JPS6011222B2 - Heat exchanger and its manufacturing method - Google Patents

Heat exchanger and its manufacturing method

Info

Publication number
JPS6011222B2
JPS6011222B2 JP50046591A JP4659175A JPS6011222B2 JP S6011222 B2 JPS6011222 B2 JP S6011222B2 JP 50046591 A JP50046591 A JP 50046591A JP 4659175 A JP4659175 A JP 4659175A JP S6011222 B2 JPS6011222 B2 JP S6011222B2
Authority
JP
Japan
Prior art keywords
layer
intermediate layer
plated
heat exchanger
gold
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.)
Expired
Application number
JP50046591A
Other languages
Japanese (ja)
Other versions
JPS50140718A (en
Inventor
トウ−シエル オツト−
ブツテル カルル
ウイツテイヒ ウイリバルト
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.)
METSUSAASHUMITSUTO BERUKO BUROOMU GmbH
Original Assignee
METSUSAASHUMITSUTO BERUKO BUROOMU GmbH
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 METSUSAASHUMITSUTO BERUKO BUROOMU GmbH filed Critical METSUSAASHUMITSUTO BERUKO BUROOMU GmbH
Publication of JPS50140718A publication Critical patent/JPS50140718A/ja
Publication of JPS6011222B2 publication Critical patent/JPS6011222B2/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081Heat exchange elements made from metals or metal alloys
    • F28F21/082Heat exchange elements made from metals or metal alloys from steel or ferrous alloys
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Description

【発明の詳細な説明】 本発明は少なくとも一つの冷却液、即ち推進燃料成分が
貫流することのできる冷却管路を有する金属製の一体の
本体で構成され、殊に液体ロケット推進装置の再生冷却
型燃焼室として使用されうる燃交換器に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention consists of a one-piece metal body with cooling channels through which at least one coolant, i.e. a propellant component, can flow, in particular for regenerative cooling of liquid rocket propulsion systems. The present invention relates to a fuel exchanger that can be used as a type combustion chamber.

この冷却管路は本体にメッキされて壁の薄い中間層とこ
の中間層にメッキされて壁厚が比較的厚いニッケル又は
等価の金属、銅コバルト合金若しくはニッケルコバルト
合金から成る耐圧ジャケットとから成る外壁部とによっ
て被われている。ロケット製造で知られている燃交換器
の構造は一般に耐食性が比較的低い材料でできていて、
そのためにたとえば赤い発煙硝酸のような貯蔵に耐える
液体推進燃料の使用が不可能になる。
The cooling conduit consists of an intermediate layer plated on the main body and having a thin wall, and an outer wall plated on the intermediate layer and consisting of a pressure jacket made of nickel or an equivalent metal, a copper cobalt alloy, or a nickel cobalt alloy and having a relatively thick wall thickness. It is covered by the part. Refueling exchanger structures known from rocket construction are generally made of materials with relatively low corrosion resistance;
This precludes the use of storable liquid propellants, such as red fuming nitric acid.

しかし乍ら貯蔵に耐える液体推進燃料で駆動されるロケ
ット推進装置はその急速な使用準備性のために低温工学
上の推進燃料を供給されるので、本発明の基本課題は、
すべての公知の貯蔵に耐える液体ロケット推進燃料に対
して耐食性の優れた経済的な熱交換器にして、液体ロケ
ット推進装置の再生冷却型燃煙室として使用されうる熱
交換器を創造することにある。本発明の課題は本発明に
従って特許請求の範囲に記載した構成の熱交換器によっ
て解決される。
However, since a rocket propulsion system powered by storage-resistant liquid propellant is supplied with cryogenic propellant for its rapid readiness for use, the basic problem of the present invention is to
To create an economical heat exchanger with excellent corrosion resistance for all known storage-resistant liquid rocket propellants, and to create a heat exchanger that can be used as a regeneratively cooled smoke chamber in liquid rocket propulsion systems. be. The object of the invention is solved according to the invention by a heat exchanger having the construction described in the claims.

この熱交換器は次のような特徴を有する。即ち本体が耐
食性の特殊鋼から成り、中間層が耐食性の金或いは銅若
し〈は金合金で作られる。本発明の基本的課題の解決は
次の認識に基くものである。
This heat exchanger has the following features. That is, the main body is made of corrosion-resistant special steel, and the intermediate layer is made of corrosion-resistant gold, copper, or a gold alloy. The solution to the basic problem of the present invention is based on the following recognition.

