JPS6064656A - Screw blade of centrifugal separator - Google Patents
Screw blade of centrifugal separatorInfo
- Publication number
- JPS6064656A JPS6064656A JP16932783A JP16932783A JPS6064656A JP S6064656 A JPS6064656 A JP S6064656A JP 16932783 A JP16932783 A JP 16932783A JP 16932783 A JP16932783 A JP 16932783A JP S6064656 A JPS6064656 A JP S6064656A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- base metal
- screw blade
- fan
- shaped segments
- 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.)
- Granted
Links
- 239000010953 base metal Substances 0.000 claims abstract description 27
- 239000000835 fiber Substances 0.000 claims abstract description 21
- 239000000463 material Substances 0.000 claims abstract description 8
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 7
- 239000000956 alloy Substances 0.000 claims abstract description 7
- 239000000843 powder Substances 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 4
- 239000000155 melt Substances 0.000 claims description 3
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 abstract description 9
- 238000003466 welding Methods 0.000 abstract description 8
- ZDKMYVQDSMZLFG-UHFFFAOYSA-N [B].[Ni].[Cr] Chemical compound [B].[Ni].[Cr] ZDKMYVQDSMZLFG-UHFFFAOYSA-N 0.000 abstract description 7
- 239000004744 fabric Substances 0.000 abstract description 6
- 239000010935 stainless steel Substances 0.000 abstract description 6
- 229910001220 stainless steel Inorganic materials 0.000 abstract description 6
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 abstract description 4
- 229910052751 metal Inorganic materials 0.000 abstract description 4
- 239000002184 metal Substances 0.000 abstract description 4
- 239000011230 binding agent Substances 0.000 abstract description 2
- 235000011187 glycerol Nutrition 0.000 abstract description 2
- 229910000521 B alloy Inorganic materials 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 238000000465 moulding Methods 0.000 abstract 1
- 238000010304 firing Methods 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 239000010802 sludge Substances 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910001347 Stellite Inorganic materials 0.000 description 2
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 235000002597 Solanum melongena Nutrition 0.000 description 1
- 244000061458 Solanum melongena Species 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 210000004907 gland Anatomy 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B1/00—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles
- B04B1/20—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles discharging solid particles from the bowl by a conveying screw coaxial with the bowl axis and rotating relatively to the bowl
- B04B1/2008—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles discharging solid particles from the bowl by a conveying screw coaxial with the bowl axis and rotating relatively to the bowl with an abrasion-resistant conveyor or drum
Landscapes
- Centrifugal Separators (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
【発明の詳細な説明】 本発明は遠心分離機のスフリーラ羽根に関ずろ。[Detailed description of the invention] The present invention relates to a spriller blade for a centrifuge.
例えば、デカンタ型遠心分離機においては、＋１Ｉｌｌ
＋腺の周りに高速回転する回転円胴に対して、同軸的に
適宜の差速をもって高速回転するスクリュウ羽根を具え
、遠心効果により回転円胴内面に清って集められた汚泥
中の固形分をスクリュウ羽根により濃縮移動して回転円
胴の一端から外部に排出するようにしている。For example, in a decanter type centrifuge, +1Ill
+ A screw blade that rotates coaxially at high speed with an appropriate differential speed is attached to the rotating cylinder that rotates at high speed around the gland, and the solid content in the sludge is purified and collected on the inner surface of the rotating cylinder by the centrifugal effect. is concentrated and moved by a screw blade and discharged to the outside from one end of the rotating cylinder.
しかしながら、この１重のスクリュウ羽根は高速回転で
汚泥中の固形分と接触して運動する関係−に、７時にそ
の先端部には激しい摩耗を生ずる。However, since this single screw blade rotates at high speed and moves in contact with the solid content in the sludge, severe wear occurs at its tip at 7 o'clock.
そこで、従来は、その摩耗対策として（１）スフリーラ
羽根の先端部にステライト等の肉盛溶接を施しており、
また（２）予め焼成成型された耐摩耗性のタイルをボル
ト等により機械的に固着又は蝋付等で接着する等の対抗
手段も知ら」ｔている。Therefore, in the past, as a countermeasure against this wear, (1) overlay welding of stellite, etc. was applied to the tip of the free roller blade,
(2) Countermeasures are also known, such as mechanically fixing pre-fired and molded wear-resistant tiles with bolts or the like, or bonding them with brazing or the like.
