JPS6320159A - Joining method for metallic member - Google Patents
Joining method for metallic memberInfo
- Publication number
- JPS6320159A JPS6320159A JP16458286A JP16458286A JPS6320159A JP S6320159 A JPS6320159 A JP S6320159A JP 16458286 A JP16458286 A JP 16458286A JP 16458286 A JP16458286 A JP 16458286A JP S6320159 A JPS6320159 A JP S6320159A
- Authority
- JP
- Japan
- Prior art keywords
- junction
- pin
- brazing
- joint
- joining
- 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
Links
- 238000000034 method Methods 0.000 title claims description 5
- 238000005219 brazing Methods 0.000 claims abstract description 18
- 238000009792 diffusion process Methods 0.000 claims description 14
- 229910052751 metal Inorganic materials 0.000 claims description 14
- 239000002184 metal Substances 0.000 claims description 14
- 239000000463 material Substances 0.000 abstract description 11
- 239000007791 liquid phase Substances 0.000 abstract description 8
- 239000007790 solid phase Substances 0.000 abstract description 4
- 238000003466 welding Methods 0.000 abstract description 3
- 239000000126 substance Substances 0.000 abstract description 2
- 239000011888 foil Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- -1 brazing Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000005300 metallic glass Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Landscapes
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明はろう付、液相拡散接合、固相拡散接合等による
金属部材の面接合(界面接合)に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to surface bonding (interfacial bonding) of metal members by brazing, liquid phase diffusion bonding, solid phase diffusion bonding, etc.
金属材料やセラミックスの面接合では、一般にろう付、
液□相拡散接合、固相拡散接合が適用されるが、接合対
の位置ぎめや間げきコントロールには治具や溶接による
仮付けが行われている。For surface joining of metal materials and ceramics, brazing,
Liquid phase diffusion bonding and solid phase diffusion bonding are applied, but temporary attachment using jigs and welding is used to position and control the gap between the bonded pairs.
前述の接合は一般に接合組立品の寸法精度上の要求が厳
しくいわゆる精密接合を要求される場合が多いが、接合
治具による位置ぎめでは、治具の熱ひずみや治具材と接
合部材の熱膨張係数の差等によシ、接合の加熱中に狂い
を生じることが多い。1だ、ろう付や液相拡散接合の場
合には接合面間の間げきを所要の範囲に実質的に一定に
保持することが必要であるが、従来の方法では困難とな
る場合が多い。The above-mentioned joining generally has strict requirements for the dimensional accuracy of the joined assembly, and so-called precision joining is often required, but positioning using a joining jig is difficult to avoid due to thermal distortion of the jig or heat between the jig material and the joining member. Due to differences in expansion coefficients, distortions often occur during heating of the bond. 1. In the case of brazing or liquid phase diffusion bonding, it is necessary to maintain the gap between the bonding surfaces substantially constant within a required range, but this is often difficult with conventional methods.
本発明は、ろう付け、拡散接合等による金属部材の面接
合に際して、金属部材の各接合面の対向する位置に縦孔
を複数穿設し、前記の対向する縦孔に共通のピンを挿着
することにより、接合面を対向固定し、接合することを
特徴とする金属部材の接合方法であり、また、ろう付け
、拡散接合等による金属部材の面接合に際して、金属部
材の各接合面の対向する位置に縦孔を複数穿設し、前記
の対向する縦孔に座金を通した共通のピンを挿着するこ
とにより、接合面間に座金を介在させて接合面の間げき
を一定に保持して接合面を対向固定し、接合することを
特徴とする金属部材の接合方法である。In the present invention, when joining metal members face-to-face by brazing, diffusion bonding, etc., a plurality of vertical holes are bored at opposing positions on each joining surface of the metal members, and a common pin is inserted into the opposing vertical holes. This is a joining method for metal members characterized by fixing and joining the joining surfaces facing each other, and also, when joining metal members face-to-face by brazing, diffusion bonding, etc., each joining surface of the metal members is By drilling multiple vertical holes at the positions where the joints are to be connected and inserting a common pin with a washer through the opposing vertical holes, the washer is inserted between the joint surfaces to maintain a constant gap between the joint surfaces. This is a method for joining metal members, characterized in that the joining surfaces are fixed facing each other and joined.
