JPH0441682A - Suction and exhaust valve for internal-combustion engine made of titanium aluminide - Google Patents

Suction and exhaust valve for internal-combustion engine made of titanium aluminide

Info

Publication number
JPH0441682A
JPH0441682A JP15079790A JP15079790A JPH0441682A JP H0441682 A JPH0441682 A JP H0441682A JP 15079790 A JP15079790 A JP 15079790A JP 15079790 A JP15079790 A JP 15079790A JP H0441682 A JPH0441682 A JP H0441682A
Authority
JP
Japan
Prior art keywords
valve
core material
titanium aluminide
combustion engine
outer skin
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
Application number
JP15079790A
Other languages
Japanese (ja)
Inventor
Masaki Kumagai
正樹 熊谷
Kazuhisa Shibue
渋江 和久
Takeshi Kawabata
武 川畑
Bokujiyun Kin
金 睦淳
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.)
Sumitomo Light Metal Industries Ltd
Original Assignee
Sumitomo Light Metal Industries Ltd
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 Sumitomo Light Metal Industries Ltd filed Critical Sumitomo Light Metal Industries Ltd
Priority to JP15079790A priority Critical patent/JPH0441682A/en
Publication of JPH0441682A publication Critical patent/JPH0441682A/en
Pending legal-status Critical Current

Links

Landscapes

  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

PURPOSE:To render high toughness as well as superior strength and heat resistance by coating the surface of the core material of a valve made of titanium aluminide having a specified compsn. with a Ti or Ni shell. CONSTITUTION:The compsn. of the core material of a valve made of titanium aluminide is composed of 25-75atomic% Ti and 25-75atomic% Al. Al least part of the surface of the core material is coated with a Ti or Ni shell to obtain a suction and exhaust valve for an internal-combustion engine. A small amt. of one or more among Cr, Mn, V, Co, Zr, Y, Mo, Nb, Hf, Ta, W, Ce, Nd, Si, B, O, C and N may be incorporated into the Al in the compsn. of the core material as required. The pref. thickness of the shell is 0.1-50% of the thickness of the valve head. The durability of the valve can be improved.

Description

【発明の詳細な説明】 [産業上の利用分野コ この発明はチタニウムアルミナイド製内燃機関用吸、排
気バルブに関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] This invention relates to titanium aluminide intake and exhaust valves for internal combustion engines.

[従来技術〕 現在知られているチタニウムアルミナイドは強度及び耐
熱性が優れているが靭性が低い欠点がある。この為耐久
性が低く内燃機関の吸、排気バルブ用材料としては不適
当である。
[Prior Art] Currently known titanium aluminide has excellent strength and heat resistance, but has the drawback of low toughness. For this reason, it has low durability and is unsuitable as a material for intake and exhaust valves in internal combustion engines.

[発明が解決しようとする課題] 優れた強度及び耐熱性の外に高い靭性を有するチタニウ
ムアルミナイド製内燃機関用吸、排気バルブの提供を課
題とする。
[Problems to be Solved by the Invention] An object of the present invention is to provide intake and exhaust valves for internal combustion engines made of titanium aluminide, which have excellent strength and heat resistance as well as high toughness.

[課題を解決するための技術的手段] 上記の課題を解決するためこの発明は下記組成のチタニ
ウムアルミナイド製の、バルブの形状を有するバルブ芯
材と、このバルブ芯材の表面の少なくとも一部を覆うT
:又はN;の外皮とからなっている。
[Technical Means for Solving the Problems] In order to solve the above problems, the present invention provides a valve core material having the shape of a valve, made of titanium aluminide having the following composition, and at least a part of the surface of this valve core material. Cover T
: or N;.

25at%≦Ti≦75at% 25at%≦Al≦75at% [作用] 上記チタニウムアルミナイド製内燃機関用吸、排気バル
ブはチタニウムアルミナイド製の、バルブの形状を有す
るバルブ芯材が優れた強度及び耐熱性を有しており、バ
ルブ芯材の表面の少なくとも一部を覆うTi又はNiの
外皮が優れた靭性を有しているのでバルブ全体として優
れた強度、耐熱性及び靭性を有することになり、内燃機
関用膜、排気バルブとして優れた機能を発揮する。
25at%≦Ti≦75at% 25at%≦Al≦75at% [Function] The above titanium aluminide intake and exhaust valves for internal combustion engines are made of titanium aluminide and have a valve core material in the shape of a valve that has excellent strength and heat resistance. The Ti or Ni outer skin that covers at least a portion of the surface of the valve core material has excellent toughness, so the valve as a whole has excellent strength, heat resistance, and toughness, making it suitable for internal combustion engines. Demonstrates excellent functions as a membrane and exhaust valve.

