CN113530831A - Exhaust pipe and exhaust cavity assembly for rotor compressor - Google Patents
Exhaust pipe and exhaust cavity assembly for rotor compressor Download PDFInfo
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- CN113530831A CN113530831A CN202110863963.4A CN202110863963A CN113530831A CN 113530831 A CN113530831 A CN 113530831A CN 202110863963 A CN202110863963 A CN 202110863963A CN 113530831 A CN113530831 A CN 113530831A
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- 238000005192 partition Methods 0.000 claims abstract description 40
- 238000003466 welding Methods 0.000 claims description 11
- 230000000670 limiting effect Effects 0.000 claims description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000010949 copper Substances 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 238000002347 injection Methods 0.000 abstract description 11
- 239000007924 injection Substances 0.000 abstract description 11
- 230000035515 penetration Effects 0.000 abstract 1
- 238000009423 ventilation Methods 0.000 abstract 1
- 239000003921 oil Substances 0.000 description 32
- 239000003507 refrigerant Substances 0.000 description 19
- 239000012530 fluid Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000030279 gene silencing Effects 0.000 description 4
- 230000002035 prolonged effect Effects 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000010349 pulsation Effects 0.000 description 3
- 238000005057 refrigeration Methods 0.000 description 3
- 230000003584 silencer Effects 0.000 description 3
- 230000000903 blocking effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000010725 compressor oil Substances 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/12—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0092—Removing solid or liquid contaminants from the gas under pumping, e.g. by filtering or deposition; Purging; Scrubbing; Cleaning
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/02—Lubrication; Lubricant separation
- F04C29/026—Lubricant separation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/06—Silencing
- F04C29/065—Noise dampening volumes, e.g. muffler chambers
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
本发明公开一种用于转子压缩机的排气管及排气腔组合体，所述排气腔包括固定连接的第一端盖和第二端盖，所述第一端盖和所述第二端盖之间固定有隔板，所述隔板与所述第一端盖形成的空间构成第一腔体，所述隔板与所述第二端盖形成的空间构成第二腔体，在所述隔板与所述第二端盖间贯穿的连接有多根进气管，多根所述进气管连通所述第一腔体与所述排气腔外部，所述隔板上还开有多个通气孔，所述排气管的进气端贯穿所述第一端盖和所述隔板，所述排气管的进气端位于所述第二腔体内，所述排气管贯穿的与压缩机的壳体连接；本发明能够降低压缩机运行排气噪音，减少压缩机喷油。
The invention discloses an exhaust pipe and an exhaust cavity assembly for a rotary compressor, wherein the exhaust cavity comprises a fixedly connected first end cover and a second end cover, the first end cover and the first end cover A partition is fixed between the two end caps, the space formed by the partition and the first end cap constitutes a first cavity, and the space formed by the partition and the second end cap constitutes a second cavity, A plurality of air intake pipes are connected between the partition plate and the second end cover, and the plurality of air intake pipes communicate with the outside of the first cavity and the exhaust cavity, and the partition plate is also opened. There are a plurality of ventilation holes, the intake end of the exhaust pipe penetrates the first end cover and the partition plate, the intake end of the exhaust pipe is located in the second cavity, and the exhaust pipe The penetration is connected to the casing of the compressor; the invention can reduce the exhaust noise of the compressor during operation and reduce the oil injection of the compressor.
Description
Technical Field
The invention belongs to the technical field of refrigeration equipment, and particularly relates to an exhaust pipe and exhaust cavity assembly for a rotor compressor.
Background
The compressor is a driven fluid machine that raises low-pressure gas to high-pressure gas, and is the heart of a refrigeration system. The refrigerating cycle is powered by sucking low-temperature and low-pressure refrigerant gas from the air suction pipe, driving the piston to compress the refrigerant gas through the operation of the motor, and discharging high-temperature and high-pressure refrigerant gas to the exhaust pipe. The rotor type compressor is one of compressors, and is divided into two types, one type is a fixed-vane type and the other type is a sliding-vane type. The stator plate type rotary compressor has rotor mounted on eccentric shaft and produces volume change during rotation, and the stator plate separates the cylinders. A sliding vane rotor compressor is very similar to a vane pump. Without sealing ring, it depends on centrifugal force and lubricating oil, and the eccentricity of rotor to cylinder to reach the close fit between vane and cylinder.