即ち此の種の熱交換器では冷却管路の壁部のみが従来公
知の貯蔵に耐えるいかなる液体ロケット推進燃料の酸化
成分によっても腐食されないばかりではなく、すべての
通常の使用条件の下でも過熱という結果になる熱のせき
とめが起らず且つ中間層が本体にも耐圧ジャケットにも
付着して且つ自体高い機械的剛性を有して、熱交換器が
通常の使用条件の下で生じるすべての機械的及び或いは
熱的負荷に耐えるということである。本発明による熱交
換器の中間層は特に費用の関係から金で作るのが良い。
更に次に詳しく記載する理由から特に銅、若しくは金合
金、特に金一銅−合金で作られる。この発明の熱交換器
は次のようにして作られる。
This means that in heat exchangers of this kind, only the walls of the cooling channels are not only not corroded by the oxidizing components of any liquid rocket propellant that is capable of being stored in the known manner, but also that they do not overheat under all normal conditions of use. All machines in which heat exchangers occur under normal conditions of use, with no resulting heat damming and with the intermediate layer adhering to both the body and the pressure jacket and having high mechanical rigidity themselves. This means that it can withstand physical and/or thermal loads. The intermediate layer of the heat exchanger according to the invention is preferably made of gold, especially for reasons of cost.
Furthermore, for reasons detailed below, it is especially made of copper or a gold alloy, especially a gold-copper alloy. The heat exchanger of this invention is manufactured as follows.

即ち先づ自体公知の態様で本体をたとえば耐食性特殊鋼
たとえばニモニック合金(Njmonlc75)〔Ni
cr2町i,抗張力38k9/肋2 〕から成るブロッ
クから鍛造し且つ冷却管路を切削によってつくり、次い
で冷却管路に導電性で溶融が容易な、特にワックスベー
スの材料を満たし、その上に薄壁の中間層を、そしてこ
の中間層の上に壁の厚い耐圧ジャケットをメッキして、
最後に冷却管路を満たしている熔融が容易な材料が溶解
する。容易に溶融する導補性充填物質を冷却管路に入れ
るには、本体を特にワックスベースによる充填物質の使
用時に充填物質の軟化温度に予熱するのが好都合である
ことが実証される。冷却管路への充填は次のようにする
のが好都合である。
That is, the body is first made of a corrosion-resistant special steel, such as Nimonic alloy (Njmonlc75), in a manner known per se.
cr2 town i, tensile strength 38k9/rib 2], and the cooling channels are made by cutting, then the cooling channels are filled with a conductive and easily meltable material, especially wax-based material, and a thin Plating the middle layer of the wall and the thick pressure jacket of the wall on top of this middle layer,
Finally, the easily meltable material filling the cooling channels melts. In order to introduce readily meltable, conductive filling materials into the cooling channels, it has proven advantageous to preheat the body to the softening temperature of the filling material, especially when using wax-based filling materials. The cooling channels are conveniently filled as follows.

即ち充填物質の軟化温度に予熱された本体の冷却管路へ
対応して変形されて且つ寸法が定められた紐状の充填物
質を装入して、銀或いは銀〆ッキされたはんだごてによ
って溶融する。特に本発明の方法の場合にはワックスベ
ースの充填物質及び、特に15〜25%の半コロイド状
の石墨粉末の添加によって導電性にされて容易に溶融す
るワックスが機能を発揮した。過剰量の充填物質は中間
層のメッキの前にはぎとりとそれに続く緑式研磨によっ
て除くのが好都合である。
In other words, a soldering iron that is silver or silver-plated is charged with a string-like filling material that has been deformed and sized accordingly into the cooling pipe of the main body that has been preheated to the softening temperature of the filling material. melted by Particularly in the case of the process according to the invention, wax-based fillers and readily meltable waxes made electrically conductive by the addition of 15 to 25% of semi-colloidal graphite powder were particularly effective. Advantageously, excess filler material is removed by stripping and subsequent green polishing before plating the intermediate layer.

中間層と耐圧ジャケットのメッキはその都度対象となる
金属の電離の公知の任意の態様で行なうことができる。
The plating of the intermediate layer and the pressure jacket can be carried out in any case in any known manner for ionizing the metal concerned.