L実施例J 以下実施例を示す図面によりこの発明を説明する。第1
図は第1実施例を示す。第1図(イ)の1はバルブ芯材
で、T i −36wt%A]のチタニウムアルミナイ
ドを使用し、バルブに近い形状に1600℃で鋳造し、
切削により所望のバルブよりヤヤ小さい寸法に形成され
ている。このバルブ芯材1を第1図(ロ)に示すように
真空中でN缶2内に封入する。次に第1図(ハ)に示す
ように1300℃×1時間、1000気圧(7)Ar7
jスHIP(熱間静水圧処理)する。このHIPにより
バルブ芯材1の全表面にN1缶2が密着してN1を外皮
3として有するバルブ形状体4となる。
L Example J This invention will be explained below with reference to drawings showing examples. 1st
The figure shows a first embodiment. 1 in Fig. 1 (A) is the valve core material, which is made of titanium aluminide with Ti -36wt%A] and is cast at 1600°C into a shape similar to the valve.
By cutting, it is formed into a size that is much smaller than the desired valve. This valve core material 1 is sealed in an N can 2 in a vacuum as shown in FIG. 1 (b). Next, as shown in FIG.
jSu HIP (hot isostatic pressure treatment). This HIP brings the N1 can 2 into close contact with the entire surface of the valve core material 1, resulting in a valve-shaped body 4 having N1 as the outer skin 3.

このバルブ形状体4を1300’CX24時間の均質化
処理を施し、切削により所望のバルブ形状とする。
This valve-shaped body 4 is subjected to a homogenization treatment at 1300'CX for 24 hours, and cut into a desired valve shape.

第2図は第2実施例を示す。第2図(イ)の11は円柱
状の芯材で、この芯材11はr*−33wt%At−3
wt%Mrlとなるようにli粉末及びAl−Mn合金
粉末を混合し、Al缶に入れて500℃で脱気後68φ
から26φに押し出され、この押出し材を25mの長さ
に切断したものである。芯材11に外径が30φになる
ように一端閉鎖、他端解放のTi缶12を被せて被覆体
13とする。この被覆体13を第2図(ロ)に示すよう
にバルブ形状型14の中に据え込んでバルブ形状体15
を得た。従ってバルブ形状体15はバルブ芯材15aと
Tiの外皮15bとから構成されている。なお、第2図
(ロ)に示すようにバルブ芯材15aの上、下面は外皮
15bで被覆されていない。このバルブ形状体15を1
200℃x2時間、Arガス中1300気圧でHIPし
た後1200’CX24時間均質化処理をし、切削して
所望のバルブとする。
FIG. 2 shows a second embodiment. 11 in FIG. 2(A) is a cylindrical core material, and this core material 11 is r*-33wt%At-3
Mix li powder and Al-Mn alloy powder so that wt% Mrl, put in an Al can, degas at 500℃, and then heat to 68φ.
This extruded material was extruded to a diameter of 26 mm and cut into a length of 25 m. The core material 11 is covered with a Ti can 12 with one end closed and the other end open so as to have an outer diameter of 30φ to form a covering 13. As shown in FIG.
I got it. Therefore, the valve-shaped body 15 is composed of a valve core material 15a and a Ti outer skin 15b. Note that, as shown in FIG. 2(b), the upper and lower surfaces of the valve core material 15a are not covered with the outer skin 15b. This valve-shaped body 15 is
After HIPing at 200° C. for 2 hours at 1300 atmospheres in Ar gas, homogenization treatment was performed at 1200° C. for 24 hours, and the desired valve was cut.

第3実施例として図示しないがバルブ形状に近い形ニT
 i −36wt%A +を1600℃F溶解鋳造し、
切削によりバルブ形状よりヤヤ小さく成形したものに、
Tiを表面に1mの厚さになるように溶射した後所望の
形状に仕上げることも可能である。
Although not shown as a third embodiment, a shape similar to a valve shape is shown in FIG.
i -36wt% A + was melted and cast at 1600°C,
It is molded by cutting to be much smaller than the valve shape.
It is also possible to thermally spray Ti onto the surface to a thickness of 1 m and then finish it into a desired shape.

