CN112719788A - Manufacturing method of injection module of large exhaust system - Google Patents

Manufacturing method of injection module of large exhaust system Download PDF

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Publication number
CN112719788A
CN112719788A CN202011464732.8A CN202011464732A CN112719788A CN 112719788 A CN112719788 A CN 112719788A CN 202011464732 A CN202011464732 A CN 202011464732A CN 112719788 A CN112719788 A CN 112719788A
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CN
China
Prior art keywords
barrel
gas collecting
pipe
collecting ring
spray pipe
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.)
Withdrawn
Application number
CN202011464732.8A
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Chinese (zh)
Inventor
陈立平
庄宇
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 Aerospace Xinguang Pressure Vessel Co ltd
Original Assignee
Shenyang Aerospace Xinguang Pressure Vessel 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.)
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Publication date
Application filed by Shenyang Aerospace Xinguang Pressure Vessel Co ltd filed Critical Shenyang Aerospace Xinguang Pressure Vessel Co ltd
Priority to CN202011464732.8A priority Critical patent/CN112719788A/en
Publication of CN112719788A publication Critical patent/CN112719788A/en
Withdrawn legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Abstract

The invention discloses a manufacturing method of an injection module of a large-scale exhaust system, which solves the problem that the manufacturing quality of the injection module of the exhaust system cannot be ensured, and the key points of the technical scheme are as follows: the manufacturing method comprises the following steps: s1: processing a barrel, namely taking a barrel raw material for blanking, cutting a groove on the barrel, assembling and welding a barrel winding drum, assembling and welding a longitudinal seam on the barrel, assembling and welding a circular seam on the barrel, carrying out nondestructive detection on the barrel, and perforating the barrel; s2: processing a gas collecting ring assembly, wherein a gas collecting pipe adopts intermediate frequency heating to form a bent pipe, the bent pipe is assembled and welded to form a gas collecting ring, the gas collecting ring is welded and subjected to nondestructive testing, the gas collecting ring is perforated, and the gas collecting ring is welded with a gas inlet connecting pipe and a gas outlet connecting pipe; s3: processing a spray pipe, namely taking a spray pipe raw material forge piece, roughly milling, performing stress relief heat treatment, finely milling and drilling the spray pipe; s4: the method comprises the steps of spray pipe assembly, connector manufacturing, connector and spray pipe assembly, connector and barrel welding and spray pipe and connector heat treatment, and achieves the purpose of high-quality injection module processing and manufacturing.