既に述べたように、金の中間層は、金が本発明の目的の
ために対象となる貴金属のうち廉価であるから特に優先
される。電離された金の中間層の附着は本体材料として
の特殊鋼にも、耐圧ジャケットにも申し分なく行なわれ
る。メッキされた金中間層の機械的剛性も、中間層が1
5ぴC以上、特にほゞ20000以上の温度に加熱され
ない限りすべての要求を満足する。
As already mentioned, a gold interlayer is particularly preferred since gold is the least expensive of the noble metals of interest for the purposes of the present invention. The application of the ionized gold intermediate layer is satisfactory both to the special steel as the body material and to the pressure jacket. The mechanical rigidity of the plated gold intermediate layer is also 1.
It satisfies all requirements as long as it is not heated to a temperature of more than 5 picoC, especially more than approximately 20,000 degrees centigrade.

メッキされた金中間層の温度が予定の限界値を遥かにこ
えてそして或いはより長時間の間に、構造変化によるも
のと思われる引張り強度急速な低下が生ずるこのことは
無論一定の使用条件の場合にのみ妨げになる、本発明の
熱交換器のこの欠陥は本発明の有利な実施態様に従って
次のようにして除くことができる。即ち純粋な貴金属中
間層、特に金中間層の代りもこ少くとも二つの相から成
る中間層をメッキするのである。その場合初めの層、即
ち本体上に直接着いている層は耐食性の金から成り、次
の層則ち特に薄い層は銅から成るか或いはメッキ技術上
及び冶金特性に関して銅に類似、金合金則ち前記の第一
の層の上に層付可能で且つ比較的低い温度でより大きい
耐熱性の合金を形成して前記の第一の層に拡散可能の金
属から成る。そのような二つの層或いはそれ以上の複数
層の中間層をほゞ150qo、特にほゞ200oo以上
に加熱する場合には、合金金属がその下或いはその上に
ある金属中に拡散する。
This is of course true under certain conditions of use, as the temperature of the plated gold interlayer rises far above the predetermined limits and/or for longer periods of time, a rapid decrease in tensile strength occurs, likely due to structural changes. This defect of the heat exchanger according to the invention, which is only a hindrance in certain cases, can be eliminated in accordance with an advantageous embodiment of the invention as follows. That is, instead of a pure noble metal interlayer, especially a gold interlayer, an interlayer consisting of at least two phases is plated. In that case, the first layer, i.e. the layer directly on the body, consists of corrosion-resistant gold, and the next layer, especially the thin layer, consists of copper or is similar to copper with respect to the plating technology and metallurgical properties, and is made of gold alloy rules. It is comprised of a metal that can be layered over the first layer and that can form a more heat resistant alloy at relatively low temperatures and diffuse into the first layer. If such an intermediate layer of two or more layers is heated to about 150 qo, especially about 200 oo or more, the alloying metal will diffuse into the underlying or overlying metal.

前記金属はそれによって恐らくは混合結晶形成によるも
のと思われる良好な耐熱性をもつことになる。此の過程
は圧力の利用によって促進することができる。
The metal thereby has good heat resistance, probably due to mixed crystal formation. This process can be facilitated by the use of pressure.

その場合特に本発明による熱交換器の好ましい実施態様
の特性が利用される。即ち本体の熱膨脹係数が耐圧ジャ
ケットの材料のそれより大きい点である。耐圧ジャケッ
トの材料としてニッケル以外に特に銅コバルト合金及び
ニッケルコバルト合金が使用されうる。
In particular, the characteristics of the preferred embodiments of the heat exchanger according to the invention are utilized here. That is, the coefficient of thermal expansion of the main body is greater than that of the material of the pressure jacket. In addition to nickel, in particular copper-cobalt alloys and nickel-cobalt alloys can be used as materials for the pressure jacket.

実施例を示した図をもとに本発明を更に詳しく説明する
The present invention will be explained in more detail based on figures showing examples.

推進ノズルをもつ熱交換器は特殊鋼からなる本体1から
構成される。
The heat exchanger with propulsion nozzle consists of a body 1 made of special steel.

