality of first elastic components 35 are evenly distributed in an annular direction between the connection cover 33 and the movable cylinder 11, with the left end thereof being connected to the connection cover 33 and the right end thereof being connected to the fixed end cover 13; The outer contour of the front end plate 32 is circular, and a plurality of through holes 6 41 are evenly opened thereon and are coaxially arranged on the left side of the first support plate 17; preferably, the through holes 6 41 are circular holes; A plurality of second elastic components 36 are evenly distributed in an annular direction between the front end plate 32 and the first support plate 17, with the left end thereof connected to the front end plate 32 and the right end thereof connected to the first support plate 17; The outer contour of the rear end plate 34 is circular, and a plurality of through holes 7 42 are formed thereon and are coaxially arranged on the right side of the movable end cover 14; preferably, the through holes 7 42 are circular holes; A plurality of third elastic components 40 are evenly distributed in an annular direction between the movable end cover 14 and the rear end plate 34, with the left end thereof being connected to the movable end cover 14 and the right end thereof being connected to the rear end plate 34; When the first elastic component 35 , the second elastic component 36 and the third elastic component 40 are in a normal state, the outer ends of the plurality of fixing pins 28 in each group of fixing pins 28 are all in a state of being tilted to the left.
[0017] As a preferred embodiment, the aperture of the through hole seven 42 on the rear end plate 34 is the same as the aperture of the through hole six 41 on the front end plate 32, and the number of the through holes six 41 on the front end plate 32 is greater than the number of the through holes seven 42 on the rear end plate 34, the aperture of the through hole four 23 on the first support plate 17 is smaller than the aperture of the through hole six 41 on the front end plate 32, and the aperture of the through hole five 38 on the connecting cover 33 and the aperture of the through hole three 16 on the movable end cover 14 are both smaller than the aperture of the through hole four 23 on the first support plate 17; The front end plate, the first support plate, the connection cover, the movable cylinder, the second support plate and the rear end plate are all hollow structures with through holes, which can facilitate the smooth passage of the detonation gas.
[0018] In order to effectively ensure the elimination effect of CO while reducing the air flow resistance, the aperture of the through hole one is greater than 0 and less than 0.05mm, the aperture of the through hole two is greater than or equal to 0.05mm and less than 0.3mm, and the aperture of the through hole three is greater than or equal to 0.3mm and less than 0.7mm; the diameter of the CO eliminator particles A is 0.05-0.1mm, the particle diameter of the CO eliminator particles B is 0.3-0.6mm, and the particle diameter of the CO eliminator particles C is 0.7-1mm.
[0019] To facilitate connection, a plurality of connecting ear plates 43 are evenly fixedly connected to the left end surface of the first support plate 17 outside the circular hole 20 in an annular direction. The plurality of connecting ear plates 43 are arranged one-to-one correspondingly to the plurality of second elastic components 36, and the right ends of the plurality of second elastic components 36 are connected to the first support plate 17 through the plurality of connecting ear plates 43.
[0020] In order to ensure good impact resistance and deformation resistance, the CO elimination mechanism 1, the movable fixing mechanism 2 and the pressure relief mechanism 3 are all made of metal materials with high temperature resistance and strong pressure resistance; the thickness of the front end plate 32 and the rear end plate 34 are both 1 to 3 mm; the thickness of the first support plate 17 and the second support plate 18 are both 1 to 2 mm; the thickness of the main cylinder 12 is 1 to 1.5 mm; the thickness of the connecting cover 33, the fixed end cover 13 and the movable end cover 14 are all 1 to 2 mm.
[0021] As a preferred embodiment, the number of the support rods 19 is 4 to 12, and the number of holes on each support rod 19 is 2 to 6; the number of the fixing pins 28 is 8 to 72.
[0022] In order to ensure that the elastic component has good elastic properties and at the same time has good load-bearing capacity, the first elastic component 35, the second elastic component 36 and the third elastic component 40 are all combination springs of stainless steel corrugated springs and coil springs, the number of first elastic components 35 is 2 to 4, and the number of second elastic components 36 and third elastic components 40 are both 4 to 8.