第3.4.5図はいずれも第1図のバルブ形状体4及び
第2図のバルブ形状体15と異なるバルブ形状体の実施
例を示す。第3図(第4実施例)のバルブ形状体16は
バルブ芯材16aのステムの上端面を除いてT1又はN
iの外皮16bで被覆され、第4図(第5実施例)のバ
ルブ形状体っ7はバルブ芯材17aのフェイス部全体と
ステム部の一部がTi又はNiの外皮17bて被覆され
ている。第5図(第6実施例)のバルブ形状体18はバ
ルブ芯材18aのフェイス部の下面のみがT1又はNi
の外皮18bで被覆されている。
3.4.5 each show an embodiment of a valve body different from the valve body 4 of FIG. 1 and the valve body 15 of FIG. 2. The valve-shaped body 16 in FIG. 3 (fourth embodiment) is T1 or N except for the upper end surface of the stem of the valve core material 16a.
In the valve-shaped body 7 of FIG. 4 (fifth embodiment), the entire face portion and part of the stem portion of the valve core material 17a are covered with a Ti or Ni outer skin 17b. . In the valve-shaped body 18 of FIG. 5 (sixth embodiment), only the lower surface of the face portion of the valve core material 18a is made of T1 or Ni.
It is covered with an outer skin 18b.

第6図は第7実施例のバルブ形状体19を示す。FIG. 6 shows a valve-shaped body 19 of a seventh embodiment.

バルブ形状体19はバルブ形状体16においてノベルブ
ヘッドの厚さbに対するTi又はNi外皮の厚さb−a
が0.1〜50%のものを示して0る。
The valve shape body 19 has a thickness b-a of the Ti or Ni outer skin relative to the thickness b of the novel head in the valve shape body 16.
is 0.1 to 50%.

なお、第6図で198はチタニウムアルミナイドからな
るバルブ芯材を示し、19bはTi又(よNiの外皮を
示す。
In FIG. 6, 198 indicates a valve core material made of titanium aluminide, and 19b indicates an outer skin made of Ti or Ni.

表1は第1〜3実施例の特性を示す。伸びの測定及びシ
ャルピー試験はバルブのステム部で行なった。表1から
第1〜3実施例のバルブは靭性の優れた適当な厚さのT
i又はNiの外皮を有するのでバルブは靭性に富み、実
機の寿命を長くすることが明らかである。
Table 1 shows the characteristics of the first to third examples. Elongation measurements and Charpy tests were performed on the valve stem. From Table 1, the valves of Examples 1 to 3 are made of T having an appropriate thickness and excellent toughness.
It is clear that since the valve has an outer skin of Ni or Ni, it has high toughness and prolongs the life of the actual machine.

上記の各実施例において、Al合金の成分(81%)と
して下記のうち1種以上を含有し、残部をAIとしても
よい。
In each of the above examples, one or more of the following may be contained as the Al alloy component (81%), and the remainder may be AI.

Cr・0.05〜10 Mn・・・0.05〜10 V  ・・・0.05〜10 Co0.05〜10 Z「・・・0.05〜10 Y ・・・0.05〜10 Mo・・・0.05〜10 Nb・・・0.05〜10 1−(f・・・0.05〜10 丁a・0.01〜10 W ・・・0.01〜10 Ce・・・0.01〜10 Nd・・・0.01〜10 Si・・・0.001〜10 B ・・・0.01〜5.0 0 ・・・0.01〜1.0 C・・・0.001〜5. O N ・・・0.001〜5.0 チタニウムアルミナイド製造の際上記の各成分に付いて
注意すべきことは (イ)At、Ti、Fe、Niに付イて25at%未渦
の場合、又は75at%を越える場合は合金反応せず、
金属間化合物とすることが困難である。
Cr・0.05-10 Mn...0.05-10 V...0.05-10 Co0.05-10 Z"...0.05-10 Y...0.05-10 Mo ...0.05-10 Nb...0.05-10 1-(f...0.05-10 C a.0.01-10 W...0.01-10 Ce... 0.01-10 Nd...0.01-10 Si...0.001-10 B...0.01-5.0 0...0.01-1.0 C...0 .001~5.O N...0.001~5.0 When producing titanium aluminide, the following points should be noted regarding each of the above components: (a) 25 at% for At, Ti, Fe, and Ni. If there is no vortex or if it exceeds 75 at%, the alloy will not react,
It is difficult to form it into an intermetallic compound.

