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Inconel is a registered trademark of Special Metals Corporation for a family of austenitic nickel-chromium-based superalloys.[1]

Inconel 718 round bar
Inconel 718 round bar

Inconel alloys are oxidation-corrosion-resistant materials well suited for service in extreme environments subjected to pressure and heat. When heated, Inconel forms a thick, stable, passivating oxide layer protecting the surface from further attack. Inconel retains strength over a wide temperature range, attractive for high-temperature applications where aluminium and steel would succumb to creep as a result of thermally-induced crystal vacancies. Inconel's high-temperature strength is developed by solid solution strengthening or precipitation hardening, depending on the alloy.[2][3]

Inconel alloys are typically used in high temperature applications. Common trade names for


History


The Inconel family of alloys was first developed before December 1932, when its trademark was registered by the International Nickel Company of Delaware and New York.[6][7] A significant early use was found in support of the development of the Whittle jet engine,[8] during the 1940s by research teams at Henry Wiggin & Co of Hereford, England a subsidiary of the Mond Nickel Company,[9] which merged with Inco in 1928. The Hereford Works and its properties including the Inconel trademark were acquired in 1998 by Special Metals Corporation.[10]


Specific data


Alloy Solidus °C (°F) Liquidus °C (°F)
Inconel 600[11] 1354 (2,469) 1413 (2,575)
Inconel 617[12][13] 1332 (2,430) 1377 (2,511)
Inconel 625[14] 1290 (2,350) 1350 (2,460)
Inconel 690[15] 1343 (2,449) 1377 (2,511)
Inconel 718[16] 1260 (2,300) 1336 (2,437)
Inconel X-750[17] 1390 (2,530) 1430 (2,610)

Composition


Inconel alloys vary widely in their compositions, but all are predominantly nickel, with chromium as the second element.

Inconel Element, proportion by mass (%)
Ni Cr Fe Mo Nb & Ta Co Mn Cu Al Ti Si C S P B
600[18] ≥72.0[lower-alpha 1] 14.0–17.0 6.0–10.0 ≤1.0 ≤0.5 ≤0.5 ≤0.15 ≤0.015
617[19] 44.2–61.0 20.0–24.0 ≤3.0 8.0–10.0 10.0–15.0 ≤0.5 ≤0.5 0.8–1.5 ≤0.6 ≤0.5 0.05–0.15 ≤0.015 ≤0.015 ≤0.006
625[20] ≥58.0 20.0–23.0 ≤5.0 8.0–10.0 3.15–4.15 ≤1.0 ≤0.5 ≤0.4 ≤0.4 ≤0.5 ≤0.1 ≤0.015 ≤0.015
690[21] ≥58 27–31 7–11 ≤0.50 ≤0.50 ≤0.50 ≤0.05 ≤0.015
Nuclear grade 690[21] ≥58 28–31 7–11 ≤0.10 ≤0.50 ≤0.50 ≤0.50 ≤0.04 ≤0.015
718[2] 50.0–55.0 17.0–21.0 Balance 2.8–3.3 4.75–5.5 ≤1.0 ≤0.35 ≤0.3 0.2–0.8 0.65–1.15 ≤0.35 ≤0.08 ≤0.015 ≤0.015 ≤0.006
X-750[22] ≥70.0 14.0–17.0 5.0–9.0 0.7–1.2 ≤1.0 ≤1.0 ≤0.5 0.4–1.0 2.25–2.75 ≤0.5 ≤0.08 ≤0.01
  1. Includes cobalt

Properties


Inconel alloys are oxidation- and corrosion-resistant materials well suited for service in extreme environments subjected to high mechanical loads. When heated, Inconel forms a thick and stable passivating oxide layer protecting the surface from further attack. Inconel retains strength over a wide temperature range, attractive for high-temperature applications where aluminium and steel would succumb to creep as a result of thermally induced crystal vacancies (see Arrhenius equation). Inconel's high temperature strength is developed by solid solution strengthening or precipitation strengthening, depending on the alloy. In age-hardening or precipitation-strengthening varieties, small amounts of niobium combine with nickel to form the intermetallic compound Ni3Nb or gamma double prime (γ″). Gamma prime forms small cubic crystals that inhibit slip and creep effectively at elevated temperatures. The formation of gamma-prime crystals increases over time, especially after three hours of a heat exposure of 850 °C (1,560 °F), and continues to grow after 72 hours of exposure.[23]


Machining


Inconel is a difficult metal to shape and to machine using traditional cold forming techniques due to rapid work hardening. After the first machining pass, work hardening tends to plastically deform either the workpiece or the tool on subsequent passes. For this reason, age-hardened Inconels such as 718 are typically machined using an aggressive but slow cut with a hard tool, minimizing the number of passes required. Alternatively, the majority of the machining can be performed with the workpiece in a "solutionized" form,[clarification needed] with only the final steps being performed after age hardening. However some claim[by whom?] that Inconel can be machined extremely quickly with very fast spindle speeds using a multifluted ceramic tool with small depth of cut at high feed rates as this causes localised heating and softening in front of the flute.