此の本体は従来の態様においてブロックから鍛造によっ
て予備製造し、切削によって製造することができる。本
体1に長手方向に延長する冷却管路2が作られる。これ
らの冷却管路の闇にウェプ3がある。これらの冷却管路
2を被う多層の外側ジャケットの製造のために容易に溶
融する導電性物質が冷却管路に充填される。その後本体
1にたとえば金の薄壁中間層4或いは金と銅又は金合金
が交互する相から成る薄壁中間層をメッキによって形成
する。此の中間層4の上にはニッケル又は等価の金属、
銅コバルト合金若しくはニッケルコバルト合金の肉厚の
大きい耐圧ジャケット5がメッキされる。この耐圧ジャ
ケットは燃焼室の高い内圧をうける。第3図に拡大断面
図で示した中間層4は金のいくつかの相4a〜4a″又
は銅若しくは金合金の相4b及び4b′を有する。
This body can be prefabricated from a block by forging and manufactured by machining in a conventional manner. A longitudinally extending cooling channel 2 is formed in the body 1. Web 3 exists in the darkness of these cooling pipes. For the production of a multilayer outer jacket covering these cooling channels 2, the cooling channels are filled with an easily meltable electrically conductive material. The body 1 is then provided with a thin-walled intermediate layer 4, for example of gold or of alternating phases of gold and copper or a gold alloy, by plating. On this intermediate layer 4, nickel or an equivalent metal,
A thick pressure jacket 5 made of copper cobalt alloy or nickel cobalt alloy is plated. This pressure jacket is subjected to the high internal pressure of the combustion chamber. The intermediate layer 4, shown in enlarged section in FIG. 3, has several phases 4a to 4a'' of gold or phases 4b and 4b' of copper or gold alloys.

此の中間層の厚さは、本発明による熱交換器のすべての
中間層のそれのように特に約20〜100山mであり、
金相4a〜4a″の厚さは特に夫々5〜2ふ特に7〜1
0山mであり、銅若しくは金合金相の厚さは特に夫々2
〜1リ特に3〜5ムmである。
The thickness of this intermediate layer, like that of all intermediate layers of the heat exchanger according to the invention, is in particular about 20 to 100 m;
The thickness of the gold phases 4a to 4a'' is preferably 5 to 2 mm, particularly 7 to 1 mm, respectively.
0 m, and the thickness of the copper or gold alloy phase is particularly 2 m.
-1, especially 3 to 5 mm.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は熱交換器の従断面図、第2図は第1図のローロ
線に沿う断面図、第3図は中間層の拡大断面図である。 第1図第2図 第3図
FIG. 1 is a sectional view of the heat exchanger, FIG. 2 is a sectional view taken along the Rolo line in FIG. 1, and FIG. 3 is an enlarged sectional view of the intermediate layer. Figure 1 Figure 2 Figure 3

Claims (1)

【特許請求の範囲】 1 冷却管路が本体にメツキされた肉厚の薄い中間層と
、この中間層にメツキされた肉厚が比較的厚い、ニツケ
ル又は等価の金属、銅コバルト合金若しくはニツケルコ
バルト合金から成る耐圧ジヤケツトとから形成される外
壁部によって被われる、少なくとも一つの推進燃料成分
が貫流することができる冷却管路を有する金属製の一体
の本体から構成される熱交換器において、 中間層は交
互に相異なる金属がメツキされて複数の層から構成され
ており、その際本体は耐食性の特殊鋼から成り、中間層
のうち本体に近い各第一層は金から成り、第一層に隣接
した各第二層は第一層中に拡散する銅若しくは金合金か
ら成ることを特徴とする熱交換器。 2 冷却管路が本体にメツキされた肉厚の薄い中間層と
、この中間層にメツキされた肉厚が比較的厚い、ニツケ
ル又は等価の金属、銅コバルト合金若しくはニツケルコ
バルト合金から成る耐圧ジヤケツトとから形成される外
壁部によって被われる、少なくとも一つの推進燃料成分
が貫流することができる冷却管路を有する金属製の一体
の本体から構成される熱交換器であって、かつ中間層が
交互に相異なる金属がメツキされて複数の層から構成さ
れており、その際本体は耐食性の特殊鋼から成り、中間
層のうち本体に近い各第一層は金から成り、第一層に隣
接した各第二層は第一層中に拡散する銅若しくは金合金
から成る熱交換器の製造方法において、冷却管路を有す
る本体を製造し、容易に溶融可能な導電性充填物質を冷
却管路に充填し、本体上に薄い中間層をメツキし、かつ
中間層上に比較的肉厚の厚い耐圧ジヤケツトをメツキし
、その後冷却管路から前記導電性充填物質を溶出するこ
とを特徴とする熱交換器の製造方法。
[Scope of Claims] 1. A thin intermediate layer with a cooling pipe plated on the main body, and a relatively thick intermediate layer plated with nickel or an equivalent metal, copper-cobalt alloy, or nickel-cobalt. A heat exchanger consisting of a one-piece body made of metal having a cooling channel through which at least one propellant component can flow, covered by an outer wall formed by a pressure jacket made of an alloy, an intermediate layer; is made up of several layers plated with different metals alternately, the main body being made of corrosion-resistant special steel, each first layer of the middle layer, which is closer to the main body, being made of gold; A heat exchanger characterized in that each adjacent second layer consists of a copper or gold alloy diffused into the first layer. 2. A thin intermediate layer with a cooling pipe plated on the main body, and a pressure-resistant jacket made of nickel or an equivalent metal, a copper-cobalt alloy, or a nickel-cobalt alloy, with a relatively thick wall plated on this intermediate layer. A heat exchanger consisting of a one-piece body of metal having cooling channels through which at least one propellant component can flow, covered by an outer wall formed of It consists of several layers plated with different metals, the main body being made of corrosion-resistant special steel, each first layer of the intermediate layer near the main body being made of gold, and each layer adjacent to the first layer being made of gold. The second layer is made of copper or gold alloy diffused into the first layer. In the method of manufacturing a heat exchanger, a body with cooling channels is manufactured, and the cooling channels are filled with an easily meltable conductive filling material. A heat exchanger characterized in that a thin intermediate layer is plated on the main body, a relatively thick pressure-resistant jacket is plated on the intermediate layer, and then the conductive filling material is eluted from the cooling pipe. manufacturing method.
JP50046591A 1974-04-19 1975-04-18 Heat exchanger and its manufacturing method Expired JPS6011222B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19742418885 DE2418885C3 (en) 1974-04-19 1974-04-19 Heat exchangers, in particular regeneratively cooled combustion chambers for liquid rocket engines and processes for their production
DE2418885.0 1974-04-19

