CN112268006A - Methane tail gas booster compressor - Google Patents

Methane tail gas booster compressor Download PDF

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Publication number
CN112268006A
CN112268006A CN202011206498.9A CN202011206498A CN112268006A CN 112268006 A CN112268006 A CN 112268006A CN 202011206498 A CN202011206498 A CN 202011206498A CN 112268006 A CN112268006 A CN 112268006A
Authority
CN
China
Prior art keywords
impeller
diffuser
supercharger
vane
blades
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202011206498.9A
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Chinese (zh)
Inventor
孙忠良
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Site Machinery Manufacturing Co ltd
Original Assignee
Shenyang Site Machinery Manufacturing Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenyang Site Machinery Manufacturing Co ltd filed Critical Shenyang Site Machinery Manufacturing Co ltd
Priority to CN202011206498.9A priority Critical patent/CN112268006A/en
Publication of CN112268006A publication Critical patent/CN112268006A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08Centrifugal pumps
    • F04D17/10Centrifugal pumps for compressing or evacuating
    • F04D17/12Multi-stage pumps
    • F04D17/122Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/286Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444Bladed diffusers

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to a methane tail gas supercharger, which is characterized in that: (1) the shell of the supercharger is divided into an upper shell and a lower shell from the horizontal plane of the rotating shaft, the upper shell is fixed with the lower shell through sealing bodies at two ends, and the lower shell is fixed on the support; (2) the impeller, the spacer bush, the balance disc, the thrust disc and other parts are arranged on the main shaft to form an important part of the supercharger, namely a rotor, and the rotor is arranged on the lower shell through a bearing and a bearing seat; (3) the diffuser adopts the combination of a vaneless diffuser and a vane diffuser, wherein the vaneless diffuser is arranged in front of the vane diffuser, and the vane diffuser is arranged behind the vane diffuser; (4) a plurality of cascade impellers are adopted, and between two adjacent impellers, the blade of the latter impeller is arranged to deflect a certain angle relative to the blade of the former impeller; (5) the blades are of a backward bending type constant-strength structure, the blades and the hub are integrated, and the blades and the wheel disc are connected by adopting a welding structure; (6) two air inlet air cylinders and two air outlet air cylinders are arranged below the supercharger.

