JP2755931B2 - Heat-resistant structure - Google Patents
Heat-resistant structureInfo
- Publication number
- JP2755931B2 JP2755931B2 JP7310709A JP31070995A JP2755931B2 JP 2755931 B2 JP2755931 B2 JP 2755931B2 JP 7310709 A JP7310709 A JP 7310709A JP 31070995 A JP31070995 A JP 31070995A JP 2755931 B2 JP2755931 B2 JP 2755931B2
- Authority
- JP
- Japan
- Prior art keywords
- heat
- plating layer
- combustor
- present
- resistant structure
- 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 - Lifetime
Links
- 238000005530 etching Methods 0.000 claims description 14
- 239000000758 substrate Substances 0.000 claims description 4
- 238000007747 plating Methods 0.000 description 31
- 239000006185 dispersion Substances 0.000 description 20
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 101100008047 Caenorhabditis elegans cut-3 gene Proteins 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 229910052755 nonmetal Inorganic materials 0.000 description 3
- 230000008646 thermal stress Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 101100008048 Caenorhabditis elegans cut-4 gene Proteins 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005323 electroforming Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 150000002843 nonmetals Chemical class 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
Landscapes
- Chemically Coating (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Description
【０００１】[0001]
【発明の属する技術分野】本発明は、再使用型ロケッ
ト、ラム／スクラムエンジンの燃焼器、宇宙往還機の機
体等に用いられる耐熱構造物に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a heat-resistant structure used for a reusable rocket, a combustor of a ram / scram engine, a body of a spacecraft, and the like.
【０００２】[0002]
【従来の技術】従来、燃焼器等の高熱を受ける構造物の
耐熱構造としては、分散メッキ層によるものがある。図
５に分散メッキ層をもつ従来のロケット用の燃焼器を示
す。この燃焼器では、基材としてのニッケル、銅等の燃
焼器壁１の内面に分散メッキ層２を被覆するように形成
し、燃焼器内の高温の燃焼ガスに対する耐熱構造を構成
している。2. Description of the Related Art Conventionally, as a heat-resistant structure of a structure which receives high heat such as a combustor, there is a structure using a dispersed plating layer. FIG. 5 shows a conventional rocket combustor having a dispersed plating layer. In this combustor, a dispersion plating layer 2 is formed so as to cover the inner surface of a combustor wall 1 made of nickel, copper, or the like as a base material, and has a heat-resistant structure against high-temperature combustion gas in the combustor.
【０００３】前記の分散メッキ層２の材料としてはニッ
ケル−ジルコニア等が用いられ、同分散メッキ層２を形
成するメッキ法においては、金属（ニッケル等）と非金
属（ジルコニア等）の組成を傾斜させて燃焼ガスと接す
る分散メッキ層２の内面側に耐熱性の高い非金属を集中
させるようにしている。As a material for the dispersion plating layer 2, nickel-zirconia or the like is used. In the plating method for forming the dispersion plating layer 2, the composition of a metal (nickel or the like) and a non-metal (zirconia or the like) is inclined. In this way, non-metals having high heat resistance are concentrated on the inner surface side of the dispersion plating layer 2 in contact with the combustion gas.
【０００４】[0004]
【発明が解決しようとする課題】分散メッキ層を備えた
前記の従来の燃焼器では、燃焼試験を行うと、分散メッ
キ層の表面付近に大きな熱応力がかかり不規則なクラッ
クが生ずる。このクラックは燃焼試験の回数に比例して
成長し、分散メッキ層の剥離の原因となっていた。In the above-described conventional combustor provided with the dispersed plating layer, when a combustion test is performed, a large thermal stress is applied to the vicinity of the surface of the dispersed plating layer, and irregular cracks occur. The cracks grew in proportion to the number of times of the burning test, causing the peeling of the dispersion plating layer.
【０００５】耐熱効果が大きくて寿命の長い燃焼器を製
作するために、この課題を解決する必要があった。[0005] In order to produce a combustor having a large heat resistance effect and a long life, it was necessary to solve this problem.
【０００６】本発明は、以上に鑑みてなされたものであ
り、寿命の長い耐熱用部材を用いた耐熱構造物を提供し
ようとするものである。The present invention has been made in view of the above, and an object of the present invention is to provide a heat-resistant structure using a heat-resistant member having a long life.