しかしながら（１）では肉盛溶接のだイ）に多くの工数
を要し、しかも均一厚さが得られず、そのために局部的
に大きな摩擦力を受け、硬度もロックウェル硬度約６５
以下で必ずしも十分とはいえず、また（２）では蝋付す
る場合は接着強度不足で使用中剥離し事故を起こす惧７
）を力゛・あり、さらに後言己するようにスフリーラ羽
根はｒす（゛イ１な形状を有する関係−１−タイルの成
形上＋ｄよびコスト上の問題がある。However, in (1), a lot of man-hours are required for overlay welding, and a uniform thickness cannot be obtained, which results in localized large frictional forces, and the hardness is approximately 65 on the Rockwell hardness scale.
The following is not necessarily sufficient, and if (2) is used, there is a risk that it may peel off during use due to insufficient adhesive strength and cause an accident.
), and, as I will say later, the spriller blades have a unique shape.
本発明はこのような事情に鑑みて提案されたもので、高
ＩＩＩＩ摩耗性かつ低コストのデカンタノ（１１遠心分
離機のスクリュウ羽根を提供することを１−１的とする
。The present invention has been proposed in view of the above circumstances, and has an object of 1-1 to provide a screw blade for a decantano (11 centrifuge) that is highly abrasive and low in cost.
そのために本発明は、デカンタ型遠心分旨１機に寸ｄい
て、耐摩耗材の粉末又は繊絹体とこｉｔと４１．；れ（
ＩＩ″が良くベースメタルの融点以下で溶融する自溶性
合金の粉末体又は繊絹体とをｉ、Ｊｊ ＋１．’１．１
ベースメタル」二に密着焼結して超硬］※を形成すると
ともに該超硬層を上記ベースメタルに冶金学的結合をな
さしめた複数の扇型セグメントを羽根の外周に漬って連
続的に溶接したことを特徴とする。To this end, the present invention provides a decanter-type centrifugal device with a powder or fibrous body of wear-resistant material and 41. ;Re(
i, Jj +1.'1.1 is a self-fusing alloy powder or silk body that has a good II'' and melts below the melting point of the base metal.
A plurality of fan-shaped segments are continuously sintered on the outer periphery of the blade by closely sintering the base metal to form a carbide]* and metallurgically bonding the carbide layer to the base metal. It is characterized by being welded to.
Ａ〈発明θ片−実施例を図面について説明すると、第１
図はその部分縦断げ１１図、第２図は第１図θ月１−Ｉ
Ｉに沿った部分拡大断面図、第３図は第２図の部分拡大
斜視図、第４図は第３図のセグメントのＩＶ −ＩＶに
沿った断面図である。A〈Invention θ Piece〉Explaining the embodiment with reference to the drawings, the first
The figure is a longitudinal cross-section of that part, Figure 11, and Figure 2 is Figure 1.
FIG. 3 is a partially enlarged perspective view of FIG. 2, and FIG. 4 is a cross-sectional view of the segment of FIG. 3 along IV--IV.
上図において、１は回転円胴、２はステンレス鋼よりな
るスフリーラ羽根、３はスクリュウ羽根２の汚泥を押出
す側の面上に外周に治って連続的に溶接される本発明に
係る複数の耐摩耗性扇型セグメント、４はステンレス鋼
よりなる扇型ベースメタル、５は扇型セグメント４の外
側側面および端面（Ｃ渚って焼結形成さ」１．た■７字
状断面を有する超硬層、６は耐摩耗の材、例えばタング
ステンカーバイドの第１層、７は第１層６の−にに重ね
て作られる自溶性合金、例えばニッケルクロムボロンの
第２層で、６および７が焼結されて超硬層５を形成し、
４および５が一体と１．仁って扇型セグメント３を形成
する。８オ６よひ９ばそれぞれ扇型ベースメタル４をス
クリュウ羽根２に溶接する溶接部である。In the above figure, 1 is a rotary cylinder, 2 is a stainless steel spriller blade, and 3 is a plurality of screw blades according to the present invention that are continuously welded to the outer periphery on the sludge extrusion side surface of the screw blade 2. Wear-resistant fan-shaped segment, 4 is a fan-shaped base metal made of stainless steel, 5 is an outer side surface and an end surface of the fan-shaped segment 4 (formed by sintering). The hard layer 6 is a first layer of wear-resistant material, e.g. tungsten carbide, 7 is a second layer of a self-fusing alloy, e.g. nickel chromium boron, made over the first layer 6, 6 and 7 are sintered to form a cemented carbide layer 5;
4 and 5 together and 1. In this way, a fan-shaped segment 3 is formed. 8, 6, and 9 are welding parts where the fan-shaped base metal 4 is welded to the screw blade 2, respectively.