Description

Methane tail gas booster compressor
Technical Field
The invention relates to the technical field of superchargers, in particular to a methane tail gas supercharger which is matched with an ethylene three-machine in operation.
Background
The cracking of petroleum hydrocarbon to prepare ethylene is the process of decomposing macromolecular hydrocarbon in cracking material to produce small molecular hydrocarbon in the condition of isolating air and high temperature. The overall cracking process is a very complex process, and includes reactions such as dehydrogenation, chain scission, diene synthesis, ring opening decomposition, dealkylation or dehydrogenation of alkyl aromatics, hydrogenation, aromatization, isomerization, polymerization and the like, so as to obtain ethylene, propylene, butadiene, aromatics and other products, such as hydrogen, methane and the like. Methane is the second largest greenhouse gas, accounting for 14% of global greenhouse gas emissions, and has more than one third of its role in anthropogenic climate warming, whereas methane is a major component of natural gas from an energy and economic perspective, and is a valuable, clean energy source.
In order to be matched with ethylene production and solve the problem of recycling the methane tail gas during the operation of an ethylene three-machine, a device for pressurizing the methane tail gas is required, and the aim of the invention is to provide the device.
Disclosure of Invention
The invention seeks a methane tail gas supercharger in order to solve the problems of recycling of tail gas during the operation of an ethylene three-machine and reducing the production cost.
The invention relates to a methane tail gas supercharger, which mainly comprises: main shaft, impeller, spacer bush, thrust disc, balance disc, diffuser, bend, exit volute chamber, sealed, bearing group part, casing etc. its characterized in that:
(1) the shell of the supercharger is divided into an upper shell and a lower shell from the horizontal plane of the rotating shaft, the upper shell is fixed with the lower shell through sealing bodies at two ends, and the lower shell is fixed on the support;
(2) the impeller, the spacer bush, the balance disc, the thrust disc and other parts are arranged on the main shaft to form an important part of the supercharger, namely a rotor, and the rotor is arranged on the lower shell through a bearing and a bearing seat;
(3) the diffuser adopts the combination of a vaneless diffuser and a vane diffuser, wherein the vaneless diffuser is arranged in front of the vane diffuser, and the vane diffuser is arranged behind the vane diffuser;
(4) a plurality of cascade impellers are adopted, and between two adjacent impellers, the blade of the latter impeller is arranged to deflect a certain angle relative to the blade of the former impeller;
(5) the blades are of a backward bending type constant-strength structure, the blades and the hub are integrated, and the blades and the wheel disc are connected by adopting a welding structure;
(6) two air inlet air cylinders and two air outlet air cylinders are arranged below the supercharger.
The invention relates to a methane tail gas supercharger, wherein between two adjacent impellers, the blade of the latter impeller is arranged to deflect 5-15 degrees relative to the blade of the former impeller.
According to the methane tail gas supercharger, the impeller is a stainless steel closed impeller, the blades are in a blade form of a backward bending structure, and compared with open impellers of other products, the whole efficiency of the unit is greatly improved.
The methane tail gas supercharger is a product designed through continuous practice and research on the basis of the prior art, and careful research and improvement are made on all aspects of the unit, so that the working efficiency, the manufacturing and maintenance cost and the service life of the product are greatly improved. The methane tail gas supercharger is uniformly favored by users in the using process of the users, and is welcomed by the users.
Drawings
Fig. 1 is a front sectional view of a methane tail gas booster of the present invention.
Fig. 2 is an external view of a methane tail gas booster according to the present invention.
The components in the above figures are as follows: the air inlet cylinder 1, 3, the air outlet cylinder 2, 4, the upper casing 5, the lower casing 6, the main shaft 7, the impeller 8, the sealing component 9, the partition board 10, the bearing 11, the coupler 12 and the bolt 13.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and embodiments.
According to the technical requirements of figures 1 and 2, parts including air inlet cylinders 1 and 3, air outlet cylinders 2 and 4, an upper casing 5, a lower casing 6, a main shaft 7, an impeller 8, a sealing assembly 9, a partition plate 10, a bearing 11 and a coupling 12 are machined and manufactured respectively, the impeller, a spacer bush, a balance disc, a thrust disc and other parts are sequentially installed on the main shaft to form a rotor, and the coupling is installed at one end of the rotor so as to be connected with a driving machine.
Example 1
The embodiment 1 is a seven-stage centrifugal supercharger, wherein an impeller adopts a ternary-plus-binary closed impeller, blades of the impeller adopt a backward bending structure, and the blades of the front impeller and the rear impeller deflect by 5 degrees; the diffuser adopts a vaneless diffuser and a vane diffuser.
Example 2
In this embodiment 2, the centrifugal supercharger is an eight-stage centrifugal supercharger, the impeller is a ternary plus binary closed impeller, the blades of the impeller are of a backward bending structure, and the blades of the front impeller and the rear impeller deflect by 10 degrees; the diffuser adopts a vaneless diffuser and a vane diffuser.
Example 3
In this embodiment 3, an eight-stage centrifugal supercharger is adopted, an impeller is a ternary plus binary closed impeller, blades of the impeller are of a backward bending structure, and the blades of the front impeller and the rear impeller deflect by 15 degrees; the diffuser adopts a vaneless diffuser and a vane diffuser.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and it will be apparent to those skilled in the art that various changes and modifications can be made in the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (3)

