CN111375860B - Method for brazing radiating tube and middle partition plate of tube type radiator - Google Patents

Method for brazing radiating tube and middle partition plate of tube type radiator Download PDF

Info

Publication number
CN111375860B
CN111375860B CN202010381714.7A CN202010381714A CN111375860B CN 111375860 B CN111375860 B CN 111375860B CN 202010381714 A CN202010381714 A CN 202010381714A CN 111375860 B CN111375860 B CN 111375860B
Authority
CN
China
Prior art keywords
brazing
filler metal
middle partition
partition plate
micro
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.)
Active
Application number
CN202010381714.7A
Other languages
Chinese (zh)
Other versions
CN111375860A (en
Inventor
吴长洪
卓著
龙本滔
张邦
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.)
Guizhou Yonghong Aviation Machinery Co Ltd
Original Assignee
Guizhou Yonghong Aviation Machinery 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 Guizhou Yonghong Aviation Machinery Co Ltd filed Critical Guizhou Yonghong Aviation Machinery Co Ltd
Priority to CN202010381714.7A priority Critical patent/CN111375860B/en
Publication of CN111375860A publication Critical patent/CN111375860A/en
Application granted granted Critical
Publication of CN111375860B publication Critical patent/CN111375860B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/20Preliminary treatment of work or areas to be soldered, e.g. in respect of a galvanic coating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/0008Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/008Soldering within a furnace

Abstract

The invention discloses a method for brazing a radiating pipe and a middle clapboard of a tubular radiator, which comprises the following steps: step 1: laying a plurality of layers of BNi82CrSiB amorphous brazing filler metal with the thickness of 0.03mm on the surface of the stainless steel plate, and micro-melting the brazing filler metal in a vacuum brazing furnace by adopting brazing parameters of 980 ℃ and 5min of heat preservation; step 2: punching the composite board formed by micro-melting brazing to form a middle partition board, and ensuring that the aperture of the middle partition board is larger than the outer diameter of the heat dissipation pipe, namely the brazing gap is in the range of 0.04mm-0.08 mm; and step 3: fitting the radiating pipe into the hole of the middle partition plate; and 4, step 4: the assembly was placed in a vacuum brazing furnace and re-brazed at 1070 c for 10 min. The invention solves the problem that the paste brazing filler metal is difficult to coat after a plurality of radiating pipes and partition plates are assembled.