Publications (2)

Publication Number Publication Date
JPS50140718A JPS50140718A (en) 1975-11-12
JPS6011222B2 true JPS6011222B2 (en) 1985-03-23

Family

ID=5913320

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50046591A Expired JPS6011222B2 (en) 1974-04-19 1975-04-18 Heat exchanger and its manufacturing method

Country Status (5)

Country Link
JP (1) JPS6011222B2 (en)
DE (1) DE2418885C3 (en)
FR (1) FR2268237B3 (en)
GB (1) GB1488959A (en)
IN (1) IN145321B (en)

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* Cited by examiner, † Cited by third party
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JPS62128847A (en) * 1985-11-29 1987-06-11 Toyota Motor Corp Sideview mirror bracket structure
JPH0247362B2 (en) * 1984-09-29 1990-10-19 Nissan Motor
JPH0247363B2 (en) * 1984-10-13 1990-10-19 Nissan Motor
JPH0364323B2 (en) * 1984-01-18 1991-10-04 Nissan Motor
JPH0436975Y2 (en) * 1985-07-16 1992-09-01

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3136252A1 (en) * 1981-09-12 1983-03-31 Rosenthal Technik Ag, 8672 Selb Ceramic combustion-chamber wall and method of manufacturing it
FR2551188A1 (en) * 1983-08-24 1985-03-01 Andre Landreau Boiler with combustion regulation, and method for regulating the combustion of a boiler.
DE4015204C1 (en) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE4137638C2 (en) * 1991-11-15 1994-08-11 Mtu Muenchen Gmbh Component with a wall to be protected against thermal stress
JP2902189B2 (en) * 1991-11-25 1999-06-07 石川島播磨重工業株式会社 Manufacturing method of gas distributor
CN113074387B (en) * 2021-04-29 2022-02-25 北京航空航天大学 Regenerative cooling channel with truss structure
CN114165362A (en) * 2021-11-08 2022-03-11 湖北三江航天江北机械工程有限公司 Composite forming method for combustion chamber of liquid rocket engine

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Patent Citations (1)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0364323B2 (en) * 1984-01-18 1991-10-04 Nissan Motor
JPH0247362B2 (en) * 1984-09-29 1990-10-19 Nissan Motor
JPH0247363B2 (en) * 1984-10-13 1990-10-19 Nissan Motor
JPH0436975Y2 (en) * 1985-07-16 1992-09-01
JPS62128847A (en) * 1985-11-29 1987-06-11 Toyota Motor Corp Sideview mirror bracket structure

Also Published As

Publication number Publication date
IN145321B (en) 1978-09-23
FR2268237A1 (en) 1975-11-14
JPS50140718A (en) 1975-11-12
DE2418885B2 (en) 1978-09-14
DE2418885A1 (en) 1975-10-30
GB1488959A (en) 1977-10-19
DE2418885C3 (en) 1979-05-10
FR2268237B3 (en) 1977-11-25

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