【０００７】[0007]
【課題を解決するための手段】本発明の耐熱構造物は、
基材面上に形成された耐熱用部材の少くとも表面付近に
エッチングカットを設けたことを特徴とする。The heat-resistant structure of the present invention comprises:
An etching cut is provided at least near the surface of the heat-resistant member formed on the substrate surface.
【０００８】本発明では、基材面上に形成された耐熱用
部材の少くとも表面付近にエッチングカットを設けてい
るので、同エッチングカットによって耐熱用部材に作用
する熱応力が緩和される。これによって、耐熱用部材に
おいてクラックが発生・成長することがなく、耐熱用部
材の剥離が防止される。なお、エッチングカットの大き
さは、カットの幅が数１０ミクロン、ピッチは２〜３mm
から数１０mm程度にするのが望ましい。In the present invention, since the etching cut is provided at least near the surface of the heat-resistant member formed on the substrate surface, the etching cut reduces the thermal stress acting on the heat-resistant member. Thereby, cracks do not occur and grow in the heat-resistant member, and peeling of the heat-resistant member is prevented. The size of the etching cut is such that the width of the cut is several tens of microns and the pitch is 2-3 mm.
To several tens of mm.
【０００９】[0009]
【発明の実施の形態】本発明の実施の一形態を、図１な
いし図３によって説明する。本実施の形態では、図１に
示すように、燃焼器のニッケル、銅等の燃焼器壁１の内
面に耐熱用の分散メッキ層２を被覆するように形成する
と共に、同分散メッキ層２の表面から燃焼器壁１に接す
る面に至る厚さ方向に規則的な多数のエッチングカット
（プリクラック）３を設けている。前記分散メッキ層２
は、図５に示す従来の燃焼器における分散メッキ層と同
様に、ニッケル−ジルコニア等の材料から成り、金属
（ニッケル等）と非金属（ジルコニア等）の組成を傾斜
させて燃焼ガスと接する分散メッキ層２の内面側（燃焼
器壁１の反対側）の表面に耐熱性の高い非金属を集中さ
せるようにしている。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of the present invention will be described with reference to FIGS. In the present embodiment, as shown in FIG. 1, a dispersion plating layer 2 for heat resistance is formed so as to cover the inner surface of a combustor wall 1 made of nickel, copper, or the like of the combustor. A large number of regular etching cuts (pre-cracks) 3 are provided in the thickness direction from the surface to the surface in contact with the combustor wall 1. The dispersion plating layer 2
Is made of a material such as nickel-zirconia in the same manner as the dispersion plating layer in the conventional combustor shown in FIG. A non-metal having high heat resistance is concentrated on the inner surface of the plating layer 2 (the side opposite to the combustor wall 1).
【００１０】図２に分散メッキ法を用いた前記本発明の
実施の形態に係る燃焼器の製作方法を示す。図２（ａ）
に示すように先ずアルミマンドレル４を製作し、図２
（ｂ）に示すようにアルミマンドレル４上に分散メッキ
を行って分散メッキ層２を形成し、中間加工面５を設け
て任意の適当な肉厚にする。次に、図２（ｃ）に示すよ
うに分散メッキ層２の外面に燃焼器壁１を電鋳によって
生成し、図２（ｄ）に示すようにアルミマンドレルを溶
出又は分解取り外して燃焼器を完成する。FIG. 2 shows a method of manufacturing a combustor according to the embodiment of the present invention using a dispersion plating method. FIG. 2 (a)
First, an aluminum mandrel 4 was manufactured as shown in FIG.
As shown in (b), the dispersion plating is performed on the aluminum mandrel 4 to form the dispersion plating layer 2, and the intermediate processing surface 5 is provided so as to have any appropriate thickness. Next, as shown in FIG. 2C, a combustor wall 1 is formed on the outer surface of the dispersed plating layer 2 by electroforming, and as shown in FIG. Complete.