このような構造において、扇状セグメント３は下記の要
領で作ることができる。In such a structure, the fan-shaped segment 3 can be made in the following manner.
＋１ψ（質のタングステンカーバイドの短繊維を電ＩＬ
Ｉ（のタングステンフィラメントの製法と同様の製法で
作り、この短繊維をグリセリン等のバインダて処理して
フェルト状の繊維布とし、同１子の蟹領て自溶性合金例
えばニッケルクロノ、ボロン合金の金属繊維布を作る。+1ψ (Electric IL of high quality tungsten carbide short fibers
The short fibers are made using the same manufacturing method as the tungsten filament of I (I), and the short fibers are treated with a binder such as glycerin to make a felt-like fiber cloth. Make metal fiber cloth.
ベースメタル４はステンレス鋼板を機械加工して成形し
、この上に第１層６としてタングステンカーバイド繊維
布を所定の形状に切１θ１１〜だものを載せ、その上に
第２層７としてニッケルクロムボロン金属繊維布を所定
の形状に明断したものを載せ、ベースメタルに密ス６し
た状態で焼成炉にて１０３０〜１１００′η〕で加熱す
る。The base metal 4 is formed by machining a stainless steel plate, and on top of this, a tungsten carbide fiber cloth cut into a predetermined shape 1θ11 is placed as the first layer 6, and on top of this, a nickel chromium boron material is placed as the second layer 7. A metal fiber cloth cut into a predetermined shape is placed on the base metal and heated in a firing furnace at a temperature of 1030 to 1100'η.
そ５才ろと、自溶性合金ニッケルクロムボロンの第２層
７は溶融しタングステンカーバイドの第１層６の繊維間
に浸透してこれと拡散１＝ｊ・１を形成し、液相焼結が
進行し、自溶性合金７はベースメタル／ＩＫ達すると、
そこに冶金学的結合層を形成し、タングステンカーバイ
ド／ニッケルクロｊ、ボロンの超硬焼結層をベースメタ
ル４に融着せしめる。At around 5 years of age, the second layer 7 of the self-fusing alloy nickel chromium boron melts and penetrates between the fibers of the first layer 6 of tungsten carbide, forming a diffusion 1=j・1 with it, resulting in liquid phase sintering. progresses and when self-fusing alloy 7 reaches base metal/IK,
A metallurgical bonding layer is formed thereon, and a cemented carbide sintered layer of tungsten carbide/nickel carbon and boron is fused to the base metal 4.
こＳ、で、タングステンカーバイド繊維の厚さとニッケ
ルクロムボロンの繊維の厚さを変えることによる成分比
の変化と、形成後の超硬層の厚さを変えることにより所
定の形状と性状の扇型セグメント３をイ、［９ろことか
できる。In this S, by changing the component ratio by changing the thickness of the tungsten carbide fiber and the thickness of the nickel chromium boron fiber, and by changing the thickness of the cemented carbide layer after formation, a fan shape with a predetermined shape and properties can be obtained. Segment 3 can be written as ``a'' or ``9''.
こ〜で、超硬層５を焼成するに当って、ニッケルクロム
ボロン繊翔−を第１層としタングステンカーバイド繊維
を第２層としてもよく、また各層に繊維を使用する代わ
りにそれぞれの粉末を使用し、適宜の型枠でその周囲を
囲繞した状態で焼結するようにしてもよく、その際ニッ
ケルクロムボロン粉末を第１層にタングステンカーバイ
ド粉末を第２層として散布してもよく、また両粉末を混
合したものを散布してもよい。When firing the carbide layer 5, nickel chromium boron fibers may be used as the first layer and tungsten carbide fibers may be used as the second layer, or instead of using fibers in each layer, each powder may be used. The nickel chromium boron powder may be used as a first layer and the tungsten carbide powder may be sprinkled as a second layer. A mixture of both powders may be sprayed.
