JPH0774601B2 - Ceramics turbine scroll and method for producing the same - Google Patents
Ceramics turbine scroll and method for producing the sameInfo
- Publication number
- JPH0774601B2 JPH0774601B2 JP14567691A JP14567691A JPH0774601B2 JP H0774601 B2 JPH0774601 B2 JP H0774601B2 JP 14567691 A JP14567691 A JP 14567691A JP 14567691 A JP14567691 A JP 14567691A JP H0774601 B2 JPH0774601 B2 JP H0774601B2
- Authority
- JP
- Japan
- Prior art keywords
- ceramics
- turbine scroll
- inner cylinder
- metal
- pores
- 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
- 239000000919 ceramic Substances 0.000 title claims description 67
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 229910052751 metal Inorganic materials 0.000 claims description 22
- 239000002184 metal Substances 0.000 claims description 22
- 239000012298 atmosphere Substances 0.000 claims description 12
- 239000010936 titanium Substances 0.000 claims description 12
- 239000011148 porous material Substances 0.000 claims description 11
- 150000004767 nitrides Chemical class 0.000 claims description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 8
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 8
- 239000001301 oxygen Substances 0.000 claims description 8
- 229910052760 oxygen Inorganic materials 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 238000005245 sintering Methods 0.000 claims description 7
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims description 6
- 229920003257 polycarbosilane Polymers 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 239000010703 silicon Substances 0.000 claims description 6
- 229910052719 titanium Inorganic materials 0.000 claims description 6
- 239000012299 nitrogen atmosphere Substances 0.000 claims description 5
- 229920001558 organosilicon polymer Polymers 0.000 claims description 5
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 4
- 229910052796 boron Inorganic materials 0.000 claims description 4
- 229910052735 hafnium Inorganic materials 0.000 claims description 4
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 239000011812 mixed powder Substances 0.000 claims description 4
- 229910052757 nitrogen Inorganic materials 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 4
- 229910052727 yttrium Inorganic materials 0.000 claims description 4
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 4
- 229910001018 Cast iron Inorganic materials 0.000 claims description 3
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 claims description 3
- 238000000151 deposition Methods 0.000 claims description 2
- 238000005121 nitriding Methods 0.000 claims description 2
- 239000010408 film Substances 0.000 claims 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 1
- 239000010409 thin film Substances 0.000 claims 1
- 229910052726 zirconium Inorganic materials 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 9
- 239000002131 composite material Substances 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 229910000505 Al2TiO5 Inorganic materials 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- AABBHSMFGKYLKE-SNAWJCMRSA-N propan-2-yl (e)-but-2-enoate Chemical compound C\C=C\C(=O)OC(C)C AABBHSMFGKYLKE-SNAWJCMRSA-N 0.000 description 4
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910021529 ammonia Inorganic materials 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910010038 TiAl Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- VRAIHTAYLFXSJJ-UHFFFAOYSA-N alumane Chemical compound [AlH3].[AlH3] VRAIHTAYLFXSJJ-UHFFFAOYSA-N 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、セラミックスタ−ビン
スク−ルおよびその製造方法に関し、特に熱の放散を極
力減らしたセラミックスと金属の複合体よりなるセラミ
ックスタ−ビンスクロ−ルとその製造方法に関するもの
である。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a ceramics turbine scroll and a method for producing the same, and more particularly to a ceramics turbine scroll comprising a composite of ceramics and a metal for reducing heat dissipation and a method for producing the same. It is a thing.
【0002】[0002]
【従来の技術】最近ファインセラミックス技術が注目さ
れ、この技術により製造されたセラミックスを用いて種
々の部品が製造され、たとえば、自動車用の内燃機関に
も多くのセラミックス製の部品が使用されている。2. Description of the Related Art Recently, fine ceramics technology has attracted attention, and various parts are manufactured by using the ceramics manufactured by this technology. For example, many ceramics parts are also used in internal combustion engines for automobiles. .
【0003】セラミックスの種類は極めて多く、それぞ
れ物性としてのそれら独特の特徴点をもっている。しか
し、たとえば内燃機関の部品のように、多くの特徴点を
兼ね備えていなければならない部品を構成する場合、1
種類のセラミックスでは実現不可能であるため、それぞ
れ特性が異なるセラミックスを数種類組合せて、あるい
はセラミックスと金属とを組み合わせて、要求特性に合
ったセラミックス複合体構造を案出することになる。The types of ceramics are extremely large, and each has their own characteristic points as physical properties. However, in the case of constructing a component that must have many features, such as a component of an internal combustion engine, 1
Since it is not possible to realize with various kinds of ceramics, it is necessary to combine several kinds of ceramics having different characteristics, or to combine ceramics and metals, to devise a ceramics composite structure that meets the required characteristics.
【0004】このようなセラミックス複合体を使用して
いる部品の一例として、内燃機関のスクロ−ルを挙げる
ことができる。An example of a component using such a ceramic composite is a scroll for an internal combustion engine.
【0005】従来のセラミックス複合体を用いた内燃機
関のスクロ−ルは、チタン酸アルミニウムからなる渦巻
状をした管状体の周囲をアルミニウム、鋳鉄などの金属
で鋳ぐるんだセラミックス複合体を用いたものが知られ
ている。A conventional scroll for an internal combustion engine using a ceramics composite uses a ceramics composite in which a spiral tubular body made of aluminum titanate is surrounded by a metal such as aluminum or cast iron. Things are known.
【0006】[0006]
【発明が解決しようとする課題】上述のような従来の内
燃機関のスクロ−ルは、断熱性はよいが、チタン酸アル
ムニウムの強度レベルが低いために、鋳ぐるんだ時の凝
固、収縮で発生する応力、あるいは作動時に発生する熱
応力その他の原因で破壊し易いという欠点を有する。The conventional scroll of the internal combustion engine as described above has a good heat insulating property, but since aluminum aluminum titanate has a low strength level, it is difficult to be solidified and contracted during casting. It has a drawback that it is easily broken due to the generated stress, the thermal stress generated during operation, or other causes.
【0007】本発明は、上述の如き従来の不都合を解消
しようとするものであり、その目的は、セラミックスと
金属の複合体からなるタ−ビンスクロ−ルにおいて、激
しい熱サイクルにも耐え、製造が簡単で低コストのセラ
ミックスタ−ビンスクロ−ルとその製造方法を得ること
にある。The present invention is intended to eliminate the above-mentioned conventional inconveniences, and an object of the present invention is to fabricate a turbine scroll made of a composite of ceramics and a metal, which can withstand a severe heat cycle and can be manufactured. It is to obtain a simple and low-cost ceramics turbine scroll and a manufacturing method thereof.
【0008】[0008]
【課題を解決するための手段】上記課題を解決するため
に、本発明は、珪素(Si)、窒素(N)、酸素
(O)、の全ての元素およびチタン(Ti),ジルコニ
ウム(Zr),ハフニウム(Hf),イットリウム
(Y),ホウ素(B),アルミニウム(Al)の元素群
の中の少なくとも1種類以上で構成され、かつ気孔を1
2%以上含むセラミックスとその外面に金属が配置され
ていることを特徴とするセラミックスタ−ビンスクロ−
ルを提供し、さらに珪素(Si)を主成分とし、これに
窒素(N)、酸素(O)、の全ての元素を含み、かつチ
タン(Ti),ジルコニウム(Zr),ハフニウム(H
f),イットリウム(Y),ホウ素(B),アルミニウ
ム(Al)の元素群の中の少なくとも1種類以上を含む
混合粉末を形成する工程と、該混合粉末を用いて渦巻形
状のセラミックスタ−ビンスクロ−ルの内筒を形成する
工程と、該渦巻形状のものを窒素雰囲気中で焼結して含
有各元素を窒化するとともに焼結する工程と、該窒化焼
結工程を経た後、酸素を含んだ雰囲気中で加熱して前記
窒化物の一部を酸化物に変化させる工程と、上記の各工
程を経て形成された焼結部品であるセラミックスタ−ビ
ンスクロ−ルの内筒を溶融金属中に浸漬して該内筒の周
囲に金属を被着する工程と、該被着された金属を所望の
形状に加工する工程とを含むことを特徴とするセラミッ
クスタ−ビンスクロ−ルの製造方法を提供する。In order to solve the above problems, the present invention provides all elements of silicon (Si), nitrogen (N), oxygen (O) and titanium (Ti), zirconium (Zr). , Hafnium (Hf), yttrium (Y), boron (B), aluminum (Al), and at least one kind of a group of pores.
A ceramics turbine scroll characterized in that ceramics containing 2% or more and a metal are arranged on the outer surface thereof.
And silicon (Si) as a main component, which contains all elements of nitrogen (N) and oxygen (O), and titanium (Ti), zirconium (Zr), hafnium (H).
f), a step of forming a mixed powder containing at least one element selected from the group of elements of yttrium (Y), boron (B), and aluminum (Al), and a spiral-shaped ceramics turbine scroll using the mixed powder. -A step of forming an inner cylinder of a slag, a step of sintering the spiral shape in a nitrogen atmosphere to nitride and sinter each element contained therein, and an oxygen-containing step after the nitriding and sintering step. In a molten atmosphere, the inner cylinder of the ceramics turbine scroll, which is a sintered part formed through the above steps, is heated in a molten atmosphere to change a part of the nitride into an oxide. Provided is a method for producing a ceramics turbine scroll, which comprises a step of immersing and depositing a metal around the inner cylinder, and a step of processing the deposited metal into a desired shape. To do.
【0009】[0009]
【実施例】以下、本発明の実施例を詳細に説明する。ま
ず、本発明に係るセラミックスタ−ビンスクロ−ルにつ
いて説明する。EXAMPLES Examples of the present invention will be described in detail below. First, the ceramics turbine scroll according to the present invention will be described.
【0010】図1において、1は内燃機関の排気管であ
り、その下部にはタ−ビンハウジング4にタ−ビンスク
ロ−ルが2が設けられている。3はタ−ビンホイ−ルで
ある。内燃機関から排気された排気ガスは矢印の通り流
れる。セラミックスタ−ビンスクロ−ルの内側には本発
明に係るセラミックスからなる渦巻型の内筒5が設けら
れ、その外側にはステンレス鋼製の外筒6が形成されて
いる。In FIG. 1, reference numeral 1 is an exhaust pipe of an internal combustion engine, and a turbine housing 2 is provided with a turbine scroll 2 at a lower portion thereof. 3 is a turbine wheel. Exhaust gas exhausted from the internal combustion engine flows as indicated by the arrow. A spiral-shaped inner cylinder 5 made of ceramics according to the present invention is provided inside the ceramics turbine scroll, and an outer cylinder 6 made of stainless steel is formed outside thereof.
【0011】図2において、セラミックスタ−ビンスク
ロ−ル2は、後に述べる製法でセラミックス製の内筒5
を作ってから該内筒5をステンレス鋼などの金属で鋳ぐ
るんで外筒6を形成して得られる。In FIG. 2, a ceramics turbine scroll 2 is an inner cylinder 5 made of ceramics by a manufacturing method described later.
It is obtained by forming the outer cylinder 6 by casting the inner cylinder 5 with a metal such as stainless steel.
【0012】前記セラミックスタ−ビンスクロ−ル2の
内筒5は次のようにして製造される。シリコン(Si)
の粉末100重量部に対して金属チタン(Ti)粉末5
重量部を加え、これにオイルを所定量配合した後に、加
圧ニ−ダで混練して可塑性を有する組成物を作成する。The inner cylinder 5 of the ceramics turbine scroll 2 is manufactured as follows. Silicon (Si)
Metallic titanium (Ti) powder 5 to 100 parts by weight of the powder
Parts by weight are added, and a predetermined amount of oil is mixed therein, and then kneaded with a pressure kneader to prepare a composition having plasticity.
【0013】別に内筒製造用の金型を作り、上記組成物
を該金型内に充填する。後にプレスにより略0.4トン
/cm2 の圧力で加圧してから、該成型された組成物を金
型から取り出す。なお、セラミックスタ−ビンスクロ−
ル2は渦巻型の筒状であるので、1回のプレス加工では
成型品を作ることができない。そこでまず渦巻型で筒状
の内筒を縦割りにした前記組成物からなる樋状の成型品
を2個作り、これらを接着剤で貼り合わせて筒状の内筒
を作り、これを炉に入れ、窒素雰囲気中で最高500℃
で脱脂し、同一の窒素雰囲気中で最高1400℃にて焼
成する。この焼成により上記組成物は完全に窒化し、内
部には略15パ−セントに近い容積を持ち、かつ均一に
分散した気孔が形成される。Separately, a mold for producing an inner cylinder is prepared, and the above composition is filled in the mold. Afterward, after pressing with a pressure of about 0.4 ton / cm @ 2, the molded composition is taken out of the mold. In addition, the ceramics turbine scroll
Since the rule 2 has a spiral tube shape, a molded product cannot be produced by a single pressing process. Therefore, first, two gutter-shaped molded products made of the above-mentioned composition in which a spirally-shaped cylindrical inner cylinder is vertically divided are made, and these are bonded with an adhesive to form a cylindrical inner cylinder, which is used in a furnace. Put in a nitrogen atmosphere up to 500 ℃
And degreasing and baking at a maximum of 1400 ° C. in the same nitrogen atmosphere. By this calcination, the above composition is completely nitrided, and pores having a volume close to 15% and having uniformly dispersed pores are formed therein.
【0014】次にこれを1000℃の大気中で加熱処理
を施した。この加熱処理後の寸法測定によれば、内筒の
寸法は金型での成型時の寸法とほとんど変わっていな
い。このようにして作られた内筒の外周をアルミニウム
あるいは鋳鉄などの金属で鋳ぐるみ、ディーゼルエンジ
ン用のタ−ビンスクロ−ルを作成する。内筒の周囲に金
属を鋳ぐるむ方法の一つとして、内筒の両側口を閉塞し
た後、これを溶融金属の中に浸漬してからこれを引き上
げて内筒の周囲に金属を被着して外筒を形成し、その
後、該金属を切削加工して所望の形状に仕上げる。な
お、上記大気中での焼結が終了した内筒の熱伝導率、強
度、熱膨張率係数、X線による生成物の同定結果を図3
および図4の図表図に示す。Next, this was heat-treated in the atmosphere at 1000 ° C. According to the dimension measurement after the heat treatment, the dimension of the inner cylinder is almost the same as the dimension at the time of molding with the mold. A turbine scroll for a diesel engine is produced by casting the outer periphery of the inner cylinder thus produced with a metal such as aluminum or cast iron. As one of the methods of casting metal around the inner cylinder, after closing both sides of the inner cylinder, immersing it in molten metal and then pulling it up to deposit metal around the inner cylinder. Then, an outer cylinder is formed, and then the metal is cut to finish it into a desired shape. The thermal conductivity, strength, coefficient of thermal expansion of the inner cylinder after sintering in the atmosphere and the product identification results by X-ray are shown in FIG.
And shown in the diagram of FIG.
【0015】以上のような製法により製造されたセラミ
ックス製の内筒5は、チタン酸アルミニウムにより制作
した従来の内筒に比べて熱的特性は同レベルであるが、
強度面で大きく優っていることが図3および図4の図表
図から分かる。The ceramic inner cylinder 5 manufactured by the above manufacturing method has the same level of thermal characteristics as the conventional inner cylinder made of aluminum titanate.
It can be seen from the diagrams of FIGS. 3 and 4 that the strength is greatly superior.
【0016】なお、このセラミックスタ−ビンスクロ−
ルは、内筒を作製する際、また該内筒に外筒を鋳ぐるむ
際に、破損は生じなかった。また、該セラミックスタ−
ビンスクロ−ルをディーゼルエンジンの排気管に接続
し、ベンチテストを行なった結果、耐久性についてはま
ったく問題はない。本願発明の要旨外の問題ではある
が、排気エネルギがセラミックス内燃機関のスクロ−ル
から外部に逸走しないので、燃料消費率も従来と比較し
て約2.9%向上していることも分かった。Incidentally, this ceramic turbine scroll
No damage occurred during the production of the inner cylinder or when the outer cylinder was cast around the inner cylinder. In addition, the ceramic target
As a result of performing a bench test by connecting the bin scroll to the exhaust pipe of the diesel engine, there is no problem in durability. Although it is a problem outside the scope of the present invention, it was also found that the exhaust energy does not escape from the scroll of the ceramic internal combustion engine to the outside, so that the fuel consumption rate is also improved by about 2.9% as compared with the conventional one. .
【0017】上記実施例の外に、本発明においては、シ
リコンSi粉末をベースにしてこれに配合する金属粉末
のパーセンテージを替え、またその種類を変え、さらに
セラミックス粉末のパーセンテージを替え、またその種
類を変えて、上記実施例と同様のセラミックス製の内筒
を作成した。図3の図表図において、実施例番号2乃至
9および図4の図表図で、10ないし13の実施例がそ
れである。In addition to the above examples, in the present invention, the percentage of the metal powder blended with silicon Si powder as a base is changed, the type thereof is changed, the percentage of the ceramic powder is changed, and the type thereof is changed. By changing the above, an inner cylinder made of ceramics similar to that in the above-mentioned example was prepared. In the diagram of FIG. 3, the embodiment numbers 2 to 9 and in the diagram of FIG. 4 are the examples 10 to 13.
【0018】次に示す実施例では、上記大気中での焼結
までが終了した実施例1の内筒をポリカルボシラン溶液
あるいは有機珪素ポリマ溶液に浸漬し、セラミックス内
部の気孔内にこれを含侵させた後、大気中あるいはアン
モニア雰囲気中で所定条件で加熱処理を行ない、この部
分を薄い窒化膜に転化させた。以降、上記の実施例と同
様にしてセラミックスタ−ビンスクロ−ルを作製した。
このようにして構成されたセラミックスタ−ビンスクロ
−ルは実施例1のものと比較して強度が幾分増加する。In the following embodiment, the inner cylinder of the embodiment 1 which has been sintered up to the atmosphere is immersed in a polycarbosilane solution or an organic silicon polymer solution, and the ceramic is contained in the pores inside the ceramic. After being soaked, a heat treatment was performed under a predetermined condition in the air or an ammonia atmosphere to convert this portion into a thin nitride film. After that, a ceramics turbine scroll was manufactured in the same manner as in the above-mentioned example.
The strength of the ceramics turbine scroll thus constructed is slightly increased as compared with that of the first embodiment.
【0019】さらに次の実施例では、上記実施例で使用
したポリカルボシラン溶液や有機珪素ポリマ溶液よりも
粘度の高いポリカルボシランペーストあるいは有機珪素
ポリマペーストを上記大気中での焼結までが終了した実
施例1のセラミックスタ−ビンスクロ−ルの内筒表面に
塗布し後、上記と同様な条件で焼成して前記内筒の表面
に薄い窒化膜を形成した。以降、上記の実施例と同様に
してセラミックスタ−ビンスクロ−ルを作製した。この
ようにして構成されたセラミックスタ−ビンスクロ−ル
は、排気ガスと接するセラミックスタ−ビンスクロ−ル
の内筒の内壁が薄い窒化膜に覆われているので、実施例
1のものと比較して断熱性が向上する。Further, in the next embodiment, the polycarbosilane paste or the organosilicon polymer paste having a viscosity higher than that of the polycarbosilane solution or the organosilicon polymer solution used in the above embodiment is sintered up to the atmosphere. After coating on the surface of the inner cylinder of the ceramics turbine scroll of Example 1, it was fired under the same conditions as above to form a thin nitride film on the surface of the inner cylinder. After that, a ceramics turbine scroll was manufactured in the same manner as in the above-mentioned example. In the ceramics turbine scroll thus constructed, the inner wall of the inner cylinder of the ceramics turbine scroll, which is in contact with the exhaust gas, is covered with a thin nitride film. Heat insulation is improved.
【0020】上記実施例群で検討した材料の内、実施例
10のチタン酸アルミ(TiAl2O5 ):15%,チ
タン(Ti):10%添加し、大気中での処理までの工
程を経て得た多孔質で低熱伝導のセラミックス材料につ
いて、トルエンで希釈したポリカルボシラン溶液に浸漬
し、セラミックスの中に形成された気孔にこれを含浸さ
せた後、アンモニア雰囲気中で熱分解させ、さらに窒素
雰囲気中での加熱処理により、気孔の表面の一部を非晶
質セラミックスで構成した。こうして得られた材料は、
図4の図表図に示すように、多孔質セラミックスの中の
気孔中に非晶質セラミックスが付着する。このようにし
て形成された多孔質セラミックスは、気孔量が20.1
%から17.1%と減りもとの材料に比べて約3%減少
しているが、強度は16%向上した。このことは、すべ
ての実施例についてもみられた。また、熱伝導率はこの
加工前と同じレベルであることが確認された。Among the materials examined in the above-mentioned group of Examples, aluminum titanate (TiAl 2 O 5 ) of Example 10: 15% and titanium (Ti): 10% were added, and the steps up to the treatment in the atmosphere were carried out. The resulting porous and low thermal conductivity ceramic material was dipped in a polycarbosilane solution diluted with toluene, and the pores formed in the ceramic were impregnated with it, followed by thermal decomposition in an ammonia atmosphere. A part of the surface of the pores was composed of amorphous ceramics by heat treatment in a nitrogen atmosphere. The material thus obtained is
As shown in the diagram of FIG. 4, the amorphous ceramics adhere to the pores in the porous ceramics. The porous ceramics thus formed has a porosity of 20.1.
%, Which is 17.1%, which is about 3% less than the original material, but the strength has been improved by 16%. This was also seen in all the examples. It was also confirmed that the thermal conductivity was at the same level as before this processing.
【0021】[0021]
【発明の効果】本発明は、セラミックスと金属の複合体
からなるセラミックスタ−ビンスクロ−ルにおいて、管
状体を構成するセラミックスであるチタン酸アルミニウ
ムの代わりに酸化物複合反応焼結セラミックスを用いて
セラミックスタ−ビンスクロ−ルを構成したので、熱伝
導率は従来形のものと同程度でありながら強度は従来の
ものより3倍であり、熱サイクルの激しい部分に使用す
る部品の信頼性が向上する。また、焼結時の寸法変化率
が小さく、また該変化率のばらつきも小さいので、金型
設計も容易となる。また、同じ理由で焼結後の加工量が
小さくなり、部品の低コストにつながる。INDUSTRIAL APPLICABILITY The present invention relates to a ceramics turbine scroll composed of a composite of ceramics and a metal, wherein an oxide composite reaction-sintered ceramics is used in place of aluminum titanate which is a ceramic constituting a tubular body. Since the turbine scroll is constructed, the thermal conductivity is about the same as that of the conventional type, but the strength is three times that of the conventional type, and the reliability of the parts used in the part where the heat cycle is intense is improved. . Further, since the dimensional change rate at the time of sintering is small and the variation in the change rate is small, the mold design becomes easy. Further, for the same reason, the processing amount after sintering becomes small, which leads to low cost of parts.
【図1】セラミックスタ−ビンスクロ−ルの一部破断正
面図。FIG. 1 is a partially cutaway front view of a ceramics turbine scroll.
【図2】セラミックスタ−ビンスクロ−ルの要部横断面
図。FIG. 2 is a lateral cross-sectional view of a main part of a ceramics turbine scroll.
【図3】図表図。FIG. 3 is a diagrammatic chart.
【図4】別の図表図。FIG. 4 is another diagram.
1・・・・・内燃機関の排気管 2・・・・・タ−ビンスクロ−ル 3・・・・・タ−ビンホイ−ル 4・・・・・タ−ビンハウジング 5・・・・・内筒 6・・・・・外筒 1 ... Exhaust pipe of internal combustion engine 2 ... Turbin scroll 3 ... Turbin wheel 4 ... Turbin housing 5 ... Inside Cylinder 6 ... Outer cylinder
Claims (8)
の全ての元素及びチタン(Ti),ジルコニウム(Z
r),ハフニウム(Hf),イットリウム(Y),ホウ
素(B),アルミニウム(Al)の元素群の中の少なく
とも1種類以上で構成されかつ気孔を12%以上含むセ
ラミックスとその外面に金属が配置されていることを特
徴とするセラミックスタ−ビンスクロ−ル。1. Silicon (Si), nitrogen (N), oxygen (O),
Of all elements and titanium (Ti), zirconium (Z
r), hafnium (Hf), yttrium (Y), boron (B), aluminum (Al) and at least one element selected from the group consisting of at least 12% of pores and a metal on the outer surface thereof. The ceramics turbine scroll which is characterized in that
されていることを特徴とする請求項1記載のセラミック
スタ−ビンスクロ−ル。2. A ceramics turbine scroll according to claim 1, wherein amorphous ceramics are formed inside said pores.
金属と接触していない内面には緻密なセラミックス薄膜
が形成されていることを特徴とする請求項1記載のセラ
ミックスタ−ビンスクロ−ル。3. A ceramics turbine scroll according to claim 1, wherein a dense ceramics thin film is formed on the inner surface of said ceramics containing 12% or more of pores, which is not in contact with the metal.
を特徴とする請求項1記載のセラミックスタ−ビンスク
ロ−ル。4. The ceramics turbine scroll according to claim 1, wherein the metal on the outer surface is aluminum.
する請求項1記載のセラミックスタ−ビンスクロ−ル。5. The ceramics turbine scroll according to claim 1, wherein the metal on the outer surface is cast iron.
(N)、酸素(O)、の全ての元素を含みかつチタン
(Ti),ジルコニウム(Zr),ハフニウム(H
f),イットリウム(Y),ホウ素(B),アルミニウ
ム(Al)の元素群の中の少なくとも1種類以上を含む
混合粉末を形成する工程と、該混合粉末を用いてセラミ
ックスタ−ビンスクロ−ルの内筒を形成する工程と、該
内筒を窒素雰囲気中で焼結して含有各元素を窒化すると
ともに焼結する工程と、該窒化焼結工程を経た後、酸素
を含んだ雰囲気中で加熱して前記窒化物の一部を酸化物
に変化させる工程と、上記の各工程を経て形成された焼
結部品であるセラミックスタ−ビンスクロ−ルの内筒を
溶融金属中に浸漬して該内筒の周囲に金属を被着する工
程と、該被着された金属を所望の形状に加工する工程と
を含むことを特徴とするセラミックスタ−ビンスクロ−
ルの製造方法。6. Silicon (Si) as a main component, containing all elements of nitrogen (N) and oxygen (O), and titanium (Ti), zirconium (Zr), hafnium (H).
f), a step of forming a mixed powder containing at least one element selected from the group of elements of yttrium (Y), boron (B), and aluminum (Al), and a step of forming a ceramic turbine scroll using the mixed powder. A step of forming an inner cylinder, a step of sintering the inner cylinder in a nitrogen atmosphere to nitride and sinter each contained element, and a heating in an atmosphere containing oxygen after the nitriding and sintering step. And a step of converting a part of the nitride into an oxide, and an inner cylinder of a ceramics turbine scroll, which is a sintered part formed through the above-mentioned steps, is dipped in a molten metal. A ceramics turbine scroll including a step of depositing a metal around a cylinder and a step of processing the deposited metal into a desired shape.
Manufacturing method.
加熱する工程の後、ポリカルボシランあるいは有機珪素
ポリマ溶液に浸漬した後、加熱処理して気孔中の表面に
薄い窒化膜を形成する工程を有することを特徴とする請
求項6記載のセラミックスタ−ビンスクロ−ルの製造方
法。7. After the step of heating a part of the inner cylinder in an atmosphere containing oxygen, it is immersed in a polycarbosilane or organic silicon polymer solution and then heat-treated to form a thin nitride film on the surface of the pores. 7. The method for manufacturing a ceramics turbine scroll according to claim 6, further comprising the step of forming.
加熱する工程の後、ポリカルボシランあるいは有機珪素
ポリマペーストを内筒内側面に塗布した後、加熱処理し
て該内筒内側面に薄い窒化膜を形成する工程を有するこ
とを特徴とする請求項6記載のセラミックスタ−ビンス
クロ−ルの製造方法。8. After the step of heating a part of the inner cylinder in an atmosphere containing oxygen, polycarbosilane or an organosilicon polymer paste is applied to the inner surface of the inner cylinder, and then heat treated to heat the inner cylinder. 7. The method for manufacturing a ceramics turbine scroll according to claim 6, further comprising the step of forming a thin nitride film on the inner surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14567691A JPH0774601B2 (en) | 1991-05-21 | 1991-05-21 | Ceramics turbine scroll and method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14567691A JPH0774601B2 (en) | 1991-05-21 | 1991-05-21 | Ceramics turbine scroll and method for producing the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH04347302A JPH04347302A (en) | 1992-12-02 |
| JPH0774601B2 true JPH0774601B2 (en) | 1995-08-09 |
Family
ID=15390515
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14567691A Expired - Lifetime JPH0774601B2 (en) | 1991-05-21 | 1991-05-21 | Ceramics turbine scroll and method for producing the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0774601B2 (en) |
-
1991
- 1991-05-21 JP JP14567691A patent/JPH0774601B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH04347302A (en) | 1992-12-02 |
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