(ロ)Cr、Mn、B、C,NについTCr、1vln
は0.05at%未満、Bは0.01at%未満、C,
Nは0.0018t%未満では延性の向上が見られない
。又Cr、 Mnは10at%を、B、C,Nは5.Q
at%を越えると延性の改良が飽和する。
(b) TCr, 1vln for Cr, Mn, B, C, N
is less than 0.05 at%, B is less than 0.01 at%, C,
If N is less than 0.0018t%, no improvement in ductility is observed. Also, Cr and Mn are 10 at%, and B, C, and N are 5. Q
Above at%, the improvement in ductility is saturated.

(ハ>W、Siについて Wは0.01at%未満、Siは0.0018t%未満
では耐酸化性の向上が見られず、又W、Siは10at
%を越えると耐酸化性が飽和する。
(C> Regarding W and Si, no improvement in oxidation resistance is observed when W is less than 0.01 at% and Si is less than 0.0018 t%, and W and Si are less than 10 at%.
%, oxidation resistance becomes saturated.

(ニ)Co、Zr、Y、Mo、Nb、1−1f、 Ta
、Ce、Nd、Oにライて Co、Zr、Y、MOlNb、Hfは0.05at%未
満、Ta、Ce、Nd、Oは0.01at%未満では強
度の向上が見られず、又多元素は10at%を越えると
強度が飽和する。
(d) Co, Zr, Y, Mo, Nb, 1-1f, Ta
, Ce, Nd, O, Co, Zr, Y, MOINb, Hf is less than 0.05 at%, Ta, Ce, Nd, O is less than 0.01 at%, no improvement in strength is observed, and multi-element When the amount exceeds 10 at%, the strength is saturated.

(ホ)外皮の厚さ Tr、Nrの外皮の厚さがバルブ芯材の厚さの0.1%
未満では靭性を高める効果がない。又50%を越えると
チタニウムアルミナイド本来の耐熱性が大きく失われる
(e) Thickness of the outer skin Tr, the thickness of the outer skin of Nr is 0.1% of the thickness of the valve core material
If it is less than that, there is no effect of increasing toughness. Moreover, if it exceeds 50%, the inherent heat resistance of titanium aluminide will be greatly lost.

[効果] この発明のチタニウムアルミナイド製内燃機関用吸、排
気バルブは上記の構成を有するので強度、耐熱性の外に
靭性が非常に優れているので耐久性がおる。従って内燃
機関用吸、排気バルブの材料として非常に適している。
[Effects] The titanium aluminide intake and exhaust valves for internal combustion engines of the present invention have the above-mentioned structure, and have excellent toughness and durability in addition to strength and heat resistance. Therefore, it is very suitable as a material for intake and exhaust valves for internal combustion engines.

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

第1図は第1実施例を示し、(イ)はバルブ芯材の正面
図を、(ロ)は製作過程の正断面図を、(ハ)はバルブ
形状体の正断面図を示す。第2図は第2実施例を示し、
(イ)は芯材をTi缶で被覆したものの正断面図を図を
、(ロ)はバルブ形状体の正断面図を示す。第3.4.
5図はそれぞれバルブ形状体の異なる例の正断面図を示
す。第6図は第3図の特別例を示す。 1・・・バルブ芯材 3・・・外皮 4・・・バルブ形状体 15・・・バルブ形状体 15a・・・バルブ芯材   15b・・・外皮16・
・・バルブ形状体 16a・・・バルブ芯材   16b・・・外皮17・
・・バルブ形状体 17a・・・バルブ芯材   17b・・・外皮18・
・・バルブ形状体 18a・・・バルブ芯材   18b・・・外皮19・
・・バルブ形状体
FIG. 1 shows a first embodiment, in which (a) shows a front view of the valve core material, (b) shows a front sectional view of the manufacturing process, and (c) shows a front sectional view of the valve-shaped body. FIG. 2 shows a second embodiment,
(a) shows a front sectional view of a core material covered with a Ti can, and (b) shows a front sectional view of a valve-shaped body. Section 3.4.
FIG. 5 each shows a front sectional view of a different example of a valve shape. FIG. 6 shows a special example of FIG. 1... Valve core material 3... Outer skin 4... Valve shaped body 15... Valve shaped body 15a... Valve core material 15b... Outer skin 16.
...Valve shaped body 16a...Valve core material 16b...Outer skin 17.
...Valve shaped body 17a...Valve core material 17b...Outer skin 18.
...Valve shaped body 18a...Valve core material 18b...Outer skin 19.
・・Valve shape body