このようにして成型さ、）］、た複数の扇型セグメント
３をそれぞれその円弧状内端において溶接部８でスフリ
ーラ羽根２に溶接するととも（・入 スクリ・つ羽根２
の外周にて（容接部９てスクリュウ羽根２に溶接する。In this way, the plurality of fan-shaped segments 3 are welded to the freewheel blade 2 at the welding part 8 at their arcuate inner ends.
(Welded to the screw blade 2 at the welding part 9.
スクリ・−ウ羽根２はらせん面を有するとともに、その
夕１径が、第１図に示すように、軸方向にｉｌ″ｆっで
徐々に小さくなっているので、１、ｉ１！’Ｉ”、セグ
メント３は１個１個若干形状を異にしたべ、のが必要で
あるが、ベースメタル４はステンレス鋼板で作られてい
るので、その機械加工は比較的容易に行なうことができ
る。The screw blade 2 has a helical surface, and its diameter gradually decreases in the axial direction as shown in FIG. Although each segment 3 needs to have a slightly different shape, since the base metal 4 is made of a stainless steel plate, its machining can be performed relatively easily.
このようにして作られた扇型セグメント３のベースメタ
ル４はスフリーラ羽根２と同質の（」質で作られるので
、その溶接は強固なものとなり、ベースメタル／Ｉ１．
に焼成された超硬層３の硬度はロックウェル硬度で６８
程度どなるので、十分大きな耐摩耗性を発揮することが
てきる。Since the base metal 4 of the fan-shaped segment 3 made in this way is made of the same quality as the freewheel blade 2, the welding thereof is strong, and the base metal/I1.
The hardness of the carbide layer 3 fired is 68 on the Rockwell hardness scale.
Depending on the degree of wear resistance, sufficiently high wear resistance can be exhibited.
なす（（、ベースメタル４としては、スクリュウ羽根２
を形成するステンレス鋼と超硬層５との中間的性質を有
する材料を使用することもできろ。Eggplant ((, as base metal 4, screw blade 2
It is also possible to use a material having intermediate properties between the stainless steel forming the carbide layer 5 and the cemented carbide layer 5.
このような構造＋／ｒＣよれば、下記の効果が奏せられ
る。According to such a structure +/rC, the following effects can be achieved.
（１）超硬層は複！ｘＫＩ＝な形状のベースメタル上に
も焼成することができろ。(1) The carbide layer is complex! It should be possible to fire on a base metal with a shape of xKI=.
（２）超硬層ば、ベースメタル上で焼成されので、累月
として金属繊維を使用する場合は、焼成枠型が不要であ
る。(2) Since the carbide layer is fired on the base metal, a firing frame is not required when using metal fiber as the layer.
（３）ベースメタルと一体的に焼成するので、超硬層と
ベースメタル間の蝋イヌ１は不要である。(3) Since it is fired integrally with the base metal, the wax dog 1 between the carbide layer and the base metal is unnecessary.
（４）ステライト等による肉盛り溶接よりも高硬度で緻
密な組織が得られ、スラリ３−９羽根の耐用命数を著し
く伸ばすことができる。(4) A harder and denser structure can be obtained than build-up welding using stellite or the like, and the service life of the slurry 3-9 blade can be significantly extended.
蟹するに本発明によ１・１．ば、デカンタ型遠心分離機
において、酬摩粍材の粉末体又は繊維体とこれと濡れ性
が良くベースメタルの融点」ユ下で溶融刊−ろ自溶性合
金の粉末体又は繊維体とを扇型ベースメタル」二に密Ｍ
焼結して超硬層を形成するとともに該超硬層を上記べ一
フ、ノタル１／こ冶金学的結合をなさし１）た複数の１
：４’、：ｉ ｌ（’ｊセグノントを羽根の外周に泪っ
て連続的に溶灰したことにより、長寿命の遠心分前機の
スクリュウ羽根を得るから、本発明は産縮七極めて有益
なものである。According to the present invention, 1.1. For example, in a decanter-type centrifugal separator, powder or fibers of a swarm material and powders or fibers of a self-fusing alloy with good wettability and melting at a temperature below the melting point of the base metal are combined. Type base metal ``Ninimushi M
A plurality of 1) are sintered to form a carbide layer, and the carbide layer is metallurgically bonded to the base and 1).
:4', :i l('j By pouring segmentont onto the outer periphery of the blade and continuously dissolving the ash, a long-life screw blade for a centrifugal preparator is obtained, so the present invention is extremely useful for production reduction. It is something.