1. A methane tail gas booster compressor mainly comprises: main shaft, impeller, spacer bush, thrust disc, balance disc, diffuser, bend, exit volute chamber, sealed, bearing group part, casing etc. its characterized in that:
(1) the shell of the supercharger is divided into an upper shell and a lower shell from the horizontal plane of the rotating shaft, the upper shell is fixed with the lower shell through sealing bodies at two ends, and the lower shell is fixed on the support;
(2) the impeller, the spacer bush, the balance disc, the thrust disc and other parts are arranged on the main shaft to form an important part of the supercharger, namely a rotor, and the rotor is arranged on the lower shell through a bearing and a bearing seat;
(3) the diffuser adopts the combination of a vaneless diffuser and a vane diffuser, wherein the vaneless diffuser is arranged in front of the vane diffuser, and the vane diffuser is arranged behind the vane diffuser;
(4) a plurality of cascade impellers are adopted, and between two adjacent impellers, the blade of the latter impeller is arranged to deflect a certain angle relative to the blade of the former impeller;
(5) the blades are of a backward bending type constant-strength structure, the blades and the hub are integrated, and the blades and the wheel disc are connected by adopting a welding structure;
(6) two air inlet air cylinders and two air outlet air cylinders are arranged below the supercharger.
2. The methane tail gas supercharger according to claim 1, wherein between two adjacent impellers, the vane of the latter impeller is arranged to be deflected by 5 to 15 degrees with respect to the vane of the former impeller.
3. The methane tail gas booster according to claim 1, wherein the impeller is a stainless steel shrouded impeller, and the vanes are in the form of backward-curved vanes.
CN202011206498.9A 2020-11-03 2020-11-03 Methane tail gas booster compressor Pending CN112268006A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011206498.9A CN112268006A (en) 2020-11-03 2020-11-03 Methane tail gas booster compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011206498.9A CN112268006A (en) 2020-11-03 2020-11-03 Methane tail gas booster compressor

Publications (1)

Publication Number Publication Date
CN112268006A true CN112268006A (en) 2021-01-26

Family

ID=74345541

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011206498.9A Pending CN112268006A (en) 2020-11-03 2020-11-03 Methane tail gas booster compressor

Country Status (1)

Country Link
CN (1) CN112268006A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103807185A (en) * 2014-02-13 2014-05-21 沈阳斯特机械制造有限公司 Multistage centrifugal compressor capable of being detached horizontally
CN203770209U (en) * 2014-02-13 2014-08-13 沈阳斯特机械制造有限公司 Enclosed impeller of centrifugal compressor
CN104632645A (en) * 2014-11-06 2015-05-20 沈阳斯特机械制造有限公司 Double inlet multistage centrifugal compressor
CN205669505U (en) * 2016-03-17 2016-11-02 北京斯特透平机械有限公司 A kind of centrifugal compressor of band Series Connection Type Dry Gas
CN106151063A (en) * 2016-08-29 2016-11-23 沈阳斯特机械制造有限公司 A kind of CO recycle gas compressor
CN107387432A (en) * 2017-08-15 2017-11-24 沈阳斯特机械制造有限公司 It is a kind of to be alkylated applicable middle aerating formula multistage centrifugal compressor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103807185A (en) * 2014-02-13 2014-05-21 沈阳斯特机械制造有限公司 Multistage centrifugal compressor capable of being detached horizontally
CN203770209U (en) * 2014-02-13 2014-08-13 沈阳斯特机械制造有限公司 Enclosed impeller of centrifugal compressor
CN104632645A (en) * 2014-11-06 2015-05-20 沈阳斯特机械制造有限公司 Double inlet multistage centrifugal compressor
CN205669505U (en) * 2016-03-17 2016-11-02 北京斯特透平机械有限公司 A kind of centrifugal compressor of band Series Connection Type Dry Gas
CN106151063A (en) * 2016-08-29 2016-11-23 沈阳斯特机械制造有限公司 A kind of CO recycle gas compressor
CN107387432A (en) * 2017-08-15 2017-11-24 沈阳斯特机械制造有限公司 It is a kind of to be alkylated applicable middle aerating formula multistage centrifugal compressor

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Application publication date: 20210126

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