[0023] In the process of pushing the elimination system toward the bottom of the blast hole 45, the front end plate 32 in the pressure relief mechanism 3 contacts the explosive 44, the second elastic component 36 in a relaxed state is connected to the first support plate 17 in the support frame 15, and the connecting cover 33 connected to the movable cylinder 11 through the first elastic component 35 is connected to the first support plate 17 by threaded cooperation. In the process of the movable cylinder 11 being squeezed inward, the second elastic component 40 is in a compressed state, and the fixing pin 28 extends outward along the through hole 26 on the support rod 19, and is restricted by the limit baffle 29 outside the through hole 26 to change from an inclined state to a vertical state, and is inserted into the wall of the blast hole 45.
[0024] During use, the multiple sections of explosives 44 are first pushed to the bottom of the blast hole 45 in sequence, and then the CO poisoning product in-situ efficient elimination system is pushed into the blast hole 45. In this process, the rear end plate 34 in the pressure relief mechanism 3 is squeezed toward the bottom of the hole by the thrust, and the third elastic component 40 is compressed and pushes the movable cylinder 11 to move toward the bottom of the hole after being stressed. The fixing pin 28 penetrated on the support rod 19 extends outward under the drive of the movable cylinder 11, and is quickly anchored in the hole wall of the blast hole 45 under the limiting action of the limiting baffle 29. At this time, the first elastic component 35, the second elastic component 36 and the third elastic component 40 are all in a compressed state, and then the plug 46 is blocked at the orifice of the blast hole 45; at the moment when the explosive 44 explodes, the detonation gas generated impacts the front end plate 32; in this process, the plurality of second elastic components 36 and the plurality of third elastic components 40 buffer the explosion impact force received by the elimination system as a whole, and the plurality of first elastic components 35 and the third elastic components 40 slidingly matched with the movable cylinder 11 are used to reduce the impact of the explosion. The second support plate 18 and the multiple fixing pins 28 anchored in the hole wall are used to further buffer the impact force on the movable cylinder 11; at the same time, the detonation gas enters the interior of the movable cylinder 11 through the several through holes 6 41 on the front end plate 32, the circular hole 1 20 and the several through holes 4 23 on the first support plate 17, the circular hole 3 37 and the several through holes 5 38 on the connecting cover 33, the several through holes 1 on the main cylinder 12 and the several through holes 2 on the fixed end cover 13 in sequence, and fully contacts with the first charging cylinder 4, the second charging cylinder 5 and the third charging cylinder 6, and then, the CO eliminator particles A, the CO eliminator particles B and the CO eliminator particles C inside the first charging cylinder 4, the second charging cylinder 5 and the third charging cylinder 6 fully act on the CO in the gas, realizing the efficient elimination operation of CO in the gas, wherein the gas after the CO is eliminated flows toward the orifice direction through the several through holes 3 16 on the movable end cover 14 and the several through holes 7 42 on the rear end plate 34.
[0025] In the present invention, the CO elimination mechanism is a multi-layer annular structure composed of a first charging barrel, a second charging barrel and a third charging barrel. At the same time, an outer annular ventilation area is formed between the first charging barrel and the second charging barrel, and an inner annular ventilation area is formed between the second charging barrel and the third charging barrel, so that the detonation gas can pass through the CO elimination mechanism smoothly through the outer annular ventilation area and the inner annular ventilation area. Since the first, second and third charging barrels are respectively filled with CO eliminator particles A, B and C, and at the same time, through holes are arranged on the barrel of each charging barrel, in this way, during the process of the detonation gas passing through the CO elimination mechanism, it can fully contact with the CO eliminator particles in the three charging barrels, so that the CO gas contained in the gas can be effectively eliminated by using the CO eliminator particles, and the purpose of quickly and efficiently removing toxic and harmful gases is achieved. The movable end cover is detachably covered on the right open end of the main barrel, which can facilitate opening or closing the movable barrel, and then it can facilitate loading or removing the CO elimination mechanism into or out of the movable barrel. The movable cylinder is provided with a plurality of through holes, so that the detonation gas can pass through the movable cylinder and enter the CO elimination mechanism smoothly. The second support plate is axially slidably mounted on the outer side of the movable cylinder through the circular hole in the center thereof. At the same time, a plurality of support rods surrounding the outer periphery of the movable cylinder are used to connect the second support plate and the first support plate located on the left side of the