Along with the improvement of living standard, people also have higher and higher requirements on the use of the compressor, the noise is high, and the oil injection of the compressor is a serious problem in the prior art of the compressor, wherein the exhaust noise is one of main noise sources of the compressor, and the oil injection problem can cause that a refrigeration system does not refrigerate, and a pipeline is blocked or even completely scrapped.
China (CN111706510A) discloses a novel rotor compressor with flexible connection and direct air suction, which comprises a casing, wherein a pump body is installed inside the casing through a plurality of elastic support members, the pump body comprises a cylinder assembly, a crankshaft is sleeved on the cylinder assembly, and a motor is sleeved above the crankshaft; the pump body also comprises a swinging or sliding rotor arranged in the cylinder component, and the rotor is sleeved with the crankshaft; the rotor is connected with the cylinder assembly through a sliding sheet, and the rotor and the sliding sheet divide an inner cavity of the cylinder assembly into a low-pressure cavity and a high-pressure cavity; the low-pressure cavity is connected with an air suction and silencing cavity through an air inlet channel, and the air suction and silencing cavity is connected with an air suction pipe of the shell through an air suction flexible connecting pipe; the high-pressure cavity is connected to an exhaust silencing cavity through an exhaust channel, and the exhaust silencing cavity is communicated with the inner cavity of the shell; although a silencer is arranged, a specific structural scheme is not disclosed, and an exhaust cavity is not arranged at an exhaust pipe in the shell to reduce noise and prevent oil injection.
China (CN213039419U) discloses an exhaust silencer for a compressor, which comprises a first end cover (1), a second end cover (2), a shell (3), a first partition plate (4), a second partition plate (5), an air inlet pipe (6), an exhaust pipe (7), a first vent pipe (8) and a second vent pipe (9), wherein the first end cover (1) and the second end cover (2) are respectively arranged at two ends of the shell (3), the first partition plate (4) and the second partition plate (5) are arranged in the middle of the shell, the air inlet pipe (6) is arranged in the first end cover (1), the exhaust pipe (7) is arranged in the second end cover (2) and the second partition plate (5), the first vent pipe (8) is arranged in the first partition plate (4) and the second partition plate (5), the second vent pipe (9) is arranged in the second partition plate (5), the running path of refrigerant airflow is lengthened, the flow rate of the refrigerant is reduced, and a plurality of expansion cavities are arranged on the airflow path, the exhaust pulsation and the noise of the compressor are effectively reduced, so that the compressor has wide market prospect; the exhaust silencer is generally applied to a reciprocating compressor, is connected to a sealed exhaust pipeline and mainly used for reducing noise and solving the problem of oil injection of the compressor.
How to provide a technical scheme that can reduce compressor noise, can reduce the compressor oil spout again, is the problem that needs to solve.
Disclosure of Invention
The invention aims to solve the problems in the prior art and provides an exhaust pipe and exhaust cavity combination for a rotor compressor, which can reduce the exhaust noise of the operation of the compressor and reduce the oil injection of the compressor.
In order to achieve the purpose, the invention adopts the technical scheme that: the utility model provides an exhaust pipe and exhaust chamber assembly for rotor compressor, the exhaust chamber includes fixed connection's first end cover and second end cover, first end cover with be fixed with the baffle between the second end cover, the baffle with the space that first end cover formed constitutes first cavity, the baffle with the space that the second end cover formed constitutes the second cavity the baffle with run through between the second end cover be connected with many intake pipes, many the intake pipe intercommunication first cavity with the exhaust chamber is outside, still open a plurality of air vents on the baffle, the inlet end of blast pipe runs through first end cover with the baffle, the inlet end of blast pipe is located in the second cavity, what the blast pipe ran through is connected with the casing of compressor.