Description

Method for brazing radiating tube and middle partition plate of tube type radiator
Technical Field
The invention relates to the technical field of stainless steel brazing, in particular to a remelting brazing method for a partition plate and a radiating pipe in a tube array radiator.
Background
The stainless steel tube type radiator is internally provided with a fuel oil cavity, the outside of the stainless steel tube type radiator is provided with an oil lubricating cavity, and the oil lubricating cavity is divided into oil lubricating channels by a plurality of middle partition plates to radiate the radiating tube. Generally, the middle partition plate and the radiating pipe are only in an assembly state, and the lubricant can flow through the assembly gap between the middle partition plate and the radiating pipe, so that the radiating efficiency of the radiating pipe is reduced. In order to improve the lubricating oil-burning heat dissipation efficiency of the tube nest radiator, if the paste-shaped brazing filler metal is coated on the middle partition plate for brazing, the brazing filler metal can be stacked and cover the surfaces of the radiating tubes at the non-brazed parts to influence the quality of products because the radiating tubes are arranged too tightly and the coating operation difficulty is high.
Disclosure of Invention
In order to solve the above problems, the present invention provides a remelting brazing method for a partition plate and a heat dissipation pipe in a tubular radiator, so as to solve the problem that the partition plate and the heat dissipation pipe are difficult to assemble when brazing.
The invention is realized by the following technical scheme:
a method for brazing a radiating pipe and a middle clapboard of a tube type radiator comprises the following steps,
step 1: degreasing and pickling the surface of the stainless steel plate, degreasing the surface of the brazing filler metal foil strip, assembling the stainless steel plate and the brazing filler metal foil strip after the stainless steel plate is dried, and then carrying out micro-melting brazing on the stainless steel plate and the brazing filler metal foil strip;
step 2: processing the composite board formed by the micro-melting brazing in the step 1 by using a punching machine to form a middle partition board, and removing oil stains and impurities on the surface of the middle partition board by using ultrasonic cleaning equipment;
and step 3: assembling the radiating pipe into the hole of the middle partition plate in the step 2, and fixing the relative position of the middle partition plate and the radiating pipe by using a tool;
and 4, step 4: and (3) placing the assembly in the step (3) in a vacuum brazing furnace, monitoring the temperature of the assembly by using a thermocouple, and then carrying out remelting brazing.
Preferably, the brazing filler metal foil strip is BNi82CrSiB amorphous brazing filler metal, and the thickness of the brazing filler metal foil strip is 0.03 mm.
Preferably, the brazing filler metal foil strip is single-layer or multi-layer.
Preferably, in the step 1, the temperature rise uniform speed before micro-melting brazing is 10 ℃/min, the micro-melting brazing temperature is 980 ℃, and the heat preservation time is 5 min.
Preferably, in the step 2, the composite plate formed by the micro-fusion brazing has a machining hole diameter larger than the outer diameter of the heat dissipation tube.
Furthermore, the difference between the processing aperture of the composite plate and the outer diameter of the heat dissipation pipe forms a brazing gap, and the brazing gap is controlled within the range of 0.04mm-0.08 mm.
Further, in the step 2, hole machining is performed from one side of the brazing filler metal of the composite plate, and the brazing filler metal at the edge of the hole is well covered by milling with a hard alloy milling cutter, so that subsequent brazing is facilitated.
Preferably, in the step 4, during the remelting brazing, the temperature rise uniform speed before the remelting brazing is 10 ℃/min, the remelting brazing temperature is 1070 ℃, and the heat preservation time is 10 min.
Compared with the prior art, the brazing filler metal and the middle partition plate form the composite plate by micro-fusion welding of the middle partition plate and the BNi82CrSiB amorphous brazing filler metal, and the composite plate is mechanically processed and then subjected to secondary remelting brazing. By the brazing method, the problems of brazing accumulation, non-brazing and difficult assembly are effectively avoided, the brazing quality of the product is ensured, and the heat dissipation efficiency of the product is improved.
Drawings
FIG. 1 is an assembly view of a brazing filler metal and stainless steel center spacer for micro-brazing;
FIG. 2 is a front view of FIG. 1;
FIG. 3 is a view of a spacer machining;
FIG. 4 is an assembly view of the heat pipe and the middle partition plate;
FIG. 5 is a front sectional view of FIG. 4;
in the figure: 1-BNi82CrSiB amorphous brazing filler metal, 2-middle partition plates, 3-brazing parts and 4-radiating pipes.
Detailed Description
The invention will be further described with reference to the following drawings and specific examples:
a remelting and brazing method for a clapboard and a radiating pipe in a tubular radiator comprises the following steps:
step 1: degreasing and pickling the surface of a stainless steel plate, degreasing the surface of a BNi82CrSiB amorphous brazing filler metal 1 (foil strip) with the thickness of 0.03mm, drying the stainless steel plate, assembling the stainless steel plate with a brazing filler metal foil strip according to a graph 1 and a graph 2 (namely paving the brazing filler metal foil strip on the surface of the stainless steel plate), and then carrying out micro-fusion brazing on the brazing filler metal, wherein the temperature rise and average speed is 10 ℃/min before the micro-fusion brazing, the micro-fusion brazing temperature is 980 ℃, and the heat preservation time is 5 min;
step 2: according to the figure 3, the composite board formed by micro-melting brazing is processed by a punching machine to form the middle partition board 2, the hole tolerance is to ensure that the brazing gap is within the range of 0.04mm-0.08mm (namely the difference value between the processing aperture of the composite board and the outer diameter of the radiating pipe), a hard alloy milling cutter is adopted to mill the brazing filler metal side during hole processing, and after the processing, surface oil stains and impurities are removed by ultrasonic cleaning equipment;
and step 3: assembling the radiating pipe 4 into the hole of the middle partition plate 2 according to fig. 4 and 5, and fixing the relative positions of the middle partition plate 2 and the radiating pipe 4 by using a tool, wherein the brazing part 3 is shown as a standard in fig. 5;
and 4, step 4: and (3) placing the assembly part in a vacuum brazing furnace, monitoring the temperature of the assembly part by using a thermocouple, carrying out remelting and brazing, wherein the temperature rise uniform speed is 10 ℃/min before remelting and brazing, the remelting and brazing temperature is 1070 ℃, and the heat preservation time is 10 min.