Claims (3)

【特許請求の範囲】[Claims] (1)下記組成のチタニウムアルミナイド製の、バルブ
の形状を有するバルブ芯材と、このバルブ芯材の表面の
少なくとも一部を覆うTi又はNiの外皮とからなるこ
とを特徴とするチタニウムアルミナイド製内燃機関用吸
、排気バルブ。 25at%≦Ti≦75at% 25at%≦Al≦75at%
(1) An internal combustion engine made of titanium aluminide, characterized by comprising a valve core material in the shape of a valve made of titanium aluminide having the following composition, and an outer skin of Ti or Ni that covers at least a portion of the surface of the valve core material. Engine intake and exhaust valves. 25at%≦Ti≦75at% 25at%≦Al≦75at%
(2)AlがAt%で下記元素の1種以上を含み、残余
はAlであることを特徴とする請求項(1)記載のチタ
ニウムアルミナイド製内燃機関用吸、排気バルブ。 Cr・・・0.05〜10 Mn・・・0.05〜10 V・・・0.05〜10 Co・・・0.05〜10 Zr・・・0.05〜10 Y・・・0.05〜10 Mo・・・0.05〜10 Nb・・・0.05〜10 Hf・・・0.05〜10 Ta・・・0.05〜10 W・・・0.05〜10 Ce・・・0.05〜10 Nd・・・0.05〜10 Si・・・0.001〜10 B・・・0.01〜5.0 O・・・0.01〜1.0 C・・・0.001〜5.0 N・・・0.001〜5.0
(2) The titanium aluminide intake and exhaust valve for an internal combustion engine according to claim (1), wherein Al contains at least one of the following elements in At%, and the remainder is Al. Cr...0.05-10 Mn...0.05-10 V...0.05-10 Co...0.05-10 Zr...0.05-10 Y...0 .05-10 Mo...0.05-10 Nb...0.05-10 Hf...0.05-10 Ta...0.05-10 W...0.05-10 Ce ...0.05-10 Nd...0.05-10 Si...0.001-10 B...0.01-5.0 O...0.01-1.0 C. ...0.001-5.0 N...0.001-5.0
(3)バルブヘッドを覆うTi又はNiの外皮の厚さが
バルブヘッドの厚さに対し0.1〜50%であることを
特徴とする請求項(1)又は(2)記載のチタニウムア
ルミナイド製内燃機関用吸、排気バルブ。
(3) Made of titanium aluminide according to claim (1) or (2), wherein the thickness of the Ti or Ni outer skin covering the valve head is 0.1 to 50% of the thickness of the valve head. Intake and exhaust valves for internal combustion engines.
JP15079790A 1990-06-08 1990-06-08 Suction and exhaust valve for internal-combustion engine made of titanium aluminide Pending JPH0441682A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15079790A JPH0441682A (en) 1990-06-08 1990-06-08 Suction and exhaust valve for internal-combustion engine made of titanium aluminide

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15079790A JPH0441682A (en) 1990-06-08 1990-06-08 Suction and exhaust valve for internal-combustion engine made of titanium aluminide

Publications (1)

Publication Number Publication Date
JPH0441682A true JPH0441682A (en) 1992-02-12

Family

ID=15504644

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15079790A Pending JPH0441682A (en) 1990-06-08 1990-06-08 Suction and exhaust valve for internal-combustion engine made of titanium aluminide

Country Status (1)

Country Link
JP (1) JPH0441682A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0636701A3 (en) * 1993-07-19 1995-03-29 Howmet Corp Creep resistant titanium aluminide alloy.
WO1995024511A1 (en) * 1994-03-10 1995-09-14 Nippon Steel Corporation Titanium-aluminium intermetallic compound alloy material having superior high temperature characteristics and method for producing the same
US6521059B1 (en) 1997-12-18 2003-02-18 Alstom Blade and method for producing the blade
FR2868791A1 (en) * 2004-04-07 2005-10-14 Onera (Off Nat Aerospatiale) DUCTILE HOT TITANIUM ALUMINUM ALLOY
CN103572102A (en) * 2013-11-05 2014-02-12 姚芸 High-temperature heat-resistant aluminum alloy
CN104328311A (en) * 2014-10-30 2015-02-04 西北工业大学 Heat-crack-resistant medium-niobium cast TiAl alloy with over-peritectic solidification characteristic
CN110643877A (en) * 2019-09-09 2020-01-03 中国航发北京航空材料研究院 TiAl intermetallic compound containing W, Mn, Si, B, C and rare earth elements

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0636701A3 (en) * 1993-07-19 1995-03-29 Howmet Corp Creep resistant titanium aluminide alloy.
WO1995024511A1 (en) * 1994-03-10 1995-09-14 Nippon Steel Corporation Titanium-aluminium intermetallic compound alloy material having superior high temperature characteristics and method for producing the same
US6521059B1 (en) 1997-12-18 2003-02-18 Alstom Blade and method for producing the blade
FR2868791A1 (en) * 2004-04-07 2005-10-14 Onera (Off Nat Aerospatiale) DUCTILE HOT TITANIUM ALUMINUM ALLOY
EP1584697A3 (en) * 2004-04-07 2009-07-15 ONERA (Office National d'Etudes et de Recherches Aérospatiales) Titanium-aluminium alloy having high-temperature ductility
CN103572102A (en) * 2013-11-05 2014-02-12 姚芸 High-temperature heat-resistant aluminum alloy
CN104328311A (en) * 2014-10-30 2015-02-04 西北工业大学 Heat-crack-resistant medium-niobium cast TiAl alloy with over-peritectic solidification characteristic
CN110643877A (en) * 2019-09-09 2020-01-03 中国航发北京航空材料研究院 TiAl intermetallic compound containing W, Mn, Si, B, C and rare earth elements

Similar Documents

Publication Publication Date Title
KR100244786B1 (en) Exhaust valve for diesel internal combustion engine and its manufacturing method
RU2175722C2 (en) Movable partition member in form of outlet valve or piston in internal combustion engine
US4437913A (en) Cobalt base alloy
US4789412A (en) Cobalt-base alloy having high strength and high toughness, production process of the same, and gas turbine nozzle
US5076866A (en) Heat resistant slide member for internal combustion engine
US20050238907A1 (en) Highly oxidation resistant component
US5196162A (en) Ti-Al type lightweight heat-resistant materials containing Nb, Cr and Si
DK172987B1 (en) Cylinder element, nickel-based alloy and application of the alloy
US10267167B2 (en) Ductile compensation layer for brittle components
JP2008180211A (en) Manufacturing method for combustion engine or turbine parts
JPH0441682A (en) Suction and exhaust valve for internal-combustion engine made of titanium aluminide
CA2146534A1 (en) Heat-resistant nickel-based alloy excellent in weldability
CN114574740A (en) Aluminum alloy for casting and additive manufacturing of engine components for high temperature applications
RU96118497A (en) VALVE NOZZLE FOR INLET OF FUEL AND METHOD FOR ITS MANUFACTURE
JPS6253583B2 (en)
CA1198612A (en) Nickel base superalloy
FI89463C (en) ANVAENDNING AV EN NICKELBASERAD, ALUMINIUM INNEHAOLLANDE METALLEGERING SOM SUBSTRATMATERIAL FOER EN AVGASER RENANDE KATALYSATOR
RU2070601C1 (en) Refractory alloy on the base of nickel
JPH06256908A (en) Heat resistant cast steel and exhaust system parts using the same
JPH02213438A (en) Nickel-aluminum alloy
JPH06297188A (en) Fe-based alloy for overlay
JPH08501349A (en) Reinforcement material for pistons of internal combustion engines
JP2542778B2 (en) Exhaust system parts
JPH08311585A (en) Titanium aluminide for precision casting containing Fe and V
RU2751039C1 (en) Alloy with high oxidation resistance and gas turbine applications using this alloy