阅读说明：本技术 一种气体压缩机 (Gas compressor ) 是由 张红 于 2021-01-12 设计创作，主要内容包括：本发明公开了一种气体压缩机,其结构包括：轴动电机、涡旋压缩盘槽、侧连通管道、阀槽座块、基座板、分支气管,本发明实现了运用涡旋压缩盘槽与侧连通管道相配合,通过侧连通管道在阻尼压气盘涡旋压缩气体中配合旋轴吊扣盘压覆摩擦回转提升侧位输出气流时让星射供气罩发散式输出效果,提升气动进发连供推进效率,且保障气压的平稳度,让低位析出的碳粉有效降低,也避免气体压缩过度聚合处出碳粉,通过流床活塞座提升上下分流层架护的汇流反馈效果,保障气旋释压量和增压量系数的平衡整体,提升二氧化碳气体压缩连供管道机械联动的高效性。(The invention discloses a gas compressor, the structure of which comprises: the invention realizes the radial output effect of a star-jet air supply cover when the vortex compression disc groove is matched with the side communicating pipeline, the damping air pressure disc vortex compression gas is matched with a rotary shaft hanging buckle disc to press, cover, rub, rotate and lift side position output air flow through the side communicating pipeline, the pneumatic feeding continuous supply propulsion efficiency is improved, the stability of air pressure is ensured, carbon powder separated out at a low position is effectively reduced, the carbon powder is prevented from being discharged from a gas compression excessive polymerization position, the converging feedback effect of upper and lower flow distribution layer frame protection is improved through a flow bed piston seat, the balance integrity of cyclone pressure release quantity and a supercharging quantity coefficient is ensured, and the high efficiency of mechanical linkage of a carbon dioxide gas compression continuous supply pipeline is improved.)

1. A gas compressor structurally comprising: shaft-driven motor (1), vortex compression dish groove (2), side intercommunication pipeline (3), valve groove seat piece (4), base plate (5), branch trachea (6), its characterized in that:

the scroll compression disc groove (2) is nested below the bottom of the shaft-driven motor (1), the side communicating pipeline (3) is tightly attached to the front side of the scroll compression disc groove (2), the valve groove seat block (4) is nested on the left side of the side communicating pipeline (3), the base plate (5) is tightly attached to the bottom surface of the scroll compression disc groove (2), and the branch air pipe (6) is installed right below the side communicating pipeline (3);

the vortex compression disc groove (2) is provided with a damping air compression disc (2A), a rotary shaft hanging buckle disc (2B), a fluid bed piston seat (2C), a star jet air supply cover (2D) and a horizontal groove shell (2E);

damping is pressed gas dish (2A) and is hung spiral shell and detain dish (2B) and cooperate with the pivot, the fluidized bed piston seat (2C) is nested under the bottom of groove casing (2E) crouches, the star is penetrated and is matched with gas cover (2D) and damping pressure gas dish (2A), the star is penetrated and is penetrated gas cover (2D) nested in the right side of groove casing (2E) crouches, the pivot is hung spiral shell and is detained dish (2B) and install on the top of groove casing (2E) crouches, groove casing (2E) are nested under the bottom of axial-motion motor (1) for sleeping in.

2. A gas compressor according to claim 1, wherein: the damping air compression disc (2A) is composed of a paddle rod vortex disc (2A1) and a spring wire plate seat (2A2), the paddle rod vortex disc (2A1) is installed on the rear side of the spring wire plate seat (2A2), and the paddle rod vortex disc (2A1) is matched with the spring wire plate seat (2A 2).

3. A gas compressor according to claim 2, wherein: the paddle rod vortex disc (2A1) is composed of a damping screw rod (2A11), a double-seam-channel lath (2A12) and a thick disc groove (2A13), the damping screw rod (2A11) is inserted and embedded in the thick disc groove (2A13), and the double-seam-channel lath (2A12) is mechanically connected with the thick disc groove (2A 13).