movable cylinder, so that a protection frame can be formed on the outer periphery of the movable cylinder. In this way, not only the movable cylinder can be protected, but also the movable cylinder can slide relative to the protection frame in the axial direction. The connecting screw sleeve is connected to the right side of the first support plate, and the connecting stud is connected to the left side of the connecting cover. It is convenient to fix the connecting cover between the first support plate and the movable cylinder through threaded matching, and then the movable cylinder is connected to the connecting cover by using a plurality of first elastic connecting components. While the supporting frame is used to protect the movable cylinder, a buffer force is provided for the axial movement process of the movable cylinder through the plurality of first elastic components, thereby improving the protection effect of the movable cylinder. The front end plate and the rear end plate are relatively arranged at the leftmost and rightmost positions, and a plurality of second elastic components are used to connect the front end plate and the first support plate, and a plurality of third elastic components are used to connect the rear end plate and the second support plate. The second elastic components and the third elastic components can cooperate to provide elastic forces for the movable cylinder and the support frame, thereby effectively buffering the impact force during the blasting process, thereby effectively protecting the CO elimination mechanism and the movable fixing mechanism.The outer ends of the plurality of fixing pins are all of a pointed cone structure, and at the same time, the inner ends of the fixing pins are movably connected to the main cylinder body through a hinge block, and the fixing pins of the elastic components are in an inclined state under normal conditions. In this way, when the elimination system is pushed toward the bottom of the blasthole, it can be ensured that the fixing pins can extend outward by a certain length, and can be smoothly inserted into the wall of the rock under the limiting effect of the limiting baffle, which is conducive to fixing the elimination system inside the blasthole. Combined with the buffering protection effect of the plurality of elastic components, the elimination system can be equipped with the ability to resist the blasting pressure and shock wave of the explosive. At the same time, by using a plurality of first elastic components evenly distributed in the annular direction to connect the connection cover and the movable cylinder body, by using a plurality of second elastic components evenly distributed in the annular direction to connect the front end plate and the connection cover, and by using a plurality of third elastic components evenly distributed in the annular direction to connect the movable end cover and the rear end plate, the load-bearing capacity can be effectively enhanced by a parallel connection method, and at the same time, a good pressure relief and buffering effect can be achieved, which is conducive to multiple protections for the elimination system, and the elimination system has the ability to be reused. Furthermore, when the elimination system is fixed inside the blast hole, it can also help prevent the occurrence of punching, which helps to improve the blasting effect to a certain extent. In addition, during the blasting process, the CO elimination mechanism placed in the blast hole can effectively remove CO from the gas, achieving the effect of eliminating CO from the source.
[0026] The system has an ideal CO elimination effect and high elimination efficiency. At the same time, it has strong impact resistance and self-protection ability. It can eliminate the CO generated during the operation from the source, which is beneficial to improving operation efficiency and ensuring the health and safety of workers.
Claims
1. A system for efficiently eliminating CO poisoning products in situ, comprising a CO elimination mechanism (1); characterized in that: It also includes a movable fixing mechanism (2) and a pressure relief mechanism (3); The CO elimination mechanism (1) comprises a first loading cylinder (4), a second loading cylinder (5) and a third loading cylinder (6); the first loading cylinder (4) is a double-layer closed structure cylinder with an annular accommodating cavity, a plurality of through holes 1 are arranged all over the cylinder, and the annular accommodating cavity is filled with CO elimination agent particles A; the second loading cylinder (5) is a double-layer closed structure cylinder with an annular accommodating cavity, a plurality of through holes 2 are arranged all over the cylinder, and the annular accommodating cavity is filled with CO elimination agent particles B, the aperture of the through hole 2 is larger than the aperture of the through hole 1, and the particle size of the CO elimination agent particles B is larger than the particle size of the CO elimination agent particles A; the second loading cylinder (5) is provided with a plurality of through holes 1 evenly distributed in the circumferential direction. The connecting bracket 1 (7) is coaxially fixedly connected to the inside of the first charging cylinder (4), and an outer annular ventilation area (9) is formed between the connecting bracket 1 (7) and the first charging cylinder (4); the third charging cylinder (6) is a closed cylinder with a cylindrical accommodating cavity, and a plurality of through holes 3 are arranged all over the cylinder body, and the cylindrical accommodating cavity is filled with CO eliminator particles C, the aperture of the through hole 3 is larger than the aperture of the through hole 2, and the particle size of the CO eliminator particles C is larger than the particle size of the CO eliminator particles B; the third charging cylinder (6) is coaxially fixedly connected to the inside of the second charging cylinder (5) through a plurality of connecting brackets 2 (8) evenly distributed in the circumferential direction, and an inner annular ventilation area (10) is formed between the connecting bracket 1 (7) and the second charging cylinder (5); The movable fixing mechanism (2) comprises a movable cylinder (11), a supporting frame (15) and a fixing assembly; The movable cylinder (11) comprises a main cylinder (12), a fixed end cover (13) and a movable end cover (14); the main cylinder (12) is provided with a plurality of through holes (1) throughout the cylinder body; the size of the main cylinder (12) matches the size of the CO elimination mechanism (1) and is coaxially sleeved on the outside of the CO elimination mechanism (1); the fixed end cover (13) is fixedly connected to the left open end of the main cylinder (12) and is provided with a plurality of through holes (2) throughout the surface thereof; the movable end cover (14) is detachably covered on the right open end of the main cylinder (12) and is provided with a plurality of through holes (3) throughout the surface thereof; the left end of the movable end cover (14) is fixedly connected to a right limit ring (31) at a position outside the main cylinder (12); The support frame (15) comprises a first support plate (17), a second support plate (18) and a support rod (19); the first support plate (17) has a circular outer contour, and its outer diameter is larger than the outer diameter of the movable cylinder (11); the first support plate (17) is coaxially arranged on the left side of the movable cylinder (11), a circular hole (20) is provided at the center of the first support plate (17), a plurality of mounting holes (22) are uniformly provided at the edge of the first support plate (17), a plurality of through holes (23) are provided in the area between the circular hole (20) and the plurality of mounting holes (22), and a connecting screw sleeve (21) is coaxially fixedly connected to the circular hole (20) on the right side of the first support plate (17); the second support plate (18) has a circular outer contour, and its outer diameter is the same as the outer diameter of the first support plate (17), and a circular hole (24) is provided at the center corresponding to the movable cylinder (11). , a plurality of second mounting holes (25) are provided on its edge portion corresponding to the plurality of first mounting holes (22); a left limiting ring (30) is fixedly connected to the right end of the second support plate (18) on the outside of the second circular hole (24); the left limiting ring (30) and the right limiting ring (31) are mutually limited and matched; the second support plate (18) is slidably mounted on the outside of the movable cylinder (11) through the second circular hole (24); the number of the support rods (19) is the same as the number of the plurality of first mounting holes (22) and the plurality of second mounting holes (25), the plurality of support rods (19) are evenly distributed on the outside of the movable cylinder (11) in a circumferential direction, and the left end of each support rod (19) is inserted into the corresponding first mounting hole (22), and the right end thereof is inserted into the corresponding second mounting hole (25), and each support rod (19) is evenly provided with a plurality of through holes (26) in the length direction; The fixing assembly comprises an articulated block (27), a fixing pin (28) and a limit baffle (29); a plurality of sets of articulated blocks (27), a plurality of sets of fixing pins (28), a plurality of sets of limit baffles (29) and a plurality of support rods (19) are arranged in a one-to-one correspondence; wherein a plurality of articulated blocks (27) in each set of articulated blocks (27) are evenly fixedly connected to the outer surface of the main cylinder (12) along the axial direction, and at the same time, the plurality of articulated blocks (27) correspond to a plurality of through holes (26) on the corresponding support rods (19) in a one-to-one correspondence; each set of articulated blocks (27) A plurality of fixed pins (28) in the pins (28) are respectively slidably inserted into a plurality of through holes (26) on the corresponding support rods (19), and at the same time, the inner ends of the plurality of fixed pins (28) are respectively movably connected to the corresponding plurality of hinge blocks (27), and the outer ends of the plurality of fixed pins (28) are all pointed cone structures; a plurality of limit baffles (29) in each group of limit baffles (29) are respectively fixedly connected to the corresponding support rods (19), and at the same time, the plurality of limit baffles (29) are respectively located on the right side of the plurality of through holes (26); The pressure relief mechanism (3) comprises a connecting cover (33), a first elastic component (35), a front end plate (32), a second