In the above scheme, the exhaust cavity includes a first end cover and a second end cover which are fixedly connected, a partition board is fixed between the first end cover and the second end cover, a space formed by the partition board and the first end cover forms a first cavity, a space formed by the partition board and the second end cover forms a second cavity, a plurality of air inlet pipes are connected between the partition board and the second end cover in a penetrating manner, the plurality of air inlet pipes communicate with the first cavity and the outside of the exhaust cavity, the partition board is further provided with a plurality of vent holes, refrigerant gas is expanded and silenced twice in the process from the inside of the compressor to the exhaust pipe by arranging the first cavity, the second cavity, the air inlet pipes and the vent holes, the refrigerant gas operation path is prolonged, the refrigerant gas flow rate is reduced, the exhaust pulsation and noise of the compressor are reduced, and the air inlet end of the exhaust pipe penetrates through the first end cover and the partition board, the air inlet end of the exhaust pipe is positioned in the second cavity, the exhaust pipe penetrates through the second cavity and is connected with the shell of the compressor, finally, the refrigerant gas flows into the exhaust pipe from the second cavity and is discharged out of the compressor, the exhaust pipe is in through connection with the exhaust cavity at the air inlet end of the exhaust pipe, because the exhaust pipe is directly related to the size of exhaust noise and the problem of oil injection of the compressor, the exhaust cavity is arranged at the exhaust pipe to reduce the exhaust noise of the compressor and reduce the oil injection of the exhaust pipe of the compressor,
the high-pressure gas in the compressor flows through the path that the cylinder discharges the high-pressure gas which is directly discharged into the shell sealed by the compressor, the high-pressure gas in the shell enters the first cavity through the air inlet pipe, the high-pressure gas in the first cavity flows into the second cavity through the vent hole, and the high-pressure gas in the second cavity enters the exhaust pipe and finally is discharged out of the compressor.
The exhaust pipe and exhaust cavity combined body structure for the rotor compressor is characterized in that the length of the air inlet end of the exhaust pipe is prolonged on the basis of the existing rotor compressor, and the exhaust structure is arranged at the air inlet end of the exhaust pipe from nothing. Among the prior art, the compressor blast pipe is mostly with the pump body lug connection, can't handle the oil extraction problem at the blast pipe air inlet, and the blast pipe is in inside open structure, and the blast pipe is direct and casing connection, and it stretches out inside the casing connection casing not to discover similar blast pipe, does not also have similar here to set up the technique of preventing oil extraction or falling the noise structure of making an uproar.
Furthermore, a plurality of oil leakage holes are formed in the bottom surface of the second end cover.
The oil discharged to the exhaust cavity can flow to the interior of the compressor again through the oil leakage hole.
Furthermore, the oil leakage hole corresponds to the vent hole.
With the arrangement, when the oil passes through the vent hole along with the refrigerant gas from the first cavity, the oil can more conveniently flow out of the exhaust cavity.
Furthermore, a limiting structure is arranged at the position of the exhaust pipe, which is 10-60mm away from the air outlet end.
Through setting up limit structure, make things convenient for blast pipe and refrigerating system pipe connection location.
Furthermore, the limiting structure is a conical pipeline or a stepped pipeline with the length of 1-5 mm.
The exhaust pipe is provided with the conical pipeline or the stepped pipeline with the length of 1-5mm, so that the exhaust pipe is simple in structure, low in cost and good in limiting effect.
Further, the air inlet end of the air inlet pipe exceeds the end face of the second end cover by 1-10mm, and the air outlet end of the air inlet pipe exceeds the end face of the partition board by 1-20 mm.
The air inlet end of the air inlet pipe exceeds the end face of the second end cover by 1-10mm to form a circular truncated cone structure, so that oil accumulated on the end face of the second end cover is prevented from flowing out of the exhaust pipe, and the air outlet end of the air inlet pipe exceeds the end face of the partition plate by 1-20mm to form a circular truncated cone structure, so that refrigerant gas can flow better, and the circulation distance of the refrigerant gas is prolonged. The end round platform structure of the pipe can play a role in blocking oil and prolonging the flowing distance of gas.
Furthermore, the exhaust pipe and the air inlet pipe are copper pipes, and the exhaust cavity is of a steel cavity structure.
The copper pipe can prevent to rust, processes easily moreover, and the exhaust chamber is established to the steel construction and has stability, and with low costs.
Further, the first end cover and the second end cover are fixed in a welding or riveting mode. The first end cover and the second end cover are stably connected through welding or riveting.
Furthermore, the exhaust pipe is provided with a convex ring structure at the contact part of the exhaust pipe and the shell of the compressor.