4. A gas compressor according to claim 1, wherein: spiral shaft hanging buckle plate (2B) comprises spiral shaft pressure plate (2B1), protruding axle cap (2B2), install under the bottom of protruding axle cap (2B2) spiral shaft pressure plate (2B1), spiral shaft pressure plate (2B1) and protruding axle cap (2B2) are nested integratively.

5. A gas compressor according to claim 4, characterized in that: the spinning shaft pressing plate (2B1) is composed of a plate groove body (2B11), a convex dome (2B12) and a ball bar truss (2B13), the convex dome (2B12) is matched with the ball bar truss (2B13), and the convex dome (2B12) is installed on the left side and the right side of the plate groove body (2B 11).

6. A gas compressor according to claim 1, wherein: the axial-motion motor (1) is composed of a tooth-groove shaft rod frame (11), a rotor block (12) and a motor shell barrel (13), the tooth-groove shaft rod frame (11) is nested below the bottom of the rotor block (12), and the rotor block (12) is installed inside the motor shell barrel (13).

7. A gas compressor according to claim 6, characterized in that: tooth's socket axostylus axostyle frame (11) comprises jack-post pole (111), tooth's socket lamella piece (112), protruding rack bar (113), jack-post pole (111) and tooth's socket lamella piece (112) weld an organic whole, tooth's socket lamella piece (112) and protruding rack bar (113) mesh mutually.

8. A gas compressor according to claim 1, wherein: the side communicating pipe (3) is composed of a gas permeable valve block (31), a propeller wing disc (32), a wheel frame groove (33) and a side anti-collision plate (34), the propeller wing disc (32) is nested on the front side of the wheel frame groove (33), the side anti-collision plate (34) is tightly attached to the right side of the wheel frame groove (33), and the gas permeable valve block (31) and the wheel frame groove (33) are of an integrated structure.

9. A gas compressor according to claim 8, wherein: ventilative lamella (31) comprise ventilative ball hole (311), bee check groove lamella piece (312), ventilative ball hole (311) is installed in the inside of bee check groove lamella piece (312), ventilative ball hole (311) link up with bee check groove lamella piece (312) each other.

Technical Field

The invention relates to a gas compressor, belonging to the field of machinery.

Background

The gas compressor utilizes the carbon dioxide gas that the air extraction needs then filters and sieves the higher gas of separation out after the polymerization, lets the gas circuit form the compressor along the pump pressure and takes over the effect of switching on regulation and control mechanical linkage to guarantee the homogeneity sense and the flexibility ratio that the gas flow scurried, the public shortcoming of treating the optimization of prior art has:

carbon chain extrusion of carbon dioxide gas compression easily causes a carbon chain twisting winding phenomenon under polymerization to make the carbon back diffusion, influence gas expansion efficiency, receive the extrusion to the divergent formula pipe-line after the gas compression, and the water conservancy diversion volume reduces, the gas compression solidification in the compressor is separated out and is swashed the surge, influences inside air current disturbance efficiency, and behind the vortex processing compressed gas, lets the logical of carbon dioxide atmospheric pressure volume reduction also influence the morphization change of gas tightness air quality.

Disclosure of Invention

Aiming at the defects in the prior art, the invention aims to provide a gas compressor to solve the problems that carbon chain extrusion of carbon dioxide gas compression easily causes a carbon chain twisting and winding phenomenon under the polymerization action, so that carbon groups are diffused, the gas expansion efficiency is influenced, divergent pipeline conveying after the gas compression is extruded, the flow guide quantity is reduced, gas in the compressor is compressed, solidified, precipitated and rapidly increased, the internal gas flow disturbance efficiency is influenced, and the form change of the airtight air quality is also influenced by the smoothness of the reduction of the carbon dioxide gas pressure after the compressed gas is treated by vortex.