Claims (5)

1. A method for brazing a radiating pipe and a middle clapboard of a tube type radiator is characterized by comprising the following steps: comprises the following steps of (a) carrying out,
step 1: the method comprises the following steps of (1) removing oil and acid on the surface of a stainless steel plate, removing oil on the surface of a brazing filler metal foil strip, assembling the stainless steel plate and the brazing filler metal foil strip after the stainless steel plate is dried, and then carrying out micro-fusion brazing on the stainless steel plate and the brazing filler metal foil strip, wherein the brazing filler metal foil strip is BNi82CrSiB amorphous brazing filler metal and is 0.03mm in thickness, the temperature rise and average speed before the micro-fusion brazing is 10 ℃/min, the micro-fusion brazing temperature is 980 ℃, and the heat preservation time is 5 min;
step 2: processing the composite board formed by the micro-melting brazing in the step 1 by using a punching machine to form a middle partition board, and removing oil stains and impurities on the surface of the middle partition board by using ultrasonic cleaning equipment;
and step 3: assembling the radiating pipe into the hole of the middle partition plate in the step 2, and fixing the relative position of the middle partition plate and the radiating pipe by using a tool;
and 4, step 4: and (3) placing the assembly in the step (3) in a vacuum brazing furnace, monitoring the temperature of the assembly by using a thermocouple, and then carrying out remelting and brazing, wherein during remelting and brazing, the temperature rise uniform speed is 10 ℃/min before remelting and brazing, the remelting and brazing temperature is 1070 ℃, and the heat preservation time is 10 min.
2. The method of claim 1, wherein the step of brazing the tube of the tubulation radiator to the middle partition plate comprises: the brazing filler metal foil strip is single-layer or multi-layer.
3. The method of claim 1, wherein the step of brazing the tube of the tubulation radiator to the middle partition plate comprises: in the step 2, the processing aperture of the composite plate formed by micro-melting brazing is larger than the outer diameter of the heat dissipation pipe.
4. The method of claim 3, wherein the step of brazing the tube of the tubulation radiator to the middle partition plate comprises: the difference between the processing aperture of the composite plate and the outer diameter of the heat dissipation pipe forms a brazing gap, and the brazing gap is controlled within the range of 0.04mm-0.08 mm.
5. The method of claim 1, wherein the step of brazing the tube of the tubulation radiator to the middle partition plate comprises: in the step 2, hole machining is performed from one side of the brazing filler metal of the composite plate, and the brazing filler metal is milled by a hard alloy milling cutter.
CN202010381714.7A 2020-05-08 2020-05-08 Method for brazing radiating tube and middle partition plate of tube type radiator Active CN111375860B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010381714.7A CN111375860B (en) 2020-05-08 2020-05-08 Method for brazing radiating tube and middle partition plate of tube type radiator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010381714.7A CN111375860B (en) 2020-05-08 2020-05-08 Method for brazing radiating tube and middle partition plate of tube type radiator

Publications (2)

Publication Number Publication Date
CN111375860A CN111375860A (en) 2020-07-07
CN111375860B true CN111375860B (en) 2021-10-01

Family

ID=71215986

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010381714.7A Active CN111375860B (en) 2020-05-08 2020-05-08 Method for brazing radiating tube and middle partition plate of tube type radiator

Country Status (1)

Country Link
CN (1) CN111375860B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112620851B (en) * 2020-12-24 2022-12-13 湘潭大学 Method for connecting graphite and stainless steel through composite gradient interlayer high-temperature brazing
CN113290297B (en) * 2021-05-27 2023-04-07 贵州永红航空机械有限责任公司 Brazing filler metal assembling method for brazing high-temperature alloy honeycomb silencer
CN113478041A (en) * 2021-07-15 2021-10-08 贵州航天电子科技有限公司 Vacuum brazing processing method of waveguide antenna
CN114850710B (en) * 2022-05-25 2023-05-05 贵州永红航空机械有限责任公司 Brazing method of large-sized tube-in-tube radiator core assembly