接合部材において接合対面に孔をあけ、これにピンを挿
入することにより、接合位置を固定することができる。The joining position can be fixed by making a hole on the joining surface of the joining member and inserting a pin into the hole.
ピンは接合後は部材の中にそのまま残るととKなる。If the pin remains in the member after joining, then K.
またピンに所要間げきに相当する厚さの座金全通し、接
合面間に介在させることにより、間げきを一定に保つこ
とができる。In addition, the gap can be kept constant by having the pin pass through a washer with a thickness corresponding to the required gap and interposing it between the joint surfaces.
上記のピン、座金の材質は接合部材と同系の材料が望ま
しい。The materials for the pins and washers mentioned above are preferably of the same type as the joining member.
上記により接合位置のずれ防止、接合間げきの一定保持
ができるとともに治具や溶接による点付けなどによらな
いで接合部材の仮組立てができる。As a result of the above, it is possible to prevent the joint position from shifting, to maintain a constant joint gap, and to temporarily assemble the joint members without using a jig or spotting by welding.
本発明の一実施例として、ガスタービンの静翼の液相拡
散接合を第1.2及び3図により説明する。As an embodiment of the present invention, liquid phase diffusion bonding of stator vanes of a gas turbine will be explained with reference to FIGS. 1.2 and 3.
第1図に示すようにガスタービンの静翼単体103枚の
バットレス(BUTTRIC88) 部の側面を接合
面2として第2図の如き静翼セグメントを製作した。こ
の場合、第5図に示すように接合面に縦孔5を明は第4
図に示すピン4を挿入するとともに接合面間にインサー
ト材料(厚さ50μm)を介在して接合を行った。As shown in FIG. 1, a stator blade segment as shown in FIG. 2 was manufactured using the side surface of the buttress (BUTTRIC88) of 103 single stator blades of a gas turbine as the joint surface 2. In this case, as shown in FIG.
The pin 4 shown in the figure was inserted, and an insert material (thickness: 50 μm) was interposed between the bonding surfaces to perform bonding.
静翼の材質はN1 基耐熱合金(N1−15%Or −
6%AI!−4%Mo −2%Wb −0,7%Ti)
であシ、これに対しピンの材質はN1 基耐熱合金(
Ni −22X Or −18,5%Fe −9X M
o −1,5X Co −0,6X W)とした。The material of the stationary blade is N1-based heat-resistant alloy (N1-15%Or-
6% AI! -4%Mo -2%Wb -0.7%Ti)
However, the material of the pin is N1-based heat-resistant alloy (
Ni -22X Or -18,5%Fe -9X M
o -1,5X Co -0,6X W).
孔の径#i5.05mとし、これに対してピンの径はS
、OWとした。インサート材料としてはN1−15%0
r−4%Bの非晶質金属箔を用いた。The diameter of the hole #i is 5.05m, and the diameter of the pin is S.
, OW. N1-15%0 as insert material
An amorphous metal foil of r-4% B was used.
接合は上記のピン挿入により固定し、かつインサート材
料を接合面間に挿入した仮組立品を真空中で1200C
,7時間加熱し接合した。The joint was fixed by inserting the pin as described above, and the temporary assembly with the insert material inserted between the joint surfaces was heated at 1200C in a vacuum.
, and bonded by heating for 7 hours.
本発明の他の実施例として、液体ロケットエンジン燃焼
室のろう付例を第5図と、そのA部拡大図の第6図によ
って説明する。As another embodiment of the present invention, an example of brazing a combustion chamber of a liquid rocket engine will be explained with reference to FIG. 5 and FIG. 6, which is an enlarged view of part A thereof.
第5図に示すような燃焼室5を、第6図に示すような冷
却溝7を有する無酸素銅製のセグメント6を積重ね各セ
グメント6間をろう付して燃焼室を組立る。A combustion chamber 5 as shown in FIG. 5 is assembled by stacking oxygen-free copper segments 6 having cooling grooves 7 as shown in FIG. 6 and brazing the segments 6 together.
この場合、第6図に示すように接合面に孔を明け、接合
間げきを一定に保持するために座金8を介してピン9を
挿入し、かつ接合面間にろう材の箔10を介してろう付
を行うた。ピン9の挿入箇所は、各セグメント6間の接
合面につき円周上3箇所とした。In this case, as shown in FIG. 6, a hole is made in the joint surface, a pin 9 is inserted through a washer 8 to maintain a constant joint gap, and a foil 10 of brazing material is inserted between the joint surfaces. I did some brazing. The pins 9 were inserted at three locations on the circumference of each joint surface between the segments 6.