In order to achieve the purpose, the invention is realized by the following technical scheme: a gas compressor structurally comprising: the vortex compression disc groove is nested under the bottom of the axial motor and is vertical to each other, the side communication pipeline is tightly attached to the front side of the vortex compression disc groove, the valve groove seat block is nested on the left side of the side communication pipeline and is collinear in the axis center, the base plate is tightly attached to the bottom surface of the vortex compression disc groove and is vertical to each other, the branch gas pipe is installed under the side communication pipeline and is located on the same vertical surface, the vortex compression disc groove is provided with a damping air pressing disc, a rotary shaft hanging buckle disc, a fluidized bed piston seat, a star-jet air supply cover and a horizontal groove shell, the damping air pressing disc and the rotary shaft hanging buckle disc are in clearance fit, the fluidized bed piston seat is nested under the bottom of the horizontal groove shell, the star-jet air supply cover is matched with the air pressing disc, and the star-jet air supply cover is nested on the right side of the horizontal groove shell, the rotary shaft hanging buckle disc is installed on the top of the horizontal groove shell, and the horizontal groove shell is nested below the bottom of the shaft-driven motor and is vertical to the shaft-driven motor.

In order to optimize the technical scheme, the method further comprises the following steps:

as a further improvement of the invention, the damping compressed air disk comprises a blade rod scroll disk and a spring wire plate seat, wherein the blade rod scroll disk is arranged on the rear side of the spring wire plate seat and is positioned on the same vertical surface, and the blade rod scroll disk and the spring wire plate seat are in clearance fit.

As a further improvement of the invention, the paddle lever vortex disc is composed of a damping screw rod, a double-seam-channel lath and a thick disc groove, wherein the damping screw rod is inserted and embedded in the thick disc groove and is positioned on the same vertical surface, and the double-seam-channel lath is mechanically connected with the thick disc groove and has a collinear axis.

As a further improvement of the invention, the rotary shaft hanging buckle disc consists of a rotary shaft pressing disc and a convex shaft cap, wherein the rotary shaft pressing disc is arranged below the bottom of the convex shaft cap and is vertical to the convex shaft cap, the rotary shaft pressing disc and the convex shaft cap are nested into a whole, and the axes of the rotary shaft pressing disc and the convex shaft cap are collinear.

As a further improvement of the invention, the rotating shaft pressure plate consists of a plate groove body, convex dome caps and a ball bar truss, wherein the convex dome caps and the ball bar truss are in clearance fit, and the convex dome caps are arranged on the left side and the right side of the plate groove body.

As a further improvement of the invention, the shaft-driven motor consists of a toothed groove shaft rod frame, a rotor block and a motor shell, wherein the toothed groove shaft rod frame is nested below the bottom of the rotor block and is positioned on the same vertical surface, and the rotor block is arranged inside the motor shell and is collinear in the axis.

As a further improvement of the invention, the toothed groove shaft rod frame is composed of a shaft column rod, toothed groove clack blocks and a convex toothed bar rod, the shaft column rod and the toothed groove clack blocks are welded into a whole and are positioned on the same vertical surface, and the toothed groove clack blocks are meshed with the convex toothed bar rod.

As a further improvement of the invention, the side communicating pipeline consists of a gas-permeable flap block, a propeller wing disc, a wheel frame groove and a side anti-collision plate, wherein the propeller wing disc is nested at the front side of the wheel frame groove, the axes of the propeller wing disc and the wheel frame groove are collinear, the side anti-collision plate is tightly attached to the right side of the wheel frame groove, and the gas-permeable flap block and the wheel frame groove are of an integral structure.

As a further improvement of the invention, the air-permeable valve block consists of an air-permeable ball hole and a honeycomb groove valve block, the air-permeable ball hole is arranged inside the honeycomb groove valve block, and the air-permeable ball hole is communicated with the honeycomb groove valve block.