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB820153A (en) * 1956-06-12 1959-09-16 Lawrence Holdings Overseas Ltd Improvements in the manufacture of heat exchangers
US3985283A (en) * 1974-08-01 1976-10-12 United Aircraft Products, Inc. Method of joining braze alloy to a parent metal part
CN102554509A (en) * 2012-02-24 2012-07-11 山东大学 Vacuum brazing solder and process of Mo-Cu alloy and stainless steel
CN106271488A (en) * 2016-08-31 2017-01-04 贵州永红航空机械有限责任公司 A kind of processing method of titanium alloy shell and tube combustion oil cooler
CN106363266A (en) * 2016-11-22 2017-02-01 中国航空工业集团公司北京航空材料研究院 Method for braze-welding core body of tube type radiator by adopting strip-shaped brazing filler metal
CN109570756A (en) * 2018-12-26 2019-04-05 江苏省宜兴电子器件总厂有限公司 A kind of thin type solder sheet and metalwork pre-fix method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB820153A (en) * 1956-06-12 1959-09-16 Lawrence Holdings Overseas Ltd Improvements in the manufacture of heat exchangers
US3985283A (en) * 1974-08-01 1976-10-12 United Aircraft Products, Inc. Method of joining braze alloy to a parent metal part
CN102554509A (en) * 2012-02-24 2012-07-11 山东大学 Vacuum brazing solder and process of Mo-Cu alloy and stainless steel
CN106271488A (en) * 2016-08-31 2017-01-04 贵州永红航空机械有限责任公司 A kind of processing method of titanium alloy shell and tube combustion oil cooler
CN106363266A (en) * 2016-11-22 2017-02-01 中国航空工业集团公司北京航空材料研究院 Method for braze-welding core body of tube type radiator by adopting strip-shaped brazing filler metal
CN109570756A (en) * 2018-12-26 2019-04-05 江苏省宜兴电子器件总厂有限公司 A kind of thin type solder sheet and metalwork pre-fix method

Also Published As

Publication number Publication date
CN111375860A (en) 2020-07-07

Similar Documents

Publication Publication Date Title
CN111375860B (en) Method for brazing radiating tube and middle partition plate of tube type radiator
CN109332837B (en) Vacuum brazing method for structure with thin-wall part
EP1215005B1 (en) Electrochemical machining process for forming surface roughness elements on a gas turbine shroud
US10081082B2 (en) Leading edge sheath manufacturing method
KR101166534B1 (en) Manufacturing thereof for oil cooler of automatic transmission
US11007592B2 (en) Heat exchanger and method for producing same
CN103801917A (en) Production technology process for automobile heat dissipation device
CS268671B2 (en) Method of two structural parts heat sealing
CN102039520B (en) Manufacturing method of aluminium alloy heat exchanger for gas water heater
CN108941837B (en) Base for brazing aluminum alloy cold plate
US20090173485A1 (en) Fin tube assembly for air cooled heat exchanger and method of manufacturing the same
CN104204711A (en) Sacrificial aluminum fins for failure mode protection of an aluminum heat exchanger
US20160054072A1 (en) A heat exchanger with a dual-function dispensing head connection assembly
CN105051481A (en) Method for manufacturing heat exchange, and heat exchanger
CN114008399A (en) Multi-material heat transfer device and method of manufacture
US10888910B2 (en) Machining method for burred flat holes in metal plates
KR100872587B1 (en) Manufacturing thereof for oil cooler of automatic transmission
CN107294237B (en) MULTILAYER COMPOSITE tubular dot matrix conductor rotor structure and its processing method
CN110072300B (en) Aluminum heating ring and manufacturing method thereof
CN110739195B (en) Cathode and focusing electrode coaxiality adjusting device, system and method of electron gun
CN201653227U (en) Anticorrosion light high-efficient finned type heat exchanger
JP6624585B2 (en) Sputtering target-backing plate assembly
KR102318527B1 (en) Manufacturing method of cooling block and coolant flow plate for cooling block applied to radiator
CN202204359U (en) Heat exchange fin structure of combustion gas water heater
US20220371093A1 (en) Method of manufacturing additively manufactured object

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant