WO1998018972A1 - Superalliage a base de nickel contenant de l'iridium - Google Patents
Superalliage a base de nickel contenant de l'iridium Download PDFInfo
- Publication number
- WO1998018972A1 WO1998018972A1 PCT/JP1997/003911 JP9703911W WO9818972A1 WO 1998018972 A1 WO1998018972 A1 WO 1998018972A1 JP 9703911 W JP9703911 W JP 9703911W WO 9818972 A1 WO9818972 A1 WO 9818972A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- iridium
- added
- temperature
- base superalloy
- tms
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
Definitions
- the present invention relates to an iridium-added Ni-base superalloy. More specifically, the present invention relates to the output of high-temperature equipment such as a gas turbine for power generation, a jet engine, a rocket engine, and the like. The present invention relates to a Ni-based super heat-resistant alloy added with a zirconia, which is effective for improving the efficiency and efficiency.
- Background art
- Ni-base superalloy has Ni as a basic constituent element and Co, Cr, Mo, W, AI, Ti, Ta, Nb, Re, Hf, etc. as main constituent elements. It is an alloy that contains
- This Ni-based super heat-resistant alloy has excellent high-temperature strength, and is also suitable for gas turbines for power generation, jet engines, and rocket engines. It is used for high temperature equipment such as turbine blades and turbine vanes, which are used under high temperature and high stress. Raising the combustion gas temperature is the most effective way to increase the output and efficiency of these high-temperature devices, but N-base super-heat-resistant alloys are the most effective way to achieve this. Improving the characteristics of these devices is urgently needed.
- Performance improvement must be considered from two perspectives. One is high temperature strength and the other is hot corrosion resistant.
- Ni-base superalloys for example, For example, addition of W, Mo, Ta, Re, etc. has been attempted. However, when the addition of these elements is large, the alloy structure becomes unstable and the harmful phase is precipitated when the addition amount is large, and the strength of the Ni-based superalloy is reversed. Has been confirmed to decrease.
- Improvement of high-temperature corrosion resistance is an important issue in high-temperature equipment because components used under high temperatures and high stresses are used in highly corrosive atmospheres.
- turbine blades of gas turbines are used in a highly oxidizing atmosphere of combustion gas, and also contain fuel in fuel.
- thermal power plants are generally located near the coast, there is an additional condition that a large amount of salt may be mixed in the combustion air.
- Dependence of the improvement of high-temperature corrosion resistance of components used in such severe corrosive atmosphere only on coatings with good corrosion resistance is a problem with coatings. It is dangerous unless the layer is not broken. It is more certain to improve the high-temperature corrosion resistance of the Ni-base superalloy itself.
- an object of the present invention is to provide an N-based super heat-resistant alloy having excellent high-temperature strength and high-temperature corrosion resistance. Disclosure of invention
- This invention adds iridium having a high melting point to a Ni-based super-heat-resistant alloy to provide a Ni-based super-heat-resistant alloy having excellent high-temperature strength and high-temperature corrosion resistance. provide.
- Iridium When iridium (Ir) is added, the alloy structure is aligned, the structure stability is kept good, and the precipitation strengthening is promoted. At the same time, iridium dissolves in the r phase and the r 'phase, and the solid solution strengthens. Iridium has the same face-centered cubic structure as Ni, and therefore can be easily replaced with Ni. Conventionally, W, Mo, Ta, etc., which have been added elements, have a body-centered cubic structure, and Re, etc., have a dense hexagonal structure, which reduces tissue stability. It is thought that this was one of the causes.
- the iridium-added Ni-based super heat-resistant alloy has excellent high-temperature strength and can be used under high temperature and high stress.
- iridium has a high melting point and a low diffusion coefficient even at high temperatures. As a result, characteristic deterioration of the Ni-based super heat-resistant alloy is suppressed, and high-temperature corrosion resistance is improved.
- Such an amount of addition of at least 0.1 atomic% is necessary for sufficient improvement in high-temperature strength and high-temperature corrosion resistance to be recognized.
- the upper limit is not particularly strict and can be appropriately adjusted according to the use of the Ni-based superalloy.
- an increase in the addition amount of 5 atomic% reflects the increase in the specific gravity and the price.
- the addition amount of iridium is preferably in the range of 0.1 atom ⁇ 1 ⁇ 2 to 5 atom ⁇ 1 ⁇ 2.
- N ⁇ -base superalloys can be used.
- Figure 1 is a graph showing the relationship between the 0.2% compressive strength of a Ni-base superalloy and the amount of iridium added.
- Fig. 2 (a) and (b) show the alloy structures of TMS-63 and Ni-based super-heat-resistant alloy in which 2 atomic% of iridium is added to TMS-63, respectively. This is a micrograph taken.
- Fig. 3 shows the creep test results of TMS-63 and Ni-base superalloy with 1.5 atom 0 / o iridium added to TMS-63. Time) One strain (%) curve.
- Fig. 4 is a graph showing the correlation between the immersion time of TMS-63 and TMS-63 with the addition of iridium and the corrosion depth from the surface. Best mode for carrying out the invention
- Ni-based super heat-resistant alloy TMS — 63 (6.9 Cr-7.5 Mo-5.8 AI-8.4 Ta-residual Ni (wt%)) with 1 atomic% and 2 atomic%
- the iridium was added by the arc dissolution method.