Description

Manufacturing method of injection module of large exhaust system
Technical Field
The invention belongs to the technical field of ejectors, and particularly relates to a manufacturing method of an ejector module of a large-scale exhaust system.
Background
The high enthalpy gas wind tunnel facility is an important infrastructure for developing a certain aircraft, and has great significance for promoting the development of certain aircrafts and combined engines in China. The exhaust system injection module injects fuel gas in the fuel gas wind tunnel into air through high-pressure airflow, so that continuous operation of fuel gas wind tunnel facilities is guaranteed, and the exhaust system injection module is an important component of high enthalpy fuel gas wind tunnel test facilities.
However, the quality of the manufactured injection module is poor in the existing injection module manufacturing method, and the application of a large-scale high-precision exhaust system cannot be met.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a manufacturing method of a high-quality large-scale exhaust system injection module.
The purpose of the invention is realized as follows: a manufacturing method of an injection module of a large-scale exhaust system comprises a cylinder body, a gas collecting ring assembly and a spray pipe, wherein the gas collecting ring assembly comprises a gas collecting pipe, a gas inlet connecting pipe and a gas outlet connecting pipe, the spray pipe is assembled with a connecting piece, and the manufacturing method comprises the following steps:
s1: processing a barrel, namely taking a barrel raw material for blanking, cutting a groove on the barrel, assembling and welding a barrel winding drum, assembling and welding a longitudinal seam on the barrel, assembling and welding a circular seam on the barrel, carrying out nondestructive detection on the barrel, and perforating the barrel;
s2: processing a gas collecting ring assembly, wherein a gas collecting pipe adopts intermediate frequency heating to form a bent pipe, the bent pipe is assembled and welded to form a gas collecting ring, the gas collecting ring is welded and subjected to nondestructive testing, the gas collecting ring is perforated, and the gas collecting ring is welded with a gas inlet connecting pipe and a gas outlet connecting pipe;
s3: processing a spray pipe, namely taking a spray pipe raw material forge piece, roughly milling, performing stress relief heat treatment, finely milling and drilling the spray pipe;
s4: assembling the spray pipe, manufacturing a connecting piece, assembling the connecting piece and the spray pipe, welding the connecting piece and the cylinder body, and carrying out heat treatment on the spray pipe and the connecting piece.
The invention is further optimized as follows: in the step S1, after the longitudinal seam of the cylinder is welded, the cylinder is rounded.
The invention is further optimized as follows: in the step S1, the nondestructive testing of the welding of the gas collecting ring adopts 100% ray detection and 100% magnetic powder detection.
The invention is further optimized as follows: in step S4, the connecting member is threadedly assembled with the nozzle.
Compared with the prior art, the invention has the outstanding and beneficial technical effects that: the injection module is subjected to nondestructive testing after the barrel is manufactured, so that the quality of the formed barrel is effectively ensured, the nondestructive testing is performed after the gas collecting ring is welded, the forming quality of the gas collecting ring is ensured, the deformation of the welded nozzle is prevented by adopting stress-relief heat treatment after the nozzle is subjected to rough milling, meanwhile, the nozzle is connected with the barrel through the connecting piece, the stability of the connection between the nozzle and the barrel is ensured, and the overall quality of the injection module is improved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
figure 2 is a schematic view of the cartridge of the present invention.
In the figure: 1-cylinder, 2-spray pipe, 3-gas collecting pipe, 4-gas inlet connecting pipe, 5-gas outlet connecting pipe and 6-connecting piece.
Detailed Description
In order to make those skilled in the art better understand the technical solution of the present invention, the following description, with reference to the drawings in the embodiments of the present invention, clearly and completely describes the technical solution in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present invention without making any creative effort, shall fall within the protection scope of the present invention.
The embodiment provides a manufacturing method of an injection module of a large-scale exhaust system, which comprises a cylinder body 1, a gas collecting ring assembly and a spray pipe 2, wherein the gas collecting ring assembly comprises a gas collecting ring 3, a gas inlet connecting pipe 4 and a gas outlet connecting pipe 5, the spray pipe is assembled with a connecting piece 6, and the manufacturing method comprises the following steps:
s1: barrel processing, taking barrel raw materials for blanking: the diameter of the cylinder body is phi 2950mm, the wall thickness is 25mm, and the length is 2775 mm; groove cutting of the cylinder: processing a welding groove by gas cutting; barrel winding drum: adopting a plate bending machine to process a winding drum; assembling and welding longitudinal seams of the cylinder; rounding the cylinder: the roundness error of the cylinder is less than 2 mm; assembling and welding a circular seam of the cylinder body, and carrying out nondestructive detection on the cylinder body: performing 100% ultrasonic detection and 100% magnetic powder detection, wherein the qualified grade is I grade, and a cylinder is provided with a hole;
s2: processing a gas collecting ring assembly, wherein a gas collecting pipe forms a bent pipe by adopting intermediate frequency heating: the gas collecting pipe adopts phi 860X30 material 16 Mn; the bent pipe is assembled and welded to form a gas collecting ring: 4, forming a phi 4060 gas collecting ring by the bent pipe section; carrying out nondestructive testing on welding of the gas collecting ring and opening the gas collecting ring: the gas collecting ring is used for gas cutting to form holes, so that the cutting precision is ensured; the gas collecting ring is welded with a gas inlet connecting pipe and a gas outlet connecting pipe;
s3: processing the spray pipe, namely taking a spray pipe raw material forging: normalizing the 16MnII forge piece; rough milling: reserving 5mm of allowance for raw materials; stress relief heat treatment; fine milling; drilling holes in the spray pipe; processing and checking: the feeler gauge is qualified when the feeler gauge does not exceed 0.5 mm.
S4: assembling the spray pipe and processing a connecting piece; the connecting piece and the spray pipe are assembled through a tool, and the tool is connected with the connecting piece through a bolt, so that the precision requirement is ensured; the connecting piece is welded with the cylinder; the connecting piece is welded with the spray pipe; thermal treatment of the spray pipe and the connecting piece: and (4) reserving in the heat treatment process, and dismantling the tool after the heat treatment is finished.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention is not limited thereby, so: all equivalent changes made according to the structure, shape and principle of the invention are covered by the protection scope of the invention. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.