elastic component (36), a rear end plate (34) and a third elastic component (40); The outer contour of the connecting cover (33) is circular, and it is located inside the plurality of support rods (19) and is coaxially arranged between the first support plate (17) and the movable cylinder (11); a circular hole three (37) is opened at the center of the connecting cover (33), and a plurality of through holes five (38) are opened in the area outside the circular hole three (37); a connecting stud (39) is coaxially fixedly connected to the circular hole three (37) on the left side of the connecting cover (33), and the connecting stud (39) is inserted into the connecting screw sleeve (21) through threaded engagement; A plurality of first elastic components (35) are evenly distributed in an annular direction between the connection cover (33) and the movable cylinder (11), with the left end of the first elastic components (35) being connected to the connection cover (33) and the right end of the first elastic components (35) being connected to the fixed end cover (13); The front end plate (32) has a circular outer contour, is evenly provided with a plurality of through holes (41), and is coaxially arranged on the left side of the first support plate (17); A plurality of second elastic components (36) are evenly distributed in an annular direction between the front end plate (32) and the first support plate (17), with the left ends of the second elastic components (36) being connected to the front end plate (32) and the right ends of the second elastic components (36) being connected to the first support plate (17); The rear end plate (34) has a circular outer contour and is provided with a plurality of through holes (42) which are coaxially arranged on the right side of the movable end cover (14); A plurality of third elastic components (40) are evenly distributed in an annular direction between the movable end cover (14) and the rear end plate (34), with the left end of the third elastic components (40) being connected to the movable end cover (14) and the right end of the third elastic components (40) being connected to the rear end plate (34); When the first elastic component (35), the second elastic component (36) and the third elastic component (40) are in a normal state, the plurality of fixing pins (28) in each group of fixing pins (28) are in a state where the outer ends thereof are tilted to the left.
2. The in-situ efficient elimination system for CO poisoning products according to claim 1 is characterized in that: The aperture of the through hole one is greater than 0 and less than 0.05 mm, the aperture of the through hole two is greater than or equal to 0.05 mm and less than 0.3 mm, and the aperture of the through hole three is greater than or equal to 0.3 mm and less than 0.7 mm; the diameter of the CO eliminator particles A is 0.05-0.1 mm, the diameter of the CO eliminator particles B is 0.3-0.6 mm, and the diameter of the CO eliminator particles C is 0.7-1 mm.
3. The in-situ efficient elimination system for CO poisoning products according to claim 1 is characterized in that: A portion of the left end surface of the first support plate (17) outside the circular hole 1 (20) is evenly and circumferentially fixedly connected with a plurality of connecting ear plates (43); the plurality of connecting ear plates (43) are arranged in a one-to-one correspondence with the plurality of second elastic components (36); and the right ends of the plurality of second elastic components (36) are connected to the first support plate (17) via the plurality of connecting ear plates (43).
4. The in-situ efficient elimination system for CO poisoning products according to claim 1 is characterized in that: The CO elimination mechanism (1), the movable fixing mechanism (2) and the pressure relief mechanism (3) are all made of metal materials with high temperature resistance and strong pressure resistance; the thickness of the front plate (32) and the rear plate (34) are both 1 to 3 mm; the thickness of the first support plate (17) and the second support plate (18) are both 1 to 2 mm; the thickness of the main cylinder (12) is 1 to 1.5 mm; the thickness of the connecting cover (33), the fixed end cover (13) and the movable end cover (14) are all 1 to 2 mm.
5. The in-situ efficient elimination system for CO poisoning products according to claim 1 is characterized in that: The number of the support rods (19) is 4 to 12, and the number of holes on each support rod (19) is 2 to 6; the number of the fixing pins (28) is 8 to 72.
6. The in-situ efficient elimination system for CO poisoning products according to claim 1 is characterized in that: The first elastic component (35), the second elastic component (36) and the third elastic component (40) are all springs composed of a stainless steel corrugated spring and a helical spring. The number of the first elastic components (35) is 2 to 4, and the number of the second elastic components (36) and the third elastic components (40) are both 4 to 8.
Citation Information
Patent Citations
Method for efficiently and synchronously eliminating CO products in blasting operation
CN114136165A
CO elimination module based on adsorption and catalysis synergistic effect and use method
CN116492840A
Air purifier is with high -efficient module that purifies
CN205095572U
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CN209743011U
Filter cartridge and casing
WO2020174251A1