- the alloy structure may be more ordered. It is confirmed . This strengthens the precipitation and strengthening of the aligned alloy structure.
- the base material is the r phase, and the r 'phase is shown as a black cubic crystal.
- the added iridium forms a solid solution in the r phase and the r 'phase, and solid solution strengthens.
- the solid With the addition of 2 atomic%, the solid forms a solid solution at a concentration ratio of 2: 1 at 870 ° C in the r and r 'phases.
- Ni-based super heat-resistant alloys The service temperature of Ni-based super heat-resistant alloys is about 1100 ° C. The strength properties are improved, and the tissue stability is excellent.
- a single crystal alloy was prepared by adding 1.5 atomic% of iridium to the Ni-based super heat-resistant alloy TMS-63 by a vacuum melting method.
- the composition of this iridium-added Ni-base superalloy is expressed in terms of% by weight as 6.5 Cr — 7.1 Mo-5.5 AI-7.9 Ta-5.7 Ir — Indicated as Remaining N i.
- High temperature strength was evaluated by creep test.
- the test conditions are The air pressure was 900 ° C and the stress was 40 kgf / mm 2 .
- the graph in Fig. 3 shows the results.
- Fig. 4 shows the correlation between the immersion time of TMS-63 and the immersion time of TMS-63 in TMS-63 and the corrosion depth from the surface, and the addition of iridium.
- the Ni-based super-heat-resistant alloy even if immersion was carried out for 20 hours, only a small amount of oxidation was observed to form a thin oxide film on the surface.
- TMS-63 corrosion in the center progressed after only 5 hours of immersion. This type of corrosion was also observed in Mar M — 24 7, and the corrosion pattern was similar to that of TMS — 63.
- a stable Provided is a practically useful iridium-added Ni-based super heat-resistant alloy having an alloy structure and having improved high-temperature strength and high-temperature corrosion resistance, which is extremely useful in practical use.
- This iridium-added Ni-base superalloy can be used to produce gas turbines for power generation, turbine engines such as jet engines and rocket engines.
- turbine engines such as jet engines and rocket engines.
- the output and efficiency of high temperature equipment can be reduced. We can expect improvement.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP97909659A EP0959143A1 (en) | 1996-10-28 | 1997-10-28 | Iridium-containing nickel-base superalloy |
US09/297,041 US6494971B1 (en) | 1996-10-28 | 1997-10-28 | Iridium-containing nickel-base superalloy |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8/285119 | 1996-10-28 | ||
JP28511996 | 1996-10-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1998018972A1 true WO1998018972A1 (fr) | 1998-05-07 |
Family
ID=17687370
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP1997/003911 WO1998018972A1 (fr) | 1996-10-28 | 1997-10-28 | Superalliage a base de nickel contenant de l'iridium |
Country Status (3)
Country | Link |
---|---|
US (1) | US6494971B1 (ja) |
EP (1) | EP0959143A1 (ja) |
WO (1) | WO1998018972A1 (ja) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060039820A1 (en) * | 2004-08-20 | 2006-02-23 | General Electric Company | Stable, high-temperature nickel-base superalloy and single-crystal articles utilizing the superalloy |
US20090035632A1 (en) * | 2007-07-31 | 2009-02-05 | Kirkwood Brad L | Solid oxide fuel cell electrode systems and methods |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5735258B2 (ja) * | 1974-07-08 | 1982-07-28 | ||
JPH058263B2 (ja) * | 1985-06-10 | 1993-02-01 | Yunaitetsudo Tekunorojiizu Corp |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2862157D1 (en) * | 1977-12-05 | 1983-02-17 | Secr Defence Brit | Improvements in or relating to nickel-, cobalt-, and iron based alloys |
GB2033925B (en) * | 1978-09-25 | 1983-07-20 | Johnson Matthey Co Ltd | Nickel based superalloys |
US4261742A (en) * | 1978-09-25 | 1981-04-14 | Johnson, Matthey & Co., Limited | Platinum group metal-containing alloys |
DE3689059T2 (de) * | 1985-08-02 | 1994-04-21 | Daiki Engineering Co | Oberflächenaktivierte amorphe Legierungen und übersättigte Legierungen für Elektroden, verwendbar zur Elektrolyse von Lösungen und Verfahren zur Aktivierung der Oberflächen. |
JPH054046A (ja) * | 1990-08-06 | 1993-01-14 | Sumitomo Metal Ind Ltd | 排ガス浄化用の低温作動型三元触媒 |
-
1997
- 1997-10-28 US US09/297,041 patent/US6494971B1/en not_active Expired - Lifetime
- 1997-10-28 EP EP97909659A patent/EP0959143A1/en not_active Withdrawn
- 1997-10-28 WO PCT/JP1997/003911 patent/WO1998018972A1/ja not_active Application Discontinuation
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5735258B2 (ja) * | 1974-07-08 | 1982-07-28 | ||
JPH058263B2 (ja) * | 1985-06-10 | 1993-02-01 | Yunaitetsudo Tekunorojiizu Corp |
Also Published As
Publication number | Publication date |
---|---|
EP0959143A1 (en) | 1999-11-24 |
US6494971B1 (en) | 2002-12-17 |
EP0959143A4 (ja) | 1999-12-01 |
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