Claims (3)

1. The manufacturing method of the injection module of the large-scale exhaust system comprises a cylinder body (1), a gas collecting ring assembly and a spray pipe (2), wherein the gas collecting ring assembly comprises a gas collecting ring (3), a gas inlet connecting pipe (4) and a gas outlet connecting pipe (5), and is characterized in that the spray pipe is assembled with a connecting piece (6), and the manufacturing method comprises the following steps:
s1: processing a barrel, namely taking a barrel raw material for blanking, cutting a groove on the barrel, assembling and welding a barrel winding drum, assembling and welding a longitudinal seam on the barrel, assembling and welding a circular seam on the barrel, carrying out nondestructive detection on the barrel, and perforating the barrel;
s2: processing a gas collecting ring assembly, wherein a gas collecting pipe adopts intermediate frequency heating to form a bent pipe, the bent pipe is assembled and welded to form a gas collecting ring, the gas collecting ring is welded and subjected to nondestructive testing, the gas collecting ring is perforated, and the gas collecting ring is welded with a gas inlet connecting pipe and a gas outlet connecting pipe;
s3: processing a spray pipe, namely taking a spray pipe raw material forge piece, roughly milling, performing stress relief heat treatment, finely milling and drilling the spray pipe;
s4: and (3) assembling the spray pipe, processing the connecting piece, assembling the connecting piece and the spray pipe, welding the connecting piece and the barrel, and carrying out heat treatment on the spray pipe and the connecting piece.
2. The manufacturing method of the injection module of the large exhaust system according to claim 1, wherein in the step S1, the cylinder is rounded after the longitudinal seam of the cylinder is welded.
3. The manufacturing method of the ejector module of the large exhaust system according to claim 1, wherein in step S1, the welding nondestructive testing of the gas collecting ring adopts 100% ray detection and 100% magnetic powder detection.
CN202011464732.8A 2020-12-14 2020-12-14 Manufacturing method of injection module of large exhaust system Withdrawn CN112719788A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011464732.8A CN112719788A (en) 2020-12-14 2020-12-14 Manufacturing method of injection module of large exhaust system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011464732.8A CN112719788A (en) 2020-12-14 2020-12-14 Manufacturing method of injection module of large exhaust system

Publications (1)

Publication Number Publication Date
CN112719788A true CN112719788A (en) 2021-04-30

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CN202011464732.8A Withdrawn CN112719788A (en) 2020-12-14 2020-12-14 Manufacturing method of injection module of large exhaust system

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CN (1) CN112719788A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1296798A1 (en) * 2000-07-06 2003-04-02 Trico Products Company Method and apparatus for flexible manufacturing a discrete curved product from feed stock
CN204495535U (en) * 2015-03-20 2015-07-22 中国航天空气动力技术研究院 1.2 meters of magnitude wind-tunnel represent dynamically injectors
CN107235433A (en) * 2017-05-09 2017-10-10 大连交通大学 Power shovel lifts wire rope drum and its procedure of processing
CN107470821A (en) * 2017-07-25 2017-12-15 武汉冶钢结构有限责任公司 Assembling fixture and its installation Nozzle methods for wind tunnel ejector
CN110743406A (en) * 2019-10-30 2020-02-04 西安交通大学 Method for manufacturing ejector by using circular straight pipe
CN110849574A (en) * 2019-12-20 2020-02-28 沈阳航天新光压力容器有限公司 Large-scale exhaust system injection device
CN111779591A (en) * 2020-07-13 2020-10-16 中国航空发动机研究院 Sectional type exhaust apparatus

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1296798A1 (en) * 2000-07-06 2003-04-02 Trico Products Company Method and apparatus for flexible manufacturing a discrete curved product from feed stock
CN204495535U (en) * 2015-03-20 2015-07-22 中国航天空气动力技术研究院 1.2 meters of magnitude wind-tunnel represent dynamically injectors
CN107235433A (en) * 2017-05-09 2017-10-10 大连交通大学 Power shovel lifts wire rope drum and its procedure of processing
CN107470821A (en) * 2017-07-25 2017-12-15 武汉冶钢结构有限责任公司 Assembling fixture and its installation Nozzle methods for wind tunnel ejector
CN110743406A (en) * 2019-10-30 2020-02-04 西安交通大学 Method for manufacturing ejector by using circular straight pipe
CN110849574A (en) * 2019-12-20 2020-02-28 沈阳航天新光压力容器有限公司 Large-scale exhaust system injection device
CN111779591A (en) * 2020-07-13 2020-10-16 中国航空发动机研究院 Sectional type exhaust apparatus

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Application publication date: 20210430

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