１１ツ］：ｉ’＋ｉの簡Ｉ１１′ｌな１脱明２４′口図
は本発明の一実施例を示す部分縦断面図、第２図は第１
図のＩＴ−ＩＩに清った１ｌｌｊ分慝ノ〈断面図、第３
図は第２図の部分拡大斜視図、第４図は２１１３図のセ
グメントの］＼ｊ〜■＼’ｌ／ｉＺ浴った断面図である
。11]: i'+i simple I11'l 1.24' Exit view is a partial vertical cross-sectional view showing one embodiment of the present invention, and Fig.
1llj section clear to IT-II in Figure 3
The figure is a partially enlarged perspective view of FIG. 2, and FIG. 4 is a cross-sectional view of the segment of FIG.
１・・・回転円胴、２・・−スクリュウ羽根、：３・・
１１４ ”ｌ’！セグメント、４ ベースメタル、５
・、［召映層、６ 第１層、７・・・第２層、８，０
・溶接部。1...Rotating cylinder, 2...-screw blade, :3...
114 "l'! segment, 4 base metal, 5
・、[Showing layer, 6 1st layer, 7...2nd layer, 8,0
·welded part.
代叩人 井埋士 塚 本 正 文
手続補正書
昭和９９年ｆ月／ρ日
特許庁長官 殿 ）
１、事件の表示
昭和５８年特 許 願第１６９３２７号３ 補正をする
者
１１件との関係用［ｉ人
住 所 東京都千代田区丸の内二丁目６番２号氏 名（
名称）二菱化工機株式会社
４、代理人
−勃→Substitute person Masashi Ibuji Tsukamoto Procedural amendment written by the Commissioner of the Japan Patent Office (February 1989/1989) 1. Indication of the case Patent Application No. 169327 of 1983 3 Relationship with the person making the amendment 11 cases Address: 2-6-2 Marunouchi, Chiyoda-ku, Tokyo Name (
Name) Nisubishi Kakoki Co., Ltd. 4, Agent - Eki →
Claims (1)
繊維体とこれと濡れ性が良くベースメタルの融点以下で
溶融する自溶性合金の粉末体又は繊維体とを扇型ベース
メタル」二に密着焼結して超硬層を形成するとともに該
超硬層を上記ベースメタルに冶金学的結合をなさしめた
複数の扇型セグメントを羽根の外周に清って連続的に溶
接したことを特徴とする遠心分離機のスフリーラ羽根。In a decanter-type centrifuge, a powder or fiber of a wear-resistant material and a powder or fiber of a self-fusing alloy that has good wettability and melts below the melting point of the base metal are closely sintered onto a fan-shaped base metal. A plurality of fan-shaped segments are bonded together to form a carbide layer and the carbide layer is metallurgically bonded to the base metal, and a plurality of fan-shaped segments are neatly and continuously welded to the outer periphery of the blade. Sfreera blades of a centrifuge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16932783A JPS6064656A (en) | 1983-09-16 | 1983-09-16 | Screw blade of centrifugal separator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16932783A JPS6064656A (en) | 1983-09-16 | 1983-09-16 | Screw blade of centrifugal separator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6064656A true JPS6064656A (en) | 1985-04-13 |
| JPS6150654B2 JPS6150654B2 (en) | 1986-11-05 |
Family
ID=15884488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16932783A Granted JPS6064656A (en) | 1983-09-16 | 1983-09-16 | Screw blade of centrifugal separator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6064656A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6229716A (en) * | 1985-07-30 | 1987-02-07 | Honda Motor Co Ltd | 2-cycle engine exhaust timing control device |
| JPS6259155U (en) * | 1985-09-13 | 1987-04-13 | ||
| EP0893188A3 (en) * | 1997-07-22 | 1999-08-18 | United Technologies Corporation | Process for joining metallic members together |
-
1983
- 1983-09-16 JP JP16932783A patent/JPS6064656A/en active Granted
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6229716A (en) * | 1985-07-30 | 1987-02-07 | Honda Motor Co Ltd | 2-cycle engine exhaust timing control device |
| JPS6259155U (en) * | 1985-09-13 | 1987-04-13 | ||
| EP0893188A3 (en) * | 1997-07-22 | 1999-08-18 | United Technologies Corporation | Process for joining metallic members together |
| EP1439022A3 (en) * | 1997-07-22 | 2004-08-04 | United Technologies Corporation | Process for joining metallic members together |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6150654B2 (en) | 1986-11-05 |
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