The exhaust pipe is provided with the convex ring structure at the contact part of the exhaust pipe and the shell of the compressor, so that the exhaust pipe is positioned when projection welding is convenient, and the welding effect can be improved.
Furthermore, the baffle is provided with a boss positioned at the periphery of the air inlet end of the exhaust pipe, and one or more layers of filter screens are fixed in the boss.
Through setting up boss and filter screen, better prevention fluid blowout blast pipe, the fluid that blocks can flow back to inside the compressor from the oil leak hole.
Compared with the prior art, the invention has the beneficial effects that:
(1) through setting up the exhaust chamber at blast pipe inlet end, make refrigerant gas carry out twice expansion amortization from the compressor is inside to the blast pipe in-process through first cavity, second cavity, intake pipe, air vent, filter screen, prolong refrigerant moving path simultaneously, reduce refrigerant gas flow velocity, reduce the exhaust pulsation and the noise of compressor.
(2) The exhaust cavity is formed in the air inlet end of the exhaust pipe, so that oil injection of the compressor can be prevented directly, and the filter screen and the oil leakage hole structure can enable oil discharged to the exhaust cavity to flow back to the interior of the compressor.
(3) Simple structure easily manufacturing, it is with low costs.
Drawings
FIG. 1 is a schematic view of an exhaust pipe and exhaust chamber assembly for a rotor compressor according to the present invention;
FIG. 2 is a schematic sectional view taken along line A-A of FIG. 1;
FIG. 3 is a schematic sectional view taken along line B-B in FIG. 2;
FIG. 4 is a bottom view of an exhaust pipe and exhaust chamber assembly for a rotary compressor according to the present invention;
FIG. 5 is a schematic structural view in example 2 of the present invention;
in the figure: 1. an exhaust pipe; 2. an exhaust chamber; 3. a first end cap; 4. a second end cap; 5. a partition plate; 6. a first cavity; 7. a second cavity; 8. an air inlet pipe; 9. a vent hole; 10. an oil leak hole; 11. a limiting structure; 12. a convex ring structure; 13. a boss; 14. filtering with a screen; 15. a housing.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1
As shown in fig. 1-4, a discharge tube and discharge chamber combination for a rotary compressor, the exhaust cavity 2 comprises a first end cover 3 and a second end cover 4 which are fixedly connected, a partition plate 5 is fixed between the first end cover 3 and the second end cover 4, the space formed by the partition plate 5 and the first end cover 3 forms a first cavity 6, the space formed by the partition plate 5 and the second end cover 4 forms a second cavity 7, two air inlet pipes 8 are penetratingly connected between the partition plate 5 and the second end cover 4, the air inlet pipes 8 are communicated with the first cavity 6 and the outside of the exhaust cavity 2, the partition board 5 is also provided with two vent holes 9, the air inlet end of the exhaust pipe 1 penetrates through the first end cover 3 and the partition board 5, the air inlet end of the exhaust pipe 1 is positioned in the second cavity 7, and the exhaust pipe 1 penetrates through and is connected with a shell 15 of the compressor.
In the above scheme, the exhaust pipe 1 is welded on a shell 15 of the compressor in a penetrating way, the pipe diameter is 7-10mm, the exhaust cavity 2 is welded at the air inlet end of the exhaust pipe 1, because the exhaust pipe 1 is directly related to the size of exhaust noise and the problem of oil injection of the compressor, the exhaust cavity 2 is arranged at the position to reduce the exhaust noise of the compressor and reduce the oil injection of the exhaust pipe 1 of the compressor, the exhaust cavity 2 comprises a first end cover 3 and a second end cover 4 which are welded together, a partition plate 5 is fixed between the first end cover 3 and the second end cover 4, the space formed by the partition plate 5 and the first end cover 3 forms a first cavity 6, the space formed by the partition plate 5 and the second end cover 4 forms a second cavity 7, a plurality of air inlet pipes 8 are connected between the partition plate 5 and the second end cover 4 in a penetrating way, the pipe diameters are 3-6mm, and the air inlet pipes 8 are communicated with the first cavity 6 and the outside of the exhaust cavity 2, the air inlet end of the exhaust pipe 1 penetrates through the first end cover 3 and the partition plate 5 and is located in the second cavity 7, the air inlet end of the exhaust pipe 1 extends out of the end face of the partition plate 5 by 3-8mm, and finally refrigerant gas flows into the exhaust pipe 1 from the second cavity 7 and is discharged out of the compressor.