ピン9の材質は5U8504ステンレメ鋼トシした。孔
の径は5.111に対し、ピンの径は5.0諺とした。The material of pin 9 was 5U8504 stainless steel. The diameter of the hole was 5.111, and the diameter of the pin was 5.0.
座金の材質は8U8504ステンレス鋼、寸法はφ15
.OXφ5.I X t O,05wmとした。The material of the washer is 8U8504 stainless steel, and the size is φ15.
.. OXφ5. IXtO, 05wm.
ろう材はBig −8(公称化学成分72%Ag−28
%au)の箔(厚さo、o811II)を用いた。ろう
付は、上記のようにピン、座金、ろう波箔を適用した仮
組立品を水素雰囲気中で800cに15分間加熱して行
った。The brazing filler metal is Big-8 (nominal chemical composition 72%Ag-28
%au) foil (thickness o, o811II) was used. Brazing was carried out by heating the temporary assembly to which the pin, washer, and wax wave foil were applied as described above at 800°C for 15 minutes in a hydrogen atmosphere.
上述したように本発明によれば、接合個所が多いろう付
け、液相拡散接合や固相拡散接合による精密接合組立が
可能となる。As described above, according to the present invention, precision bonding assembly using brazing, liquid phase diffusion bonding, or solid phase diffusion bonding with many bonding points becomes possible.
またろう付けや液相拡散接合に際しては接合面間けきを
一定に保持することにより、高品質、高強度の接合が得
られる。Furthermore, during brazing or liquid phase diffusion bonding, high quality and high strength bonding can be obtained by keeping the gap between the bonding surfaces constant.
4、面の簡単な説明
第1図は本発明の一実施例としてのガスタービン静翼単
体の概要図であり、第2図は第1図の静翼単体を拡散接
合した概要図である。第3図は接合面に穿設した孔、第
4図はピンを示す図である。第5図は他の実施例として
の液体ロケットエンジン燃焼室の概要図であり、第6図
は第5図^の拡大図である。4. Brief description of aspects FIG. 1 is a schematic diagram of a gas turbine stator vane unit as an embodiment of the present invention, and FIG. 2 is a schematic diagram of the stator vane unit of FIG. 1 bonded by diffusion bonding. FIG. 3 shows a hole drilled in the joint surface, and FIG. 4 shows a pin. FIG. 5 is a schematic view of a liquid rocket engine combustion chamber as another embodiment, and FIG. 6 is an enlarged view of FIG.
復代理人 内 1) 明 復代理人 萩 原 亮 − 復代理人 安 西 篤 夫 莞( 第3図 5図Among the sub-agents: 1) Akira Sub-agent Ryo Hagi Hara - Sub-agent Atsuo Annishi Guan ( Figure 3 Figure 5
Claims (2)
際して、金属部材の各接合面の対向する位置に縦孔を複
数穿設し、前記の対向する縦孔に共通のピンを挿着する
ことにより、接合面を対向固定し、接合することを特徴
とする金属部材の接合方法。(1) When joining metal members face-to-face by brazing, diffusion bonding, etc., a plurality of vertical holes are bored at opposing positions on each joint surface of the metal members, and a common pin is inserted into the opposing vertical holes. A method for joining metal members, characterized in that the joining surfaces are fixed facing each other and joined.
際して、金属部材の各接合面の対向する位置に縦孔を複
数穿設し、前記の対向する縦孔に座金を通した共通のピ
ンを挿着することにより、接合面間に座金を介在させて
接合面の間げきを一定に保持して接合面を対向固定し、
接合することを特徴とする金属部材の接合方法。(2) When joining metal members face-to-face by brazing, diffusion bonding, etc., a plurality of vertical holes are bored at opposing positions on each joint surface of the metal members, and a common pin is inserted with a washer through the opposing vertical holes. By inserting a washer between the joint surfaces, the gap between the joint surfaces is kept constant and the joint surfaces are fixed facing each other.