As a further improvement of the invention, the double-slot channel slat is a strip frame plate structure with a left wide, a right wide, a middle narrow, an upper narrow and a lower narrow thin valve strips inserted with double slots, so that the compression operation effect of damping winding-pressure vortex bundling carbon dioxide gas is conveniently formed by adapting to propeller displacement.

As a further improvement of the invention, the convex dome cap is of a cap seat structure that a dome ball cap is sleeved from the top to the end seat of the suspender, so that the operation effect of the wheel disc rotating around the pneumatic power source shaft in a movable pushing linkage manner can be conveniently formed by the arc surface settling, jacking and adapting spring plates.

As a further improvement of the invention, the tooth socket petal is a tooth socket block structure with convex arcs of left and right narrow hollow wide upper and lower petals, which is convenient for adapting the meshing degree left and right to improve the reciprocating linkage of tooth pitch lifting and circling.

As a further improvement of the invention, the air-permeable ball hole is of a through hole structure that the outer hole is sleeved with the right side of the inner air-permeable twill film and is provided with balls, so that the hole end can conveniently constrict airflow to form communicated air permeability and the operation efficiency of compressed gas feeding and conveying.

Advantageous effects

The invention relates to a gas compressor, wherein a worker starts a shaft-driven motor to enable a tooth socket shaft lever frame to be inserted into a rotor block and the bottom of a motor shell, so that a shaft post rod drives a tooth socket petal block to be meshed with a convex rack rod to draw a rotary shaft hanging buckle disc of a vortex compression disc groove to subside and rotate a friction damping air pressing disc to move, the rotary shaft air pressing disc drives a disc groove body to link a convex pressing dome cap and a truss ball rod to rotate and wind a spring screw plate seat under the traction of a convex shaft cap, thereby bouncing a damping screw rod of a paddle rod vortex disc and a double-seam channel plate carry out vortex air intake compression operation in a thick disc groove, then the bottom part of a horizontal groove shell is subjected to flow unloading through a flow bed piston seat and a star jet air supply cover, a communicating pipeline at the right conduction side forms an effect of butt joint valve groove seat block and branch air pipes on the butt joint aerodynamic mechanical action operation, the excessive polymerization pressure of the gas compressor on carbon dioxide is ensured, and the, the maneuverability and the stability of the gas compressor are guaranteed.

The invention has the following advantages after operation:

the application vortex compression dish groove cooperatees with the side intercommunication pipeline, through the side intercommunication pipeline cooperation spiral axle hang the spiral shaft buckle dish in the damping air compression dish vortex compressed gas and press and cover friction gyration promotion side position output air current time let the star penetrate the gas supply cover and disperse formula output effect, promote pneumatics and advance and supply the propulsive efficiency even, and ensure the stationarity of atmospheric pressure, let the carbon dust of low level separation effectively reduce, also avoid the excessive polymerization department of gas compression to go out the carbon dust, through the feedback effect that converges that reposition of redundant personnel shelf protected about the bed piston seat promotes, guarantee the balanced whole of cyclone release pressure volume and pressure boost coefficient, promote the high efficiency that carbon dioxide gas compression even supplied pipeline mechanical linkage.

Drawings

Other features, objects, and advantages of the present invention will become more apparent from the following detailed description of the embodiments of the invention when taken in conjunction with the accompanying drawings, in which:

fig. 1 is a schematic structural diagram of a gas compressor according to the present invention.

FIG. 2 is a schematic side sectional view of the axial motor and the scroll compressor groove of the present invention.

FIG. 3 is a detailed side cross-sectional structural view of the scroll compression disk slot and side communication duct of the present invention.

FIG. 4 is a schematic side sectional view of the working states of the scroll compression disk groove, the damping air compression disk and the spiral shaft hanging buckle disk of the present invention.

FIG. 5 is a side enlarged view of the spline shaft holder of the structure of FIG. 2a according to the present invention.

FIG. 6 is an enlarged side view of the b-structure flap of FIG. 3 according to the present invention.