Furthermore, two oil leakage holes 10 with the aperture of 0.5-3mm are formed in the bottom surface of the second end cover 4.
The oil discharged to the discharge chamber 2 can be re-flowed to the inside of the compressor through the oil leakage hole 10.
Further, the oil leakage hole 10 corresponds to the vent hole 9.
So arranged, when oil passes through the vent hole 9 with refrigerant gas from the first cavity 6, it flows out of the discharge cavity 2 more conveniently.
Furthermore, the exhaust pipe 1 is provided with a limiting structure 11 at a position 10-60mm away from the air outlet end.
Through setting up limit structure 11, make things convenient for blast pipe 1 and refrigerating system pipe connection location.
Furthermore, the limiting structure 11 is a tapered pipeline or a stepped pipeline with the length of 1-5 mm.
The exhaust pipe 1 is provided with the 1-5mm long conical pipeline or the stepped pipeline, so that the exhaust pipe is simple in structure, low in cost and good in limiting effect.
Further, the air inlet end of the air inlet pipe 8 exceeds the end face of the second end cover 4 by 1-10mm, and the air outlet end of the air inlet pipe 8 exceeds the end face of the partition plate 5 by 1-20 mm.
The air inlet end of the air inlet pipe 8 exceeds the end face of the second end cover 4 by 1-10mm to form a circular truncated cone structure, oil accumulated on the end face of the second end cover 4 is prevented from flowing out of the exhaust pipe 1, the air outlet end of the air inlet pipe 8 exceeds the end face of the partition plate 5 by 1-20mm to form a circular truncated cone structure, refrigerant gas can flow better, and the circulation distance of the refrigerant gas is prolonged. The end round platform structure of the pipe can play a role in blocking oil and prolonging the flowing distance of gas.
Further, the exhaust pipe 1 and the intake pipe 8 are copper pipes, and the exhaust cavity 2 is of a steel cavity structure.
The copper pipe can prevent to rust, processes easily moreover, and exhaust chamber 2 establishes to the steel construction has stability, and with low costs.
Further, the first end cap 3 and the second end cap 4 are fixed by welding or riveting. The first end cap 3 is stably connected to the second end cap 4 by welding or riveting.
Furthermore, the exhaust pipe 1 is provided with a convex ring structure 12 at a contact part with a shell 15 of the compressor.
The exhaust pipe 1 is provided with the convex ring structure 12 at the contact part of the exhaust pipe 1 and the shell 15 of the compressor, so that the exhaust pipe 1 is positioned when projection welding is convenient, the contact area can be increased, heat is concentrated when welding, and the welding effect is improved.
Example 2
As shown in fig. 5, the exhaust pipe and exhaust cavity combination for the rotary compressor of the present embodiment is further optimized based on embodiment 1:
furthermore, a boss 13 positioned at the periphery of the air inlet end of the exhaust pipe 1 is arranged on the partition plate 5, and two layers of filter screens 14 are fixed in the boss 13. The fixing mode can be welding, gluing or clamping.
Through setting up boss 13 and filter screen 14, better prevention fluid blowout blast pipe 1, the fluid that blocks can flow back to the compressor inside from oil leak hole 10.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides an exhaust pipe and exhaust chamber assembly for rotor compressor, its characterized in that, the exhaust chamber includes fixed connection's first end cover and second end cover, first end cover with be fixed with the baffle between the second end cover, the baffle with the space that first end cover formed constitutes first cavity, the baffle with the space that the second end cover formed constitutes the second cavity the baffle with run through between the second end cover be connected with many intake pipes, many the intake pipe intercommunication first cavity with the exhaust chamber is outside, still open a plurality of air vents on the baffle, the inlet end of blast pipe runs through first end cover with the baffle, the inlet end of blast pipe is located in the second cavity, the blast pipe runs through be connected with the casing of compressor.
2. The exhaust pipe and chamber combination for a rotary compressor as claimed in claim 1, wherein the second end cap has a plurality of oil leakage holes formed on a bottom surface thereof.