【００１１】図３は、前記図２に示す工程に際してエッ
チングカット３の製作を示す詳細図である。図３（ａ）
に示すように、分散メッキを行ってアルミマンドレル４
上に分散メッキ層２を形成する際に、予めマスキングを
施して２〜３mmから数１０mm程度のピッチで規則的に配
置され幅数１０ミクロンのエッチングカット３を形成す
る。分散メッキ層２に設けられた中間加工面５を中間加
工した後、図３（ｂ）に示すように、導電ワックス６を
エッチングカット３に詰める。FIG. 3 is a detailed view showing the production of the etching cut 3 in the step shown in FIG. FIG. 3 (a)
As shown in the figure, aluminum mandrel 4
When the dispersion plating layer 2 is formed thereon, masking is performed in advance to form etching cuts 3 regularly arranged at a pitch of about 2 to 3 mm to several tens of mm and several tens of microns in width. After the intermediate processing surface 5 provided on the dispersion plating layer 2 is subjected to intermediate processing, as shown in FIG. 3B, a conductive wax 6 is filled in the etching cut 3.
【００１２】さらに、図３（ｃ）に示すように、分散メ
ッキ層２の外面に燃焼器壁１を電鋳し、最後に、図３
（ｄ）に示すように、アルミマンドレル４と導電ワック
ス６を分解取り外し又は溶出して燃焼器が完成する。Further, as shown in FIG. 3C, a combustor wall 1 is electroformed on the outer surface of the dispersion plating layer 2, and finally, as shown in FIG.
As shown in (d), the aluminum mandrel 4 and the conductive wax 6 are decomposed and removed or eluted to complete the combustor.
【００１３】本発明の実施の形態においては、以上のよ
うに、燃焼器壁１の内面に分散メッキ層２が形成され、
この分散メッキ層の表面から燃焼器壁１に接する面に至
る厚さ方向に規則的な多数のエッチングカット３が設け
られているので、高温の燃焼ガスによって分散メッキ層
２の表面付近にかかる熱応力を緩和してクラックの発生
・生長を防止することができる。これによって、分散メ
ッキ層２が燃焼器壁１より剥離することがなく、燃焼器
の寿命を長くすることができる。In the embodiment of the present invention, as described above, the dispersed plating layer 2 is formed on the inner surface of the combustor wall 1,
Since a large number of regular etching cuts 3 are provided in the thickness direction from the surface of the dispersion plating layer to the surface in contact with the combustor wall 1, heat applied to the vicinity of the surface of the dispersion plating layer 2 by high-temperature combustion gas is obtained. The stress can be relieved to prevent the occurrence and growth of cracks. Thereby, the dispersed plating layer 2 does not peel off from the combustor wall 1, and the life of the combustor can be extended.
【００１４】なお、前記の本発明の実施の形態において
は、エッチングカット３は分散メッキ層２の全厚さにわ
たって形成されているが、これを分散メッキ層の表面付
近にのみ形成するようにすることもできる。In the above-described embodiment of the present invention, the etching cut 3 is formed over the entire thickness of the dispersion plating layer 2, but it is formed only near the surface of the dispersion plating layer. You can also.
【００１５】また、前記の本発明の実施の形態は、燃焼
器の耐熱構造物に係るが、図４に示すように、宇宙往還
機の大気圏再突入時に高熱入力のある機体前縁部と機体
下面の耐熱構造部７に本発明を適用することもできる。The above-described embodiment of the present invention relates to a heat-resistant structure of a combustor. As shown in FIG. The present invention can also be applied to the heat-resistant structure 7 on the lower surface.
【００１６】また更に、前記の本発明の実施の形態で
は、基材面上に耐熱用の分散メッキ層を形成している
が、本発明では、この分散メッキ層に代えてセラミック
ス等の耐熱用部材を広く用いることができる。Further, in the above-described embodiment of the present invention, a heat-resistant dispersed plating layer is formed on the surface of the base material. The member can be widely used.
【００１７】[0017]
【発明の効果】以上説明したように、本発明は、基材の
表面に形成された耐熱用部材の少くとも表面付近にエッ
チングカットを設けているので、同エッチングカットに
よって耐熱用部材に作用する熱応力が緩和され、クラッ
クの発生・生長を防止することができる。これによっ
て、耐熱用の耐熱用部材の剥離を防ぎ、耐熱構造物の寿
命を延ばすことができる。As described above, according to the present invention, since the etching cut is provided at least near the surface of the heat resistant member formed on the surface of the substrate, the etching cut acts on the heat resistant member. The thermal stress is reduced, and the occurrence and growth of cracks can be prevented. Accordingly, the heat-resistant member for heat resistance can be prevented from peeling, and the life of the heat-resistant structure can be extended.