External threads are machined using a lathe to "single-point" the threads or by rolling the threads in the solution treated condition (for hardenable alloys) using a screw machine. Inconel 718 can also be roll-threaded after full aging by using induction heat to 700 °C (1,290 °F) without increasing the grain size.[citation needed] Holes with internal threads are made by threadmilling. Internal threads can also be formed using a sinker electrical discharge machining (EDM).[citation needed]

More often than machining, water-jet or laser grinding is a preferred and economical method for forming nickel alloy components to shape and finish. Due to the hardness of the abrasives used, the grinding wheels are not as affected by the material work hardening and remain sharp and durable.


Joining


Welding of some Inconel alloys (especially the gamma prime precipitation hardened family; e.g., Waspalloy and X-750) can be difficult due to cracking and microstructural segregation of alloying elements in the heat-affected zone. However, several alloys such as 625 and 718 have been designed to overcome these problems. The most common welding methods are gas tungsten arc welding and electron-beam welding.[24]


Uses


Astra rocket engine
Astra rocket engine

Inconel is often encountered in extreme environments. It is common in gas turbine blades, seals, and combustors, as well as turbocharger rotors and seals, electric submersible well pump motor shafts, high temperature fasteners, chemical processing and pressure vessels, heat exchanger tubing, steam generators and core components in nuclear pressurized water reactors,[25] natural gas processing with contaminants such as H2S and CO2, firearm sound suppressor blast baffles, and Formula One, NASCAR, NHRA, and APR, LLC exhaust systems.[26][27] It is also used in the turbo system of the 3rd generation Mazda RX7, and the exhaust systems of high powered Wankel engined Norton motorcycles where exhaust temperatures reach more than 1,000 °C (1,830 °F).[28] Inconel is increasingly used in the boilers of waste incinerators.[29] The Joint European Torus and DIII-D tokamaks' vacuum vessels are made of Inconel.[30] Inconel 718 is commonly used for cryogenic storage tanks, downhole shafts, wellhead parts,[31] and in the aerospace industry -- where it has become a prime candidate material for constructing heat resistant turbines.[32]


Aerospace



Automotive


Rolled Inconel was frequently used as the recording medium by engraving in black box recorders on aircraft.[51]

Alternatives to the use of Inconel in chemical applications such as scrubbers, columns, reactors, and pipes are Hastelloy, perfluoroalkoxy (PFA) lined carbon steel or fiber reinforced plastic.


Inconel alloys


Alloys of inconel include:

In age hardening or precipitation strengthening varieties, alloying additions of aluminum and titanium combine with nickel to form the intermetallic compound Ni3(Ti,Al) or gamma prime (γ′). Gamma prime forms small cubic crystals that inhibit slip and creep effectively at elevated temperatures.