3. The exhaust pipe and chamber combination for a rotary compressor according to claim 2, wherein the oil leakage hole is located corresponding to the air vent hole.
4. The exhaust pipe and exhaust cavity combination for the rotor compressor as claimed in claim 1, wherein the exhaust pipe is provided with a limiting structure at a distance of 10-60mm from the gas outlet end.
5. The exhaust pipe and exhaust cavity combination for the rotor compressor as claimed in claim 4, wherein the limiting structure is a tapered or stepped pipe 1-5mm long.
6. The exhaust pipe and exhaust cavity combination for the rotor compressor as claimed in claim 1, wherein the air inlet end of the air inlet pipe extends 1-10mm beyond the end face of the second end cover, and the air outlet end of the air inlet pipe extends 1-20mm beyond the end face of the partition plate.
7. The exhaust pipe and exhaust cavity combination for a rotor compressor as claimed in claim 1, wherein the exhaust pipe and the intake pipe are copper pipes, and the exhaust cavity is a steel cavity structure.
8. The exhaust pipe and exhaust cavity combination for a rotary compressor as claimed in claim 1, wherein the first end cap and the second end cap are fixed by welding or riveting.
9. The discharge tube and discharge chamber combination for a rotary compressor as claimed in claim 1, wherein said discharge tube is provided with a raised ring structure at a contact portion with a shell of said compressor.
10. The exhaust pipe and exhaust cavity combination for a rotary compressor as claimed in claim 1, wherein the partition plate is provided with a boss located at the periphery of the inlet end of the exhaust pipe, and one or more layers of filter screens are fixed in the boss.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110863963.4A CN113530831A (en) | 2021-07-29 | 2021-07-29 | Exhaust pipe and exhaust cavity assembly for rotor compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110863963.4A CN113530831A (en) | 2021-07-29 | 2021-07-29 | Exhaust pipe and exhaust cavity assembly for rotor compressor |
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| Publication Number | Publication Date |
|---|---|
| CN113530831A true CN113530831A (en) | 2021-10-22 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202110863963.4A Pending CN113530831A (en) | 2021-07-29 | 2021-07-29 | Exhaust pipe and exhaust cavity assembly for rotor compressor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115247662A (en) * | 2022-08-01 | 2022-10-28 | 湖南比扬医疗科技有限公司 | Noise reduction device and breathing machine |
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| JP2005009423A (en) * | 2003-06-19 | 2005-01-13 | Calsonic Kansei Corp | Exhaust device |
| CN104832247A (en) * | 2015-04-29 | 2015-08-12 | 麦克维尔空调制冷(武汉)有限公司 | Exhaust silencer for screw-type unit |
| CN107120288A (en) * | 2017-04-28 | 2017-09-01 | 麦克维尔空调制冷(武汉)有限公司 | A kind of exhaust silencer for screw unit |
| CN109441767A (en) * | 2018-12-11 | 2019-03-08 | 珠海格力节能环保制冷技术研究中心有限公司 | Muffler structure and compressor with it |
| CN215762256U (en) * | 2021-07-29 | 2022-02-08 | 黄石东贝压缩机有限公司 | Exhaust pipe and exhaust cavity assembly for rotor compressor |
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2021
- 2021-07-29 CN CN202110863963.4A patent/CN113530831A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP2005009423A (en) * | 2003-06-19 | 2005-01-13 | Calsonic Kansei Corp | Exhaust device |
| CN104832247A (en) * | 2015-04-29 | 2015-08-12 | 麦克维尔空调制冷(武汉)有限公司 | Exhaust silencer for screw-type unit |
| CN107120288A (en) * | 2017-04-28 | 2017-09-01 | 麦克维尔空调制冷(武汉)有限公司 | A kind of exhaust silencer for screw unit |
| CN109441767A (en) * | 2018-12-11 | 2019-03-08 | 珠海格力节能环保制冷技术研究中心有限公司 | Muffler structure and compressor with it |
| CN215762256U (en) * | 2021-07-29 | 2022-02-08 | 黄石东贝压缩机有限公司 | Exhaust pipe and exhaust cavity assembly for rotor compressor |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN115247662A (en) * | 2022-08-01 | 2022-10-28 | 湖南比扬医疗科技有限公司 | Noise reduction device and breathing machine |
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