A method for joining metal members, characterized by joining.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP16458286A JPS6320159A (en) | 1986-07-15 | 1986-07-15 | Joining method for metallic member |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP16458286A JPS6320159A (en) | 1986-07-15 | 1986-07-15 | Joining method for metallic member |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6320159A true JPS6320159A (en) | 1988-01-27 |
Family
ID=15795908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP16458286A Pending JPS6320159A (en) | 1986-07-15 | 1986-07-15 | Joining method for metallic member |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6320159A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02136785A (en) * | 1988-11-17 | 1990-05-25 | Hitachi Ltd | Fuel assembly |
JP2015061977A (en) * | 2013-07-23 | 2015-04-02 | ゼネラル・エレクトリック・カンパニイ | Methods for modifying cooling holes with recess-shaped modifications, and components incorporating the same |
JP2015227152A (en) * | 2014-05-09 | 2015-12-17 | 株式会社シマノ | Component for bicycle, shaft member for bicycle, rear sprocket assembly for bicycle, and lever member for bicycle |
CN112108740A (en) * | 2020-09-21 | 2020-12-22 | 中国航发贵州黎阳航空动力有限公司 | Vacuum brazing method and clamp for dense gas film hole metal plate assembly |
-
1986
- 1986-07-15 JP JP16458286A patent/JPS6320159A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02136785A (en) * | 1988-11-17 | 1990-05-25 | Hitachi Ltd | Fuel assembly |
JP2015061977A (en) * | 2013-07-23 | 2015-04-02 | ゼネラル・エレクトリック・カンパニイ | Methods for modifying cooling holes with recess-shaped modifications, and components incorporating the same |
JP2015227152A (en) * | 2014-05-09 | 2015-12-17 | 株式会社シマノ | Component for bicycle, shaft member for bicycle, rear sprocket assembly for bicycle, and lever member for bicycle |
CN112108740A (en) * | 2020-09-21 | 2020-12-22 | 中国航发贵州黎阳航空动力有限公司 | Vacuum brazing method and clamp for dense gas film hole metal plate assembly |
CN112108740B (en) * | 2020-09-21 | 2022-01-21 | 中国航发贵州黎阳航空动力有限公司 | Vacuum brazing method and clamp for dense gas film hole metal plate assembly |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1760265B1 (en) | Turbine engine component with a cooling microcircuit and corresponding manufacturing method | |
US4492737A (en) | Composite metallic and non-metallic articles | |
US5732468A (en) | Method for bonding a turbine engine vane segment | |
US8375582B2 (en) | Method and apparatus for producing and/or repairing an integrally bladed rotor by inductive diffusion welding | |
JP2001323803A (en) | Stator vane, its handling method, and its detail for exchange | |
GB1583738A (en) | Method for fabricating composite bladed wheel assemblies | |
JP2008175204A (en) | Turbomachine rotor and method for manufacturing the same | |
US20190151974A1 (en) | Methods for joining materials, and material composite | |
JP4548705B2 (en) | Method for manufacturing stationary blade or moving blade component | |
IE913106A1 (en) | Apparatus and method for a stator assembly of a rotary machine | |
JPS6320159A (en) | Joining method for metallic member | |
US6131797A (en) | Method for joining ceramic to metal | |
EP0283308A1 (en) | Composite jointed bodies | |
EP2327501B1 (en) | Methods of joining a first component and a second component to form a bond joint | |
US20160326892A1 (en) | Ceramic covered turbine components | |
JPS6227380A (en) | Method of joining axis of ceramic structure to boss of metalstructure | |
JPH11114662A (en) | Joining method for casting material and manufacture of turbine blade | |
WO2021067081A1 (en) | Method of processing a joint to be brazed, a method of processing a brazed joint, and an actively brazed joint | |
JP3218800B2 (en) | How to assemble turbine vanes | |
RU2104130C1 (en) | Method for joining components of composite target from high-melting and difficultly deformable materials | |
JP2820655B2 (en) | Segment type honeycomb brazing method and honeycomb brazing jig | |
JP2508823B2 (en) | How to connect a ceramic rotor to a metal shaft | |
JPS62118004A (en) | Moving blade for steam turbine and manufacture thereof | |
EP3052763B1 (en) | A nonmetallic airfoil with a compliant attachment | |
JPS60234777A (en) | Manufacture of rotor for turbo molecular pump |