Fig. 7 is a side sectional view schematically showing the operation state of the paddle lever scroll according to the present invention.

FIG. 8 is a schematic side sectional view showing the operation of the spinning disk according to the present invention.

Description of reference numerals: a shaft-driven motor-1, a vortex compression disc groove-2, a side communicating pipeline-3, a valve groove seat block-4, a base plate-5, a branch air pipe-6, a damping air compression disc-2A, a rotary shaft hanging buckle disc-2B, a fluid bed piston seat-2C, a star-jet air supply hood-2D, a horizontal groove shell-2E, a paddle rod vortex disc-2A 1, a reed wire plate seat-2A 2, a damping screw rod-2A 11, a double seam channel slat-2A 12, a thick disc groove-2A 13, a rotary shaft pressure disc-2B 1, a convex shaft cap-2B 2, a disc groove body-2B 11, a convex pressure cap-2B 12, a ball rod truss-2B 13, a tooth groove shaft rod frame-11, a rotor block-12, a motor shell-13, a shaft column rod-111, a lobe block-112, a convex tooth bar rod-113, A ventilating valve block-31, a propeller wing disc-32, a wheel frame groove-33, a side anti-collision plate-34, a ventilating ball hole-311 and a honeycomb groove valve block-312.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.

The first embodiment is as follows:

referring to fig. 1 to 8, the present invention provides a gas compressor, which includes: the vortex compressor comprises a shaft-driven motor 1, a vortex compression disc groove 2, a side communication pipeline 3, a valve groove seat block 4, a base plate 5 and a branch air pipe 6, wherein the vortex compression disc groove 2 is nested under the bottom of the shaft-driven motor 1 and is vertical to each other, the side communication pipeline 3 is tightly attached to the front side of the vortex compression disc groove 2, the valve groove seat block 4 is nested at the left side of the side communication pipeline 3 and is collinear in the axis center, the base plate 5 is tightly attached to the bottom surface of the vortex compression disc groove 2 and is vertical to each other, the branch air pipe 6 is installed under the side communication pipeline 3 and is positioned on the same vertical surface, the vortex compression disc groove 2 is provided with a damping air compression disc 2A, a rotary shaft hanging buckle disc 2B, a fluid bed piston seat 2C, a star-jet air supply cover 2D and a horizontal groove shell 2E, the damping air compression disc 2A and the rotary shaft hanging buckle disc 2B are in clearance fit, the fluid bed piston seat 2C is nested under the bottom of the horizontal groove shell 2, the star penetrates air feed cover 2D and damping air compression disc 2A to adopt interference fit, the star penetrates air feed cover 2D to be nested on the right side of horizontal groove shell 2E, spiral shaft hanging buckle disc 2B is installed on the top of horizontal groove shell 2E, horizontal groove shell 2E is nested under the bottom of shaft-driven motor 1 and mutually perpendicular.

Referring to fig. 4, the damping air compression disc 2A is composed of a paddle rod scroll 2A1 and a spring wire plate seat 2A2, the paddle rod scroll 2A1 is installed at the rear side of the spring wire plate seat 2A2 and is located on the same vertical plane, the paddle rod scroll 2A1 and the spring wire plate seat 2A2 are in clearance fit, the rotating shaft hanging buckle disc 2B is composed of a rotating shaft pressure plate 2B1 and a protruding shaft cap 2B2, the rotating shaft pressure plate 2B1 is installed below the bottom of the protruding shaft cap 2B2 and is perpendicular to each other, the rotating shaft pressure plate 2B1 and the protruding shaft cap 2B2 are nested into a whole and have collinear axes, and a horizontal-longitudinal rotation operation effect of low-position wind-resisting rotation, high-position sinking pushing friction fit linkage is formed by the paddle rod scroll 2A1 and the rotating shaft pressure plate 2B 1.

Referring to fig. 7, the paddle rod scroll 2a1 is composed of a damping screw rod 2a11, a double-slot lath 2a12 and a thick disc groove 2a13, the damping screw rod 2a11 is inserted and embedded in the thick disc groove 2a13 and is located on the same vertical plane, the double-slot lath 2a12 is mechanically connected with the thick disc groove 2a13 and has a collinear axis, the double-slot lath 2a12 is a strip frame plate structure with narrow left and right sides, wide middle, narrow upper and lower sides and double slots for inserting thin strips, so that the matching of the displacement of the paddles is facilitated to form a compression operation effect of damping winding-pressing scroll to collect carbon dioxide gas, and a lateral strip damping wind pressure is formed by the damping screw rod 2a11 and the double-slot lath 2a12 to be pressed into the wind gap to form a scroll compression treatment effect.

Referring to fig. 8, the rotating shaft pressure plate 2B1 is composed of a plate groove 2B11, a convex dome 2B12 and a ball bar truss 2B13, the convex dome 2B12 and the ball bar truss 2B13 are in clearance fit, the convex dome 2B12 is installed on the left side and the right side of the plate groove 2B11, the convex dome 2B12 is a cap base structure that the top of the convex dome 2B12 is connected with a suspension rod end base in a sleeved mode through a dome ball cap, so that a wheel disc formed by an arc surface settling and pressing adaptive spring plate is convenient to move around an air power source to push and interlock a rotary operation effect, and the convex dome 2B12 is used for settling and pulling the suspension ball bar truss 2B13 to balance and adjust the pressure to be uniform operation effect.

Referring to fig. 2, the axial-motion motor 1 is composed of a cogging shaft holder 11, a rotor block 12 and a motor housing 13, the cogging shaft holder 11 is nested below the bottom of the rotor block 12 and is located on the same vertical plane, the rotor block 12 is installed inside the motor housing 13, the axes of the rotor block and the rotor block are collinear, and the cogging shaft holder 11 is inserted into the rotor block 12 to form a positive and negative rotation adaptive linkage operation effect of the motor.

Referring to fig. 5, the tooth socket shaft rod frame 11 is composed of a shaft column rod 111, a tooth socket petal 112 and a convex tooth bar rod 113, the shaft column rod 111 and the tooth socket petal 112 are welded into a whole and are located on the same vertical plane, the tooth socket petal 112 is meshed with the convex tooth bar rod 113, the tooth socket petal 112 is a tooth socket block structure with left and right narrow hollow wide convex arcs of upper and lower petals, the tooth pitch lifting and circling reciprocating linkage is improved by adapting the meshing degree from left to right, and the tooth socket petal 112 and the convex tooth bar rod 113 form a frame meshing clamping effect.

The working process is as follows: the staff starts the shaft-driven motor 1 to make the tooth-grooved shaft rod frame 11 insert the rotor block 12 and the bottom of the motor shell 13, the shaft column rod 111 drives the tooth-grooved petal block 112 to engage with the rack rod 113 to draw the rotary shaft hanging buckle disc 2B of the vortex compression disc groove 2 to subside and rotate the friction damping air pressing disc 2A, the rotary shaft pressing disc 2B1 drives the disc groove body 2B11 to link the convex pressing dome 2B12 and the ball bar truss 2B13 to rotate and wind the pressure spring screw plate seat 2A2 under the traction of the convex shaft cap 2B2, so that the damping screw 2A11 of the springing paddle rod vortex disc 2A1 and the double-slit channel plate 2A12 perform vortex air intake compression operation in the thick disc groove 2A13, then the bottom flow unloading and the right side communication pipeline 3 of the horizontal groove shell 2E through the fluid bed piston seat 2C and the star-jet air supply cover 2D form the effect of butt-valve seat block 4 and the butt-joint mechanical operation of the branch air pipe 6, and the pneumatic gas polymerization prevention compressor by the pneumatic pressure, the uniform texture of the compression and continuous supply for the burst output is also improved, and the maneuverability and the stability of the gas compressor are guaranteed.

Example two:

referring to fig. 1 to 8, the present invention provides a gas compressor, which is otherwise the same as embodiment 1 except that:

referring to fig. 3, the side communicating pipe 3 is composed of a gas permeable flap block 31, a propeller wing disc 32, a wheel frame groove 33, and a side anti-collision plate 34, the propeller wing disc 32 is nested in the front side of the wheel frame groove 33, the axes of the propeller wing disc 32 are collinear, the side anti-collision plate 34 is tightly attached to the right side of the wheel frame groove 33, the gas permeable flap block 31 and the wheel frame groove 33 are of an integral structure, and the forward type continuous supply homogeneity after gas compression is improved by the fact that the propeller wing disc 32 is matched with a star-shooting pipe at the front end of the wheel frame groove 33 to diffuse outward-winding gas flow continuous supply operation.

Referring to fig. 6, the gas flap block 31 is composed of a gas ball hole 311 and a bee-lattice groove flap block 312, the gas ball hole 311 is installed inside the bee-lattice groove flap block 312, the gas ball hole 311 is communicated with the bee-lattice groove flap block 312, the gas ball hole 311 is a through-hole structure in which an outer hole is annularly sleeved on the right side of an inner gas-permeable twill film and provided with balls, so that the hole end is convenient to constrict air flow to form communication gas permeability and compressed gas forward transmission operation efficiency, and the gas pressure fed back by the reciprocating shuttle matching of the gas ball hole 311 in the bee-lattice groove flap block 312 ensures the gas permeability of the through-hole and the stability of gas pressure balance adjustment.

The high-level air current motor of drawing a bunch forms the vortex gas compression operation effect through earlier stage drive disk pressure, and the unloading frame that ensures high low level flow distribution layer protects, lets inside groove release pressure after pile up star shot pipe around the outer exhaust coil cap department, and the ventilative lamella piece 31 of cooperation side intercommunication pipeline 3 promotes whole air permeability and the effect of atmospheric pressure balance adjustment at rotor wing dish 32 and wheel frame groove 33 support intercommunication ventilative ball hole 311 and bee check groove lamella piece 312.

The invention achieves the effect of diverging output of a star-shooting gas supply hood 2D when applying the vortex compression disk groove 2 to be matched with the side communication pipeline 3, matching a rotary shaft hanging buckle disk 2B in the vortex compressed gas of a damping gas compression disk 2A through the side communication pipeline 3 to press, rub, rotate and lift side output gas flow, improves pneumatic feeding and continuous feeding efficiency, ensures the stability of gas pressure, effectively reduces carbon powder separated out at a low position, avoids carbon powder from being discharged at a gas compression over-polymerization position, improves the confluence effect of upper and lower shunting layer frames through a fluid bed piston seat 2C, ensures the balance integrity of cyclone pressure release quantity and pressurization quantity coefficients, improves the high efficiency of mechanical linkage of the carbon dioxide gas compression continuous supply pipeline, and solves the problem that carbon chain twisting phenomenon is easily caused by carbon chain extrusion of carbon dioxide gas compression under the polymerization action, thereby make carbon back diffusion, influence gas expansion efficiency, receive the extrusion to the divergent formula pipe-line transportation after the gas compression, and the water conservancy diversion volume reduces, and the gas compression solidification in the compressor is precipitated and is increased suddenly, influences inside air current disturbance efficiency, and behind the vortex processing compressed gas, lets the logical of carbon dioxide atmospheric pressure volume reduction also influence the morphization of gas tightness air quality and change the problem.

The specific embodiments described herein are merely illustrative of the invention. Various modifications or additions may be made to the described embodiments or alternatives may be employed by those skilled in the art without departing from the scope of the invention or exceeding the scope of the claims appended hereto.