See also



References


  1. "High-Performance Alloys". Special Metals Corporation. Archived from the original on 2012-12-08. Retrieved 2010-04-26.
  2. INCONEL alloy 718, Special Metals Corporation
  3. "Archived copy". Archived from the original on 2015-09-02. Retrieved 2015-09-16.{{cite web}}: CS1 maint: archived copy as title (link)
  4. "Special Alloys: Inconel 625". Archived from the original on 2009-06-05. Retrieved 2010-04-26.
  5. "Alloy 600 Inconel 600". Retrieved 2018-06-30.
  6. "Word Mark : INCONEL". United States Patent and Trademark Office. Trademark Electronic Search System (TESS).
  7. Monel, Inconel, Nickel, and Nickel Alloys. Development and Research Division: International Nickel Company. 1947.
  8. Jones, T.L. "Frank Whittle's W2B Turbojet: United Kingdom versus United States Development". EngineHistory.org. Aircraft Engine Historical Society, Inc. Archived from the original on 30 March 2016. Retrieved 27 March 2016.
  9. Annual Report on the Mineral Production of Canada. Canada. Dominion Bureau of Statistics. 1932. p. 88.
  10. "Special Metals Corporation: History". Archived from the original on April 21, 2008. Retrieved 2012-05-18.
  11. "ASM Material Data Sheet".
  12. "Inconel 617 Alloy | AMERICAN ELEMENTS ®".
  13. "ASM Material Data Sheet".
  14. "Inconel 625 Alloy | AMERICAN ELEMENTS ®".
  15. "Inconel 690 Alloy | AMERICAN ELEMENTS ®".
  16. "Inconel 718 Alloy | AMERICAN ELEMENTS ®".
  17. "ASM Material Data Sheet".
  18. INCONEL alloy 600, Special Metals Corporation
  19. hightempmetals.com, High Temp Metals
  20. INCONEL alloy 625, Special Metals Corporation
  21. Inconel alloy 690, Special Metals Corporation
  22. INCONEL alloy X-750, Special Metals Corporation
  23. "DoITPoMS - Full Record". www.doitpoms.ac.uk.
  24. Joining (PDF), retrieved 2009-10-09.
  25. "Inconel alloy 625, Specials Metals, 2015" (PDF). Archived from the original (PDF) on 2009-02-26.
  26. Power Generation Archived 2012-09-14 at archive.today, Special Metals Corporation.
  27. Chemical Processing Archived 2013-02-02 at archive.today, Special Metals Corporation.
  28. Motorcycle Trader.Norton Rotary Revival.Cathcart.Dec 2007.
  29. Inconell – state-of-the-art corrosion protection Archived 2008-11-15 at the Wayback Machine by Babcock & Wilcox Vølund, 2003
  30. The Inconel JET vessel in use since 1983 Archived 2010-02-27 at the Wayback Machine. A simple, sturdy structure.
  31. Inconel Alloy, Inconel 718.
  32. "What are the applications for Inconel 718?". Langley Alloys. Retrieved 2022-03-23.
  33. Robert S. Houston, Richard P. Hallion, and Ronald G. Boston, EDITOR'S INTRODUCTION, "Transiting from Air to Space: The North American X-15", The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology, Air Force History and Museums Program, 1998. NASA.gov.
  34. Anthony Young, "The Saturn V Booster: Powering Apollo into History", Springer-Verlag, 2009.
  35. HISTORY OF INCONEL AND SUPERALLOYS
  36. >"Space Launch Report: SpaceX Falcon 9 Data Sheet". 1 May 2017. Archived from the original on 6 Apr 2022.
  37. "Elon Musk's recent "Ludicrous" announcement hints at more synergy between Tesla and SpaceX - Electrek". Electrek. Archived from the original on 12 September 2015.
  38. Norris, Guy (2014-05-30). "SpaceX Unveils 'Step Change' Dragon 'V2'". Aviation Week. Archived from the original on 2014-05-31. Retrieved 2014-05-30.
  39. Kramer, Miriam (2014-05-30). "SpaceX Unveils Dragon V2 Spaceship, a Manned Space Taxi for Astronauts — Meet Dragon V2: SpaceX's Manned Space Taxi for Astronaut Trips". space.com. Retrieved 2014-05-30.
  40. Bergin, Chris (2014-05-30). "SpaceX lifts the lid on the Dragon V2 crew spacecraft". NASAspaceflight.com. Retrieved 2015-03-06.
  41. Foust, Jeff (2014-05-30). "SpaceX unveils its "21st century spaceship"". NewSpace Journal. Retrieved 2015-03-06.
  42. "SpaceX Launches 3D-Printed Part to Space, Creates Printed Engine Chamber for Crewed Spaceflight". SpaceX. Archived from the original on 2017-08-25. Retrieved 2015-03-06. Compared with a traditionally cast part, a printed [part] has superior strength, ductility, and fracture resistance, with a lower variability in materials properties. ... The chamber is regeneratively cooled and printed in Inconel, a high performance superalloy. Printing the chamber resulted in an order of magnitude reduction in lead-time compared with traditional machining – the path from the initial concept to the first hotfire was just over three months. During the hotfire test, ... the SuperDraco engine was fired in both a launch escape profile and a landing burn profile, successfully throttling between 20% and 100% thrust levels. To date the chamber has been fired more than 80 times, with more than 300 seconds of hot fire.
  43. SpaceX Casting Raptor Engine Parts from Supersteel Alloys Feb 2019
  44. "Three Dog Day". www.teslamotors.com.
  45. "New Ford EcoBlue turbodiesel engine debuts amid diesel woes". Autoblog.com. April 26, 2016.
  46. J. Smith, Evan (22 March 2020). "Piping for Power: How to choose the best headers for your combination". NHRA. Retrieved 9 August 2022.
  47. "Inside a 7-second Ford Barra street car | fullBOOST". YouTube. 2021-05-09. Archived from the original on 2021-12-12.
  48. Shard, Abhinav; Deepshikha; Gupta, Vishal; Garg, M P (2021). "The Comprehensive Review on machining of Inconel 718 superalloy". IOP Conference Series: Materials Science and Engineering. 1033 (1): 012069. Bibcode:2021MS&E.1033a2069S. doi:10.1088/1757-899X/1033/1/012069. S2CID 234133836.
  49. "Jaguar Introduces Ultra-High Performance F-TYPE SVR Ahead Of Geneva Debut". www.jaguarusa.com.
  50. "Trailing Arm Bolts". www.delorean.com.
  51. Barrett, Brian (10 January 2011). "The Secret Sauce of an Airplane's Black Box".
  52. "Inconel alloy 617" (PDF). March 2005. Retrieved 14 July 2022.
  53. "COMMERCIAL ALLOY QUALIFIED FOR NEW USE, EXPANDING NUCLEAR OPERATING TEMPERATURE". U.S. Department of Energy Idaho National Laboratory. April 28, 2020.
  54. INCONEL alloy 690 Archived 2013-11-12 at the Wayback Machine, NDT Resource Center
  55. "DMLS in Aluminum, Inconel or Titanium - Is it worth it? - Blog". gpiprototype.com.
  56. INCONEL alloy 751, Special Metals Corporation
  57. Vishal Kumar Jaiswal "Experimental Investigation of Process Parameters on Inconel 925 for EDM Process by using Taguchi Method." International Journal for Scientific Research and Development 6.5 (2018): 277-282. , IJSRD



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