【図１】本発明の実施の一形態に係る燃焼器を示し、図
１（ａ）はその断面図、図１（ｂ）は図１（ａ）のＡ部
の拡大図である。1 shows a combustor according to an embodiment of the present invention, FIG. 1 (a) is a cross-sectional view thereof, and FIG. 1 (b) is an enlarged view of a portion A in FIG. 1 (a).
【図２】図２（ａ）〜図２（ｄ）は前記本発明の実施の
一形態に係る燃焼器の製作工程の説明図である。2 (a) to 2 (d) are explanatory views of a manufacturing process of the combustor according to the embodiment of the present invention.
【図３】図３（ａ）〜図３（ｄ）は前記本発明の実施の
一形態に係る燃焼器の分散メッキ層にプリクラックを形
成する工程の説明図である。FIGS. 3 (a) to 3 (d) are explanatory views of a process of forming a pre-crack on a dispersion plating layer of the combustor according to the embodiment of the present invention.
【図４】本発明に係る耐熱構造物が適用される宇宙往還
機の概略図である。FIG. 4 is a schematic view of a spacecraft to which the heat-resistant structure according to the present invention is applied.
【図５】従来の分散メッキ層を用いた燃焼器の要部の説
明図である。FIG. 5 is an explanatory diagram of a main part of a conventional combustor using a dispersed plating layer.
１ 燃焼器壁 ２ 分散メッキ層 ３ エッチングカット ４ アルミマンドレル ５ 中間加工面 ６ 導電ワックス ７ 耐熱構造部 DESCRIPTION OF SYMBOLS 1 Combustor wall 2 Dispersion plating layer 3 Etching cut 4 Aluminum mandrel 5 Intermediate processing surface 6 Conductive wax 7 Heat resistant structure
───────────────────────────────────────────────────── フロントページの続き (72)発明者 田口 秀之 愛知県小牧市大字東田中1200番地 三菱 重工業株式会社名古屋誘導推進システム 製作所内 (56)参考文献 特開 昭62−253713（ＪＰ，Ａ) 特開 昭63−277748（ＪＰ，Ａ) (58)調査した分野(Int.Cl.6，ＤＢ名) F02K 9/62 C23C 30/00──────────────────────────────────────────────────続 き Continuation of the front page (72) Inventor Hideyuki Taguchi 1200, Higashi Tanaka, Oaza, Komaki City, Aichi Prefecture Mitsubishi Heavy Industries, Ltd. Nagoya Guidance and Propulsion System Works (56) References 63-277748 (JP, A) (58) Fields investigated (Int. Cl. 6 , DB name) F02K 9/62 C23C 30/00
Claims (1)
とも表面付近にエッチングカットを設けたことを特徴と
する耐熱構造物。1. A heat-resistant structure wherein an etching cut is provided at least near the surface of a heat-resistant member formed on a substrate surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7310709A JP2755931B2 (en) | 1995-11-29 | 1995-11-29 | Heat-resistant structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7310709A JP2755931B2 (en) | 1995-11-29 | 1995-11-29 | Heat-resistant structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH09151799A JPH09151799A (en) | 1997-06-10 |
| JP2755931B2 true JP2755931B2 (en) | 1998-05-25 |
Family
ID=18008531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7310709A Expired - Lifetime JP2755931B2 (en) | 1995-11-29 | 1995-11-29 | Heat-resistant structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2755931B2 (en) |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2594851A1 (en) * | 1986-02-25 | 1987-08-28 | Cegedur | METAL PARTS WITH AT LEAST SIDE OF AT LEAST ONE AREA OF WEAR-RESISTANT ZONES |
| JPS63277748A (en) * | 1987-05-11 | 1988-11-15 | Toshiba Corp | Formation of heat-resistant coating layer |
-
1995
- 1995-11-29 JP JP7310709A patent/JP2755931B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH09151799A (en) | 1997-06-10 |
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