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Brass Sheets and Plates
Content:
↬ Brass Sheets and Plates Specification
↬ Brass Sheets and Plates Chemical Composition
↬ Brass Sheets and Plates Packaging Policy
↬ Brass Sheets and Plates Application
↬ Why Choose Nido Metals?
↬ Brass Sheets and Plates Inventery
Synonymous with quality and reliability, Nido Metals is a renowned Manufacturer, Exporter & Suppliers of Brass Sheets and Plates. Our management has been the key to our success as we delegates responsibility to the specific need of every customers and we have made every customer a member of our family.We have lage global Network in the countries like Qatar, Saudi Arabia, UAE, Singapore, Australia & South Africa.
We offer the best quality Brass Sheets and Plates which are used widely and are demanded all over.Our sophisticated machineries and talented workforce assist us in manufacturing products exactly according to the requirements of the customers. Brass Sheets and Plates are available in various sizes and shapes and can be customized as per the requirement of our clients.We strive to scale a new height in the industry by satisfying our customers with innovative range of quality products. When it comes to Brass Sheets and Plates, Nido Metals is the name that came into mind.We continuously bring improvements and think of new ways to make our products better. Our qualitative products and dedicated prompt services speak volumes about our commitment towards complete customer satisfaction.In Brass Sheets and Plates we are one of the leading Exporter & Suppliers in Worldwide. We have a extensive sales network in Qatar, Saudi Arabia, U.A.E, Singapore, Tanzania, South Africa.
Brass Sheets and Plates Specification
Type: Brass Sheets and Plates.
Stocking 220 and 260 sheet in 36" x 96" standard dimension.
Thickness :.020" through 2.000" .
Special cut sizes and blanks available.
Polish and plate quality available.
| Thickness In. | Width In. |
Lbs. Per Sq. Ft. | Lbs. Per Sheet |
|---|---|---|---|
| (.020) | 36 | .886 | 21.2 |
| (.025) | 36 | 1.12 | 26.8 |
| (.032) | 36 | 1.41 | 33.8 |
| (.040) | 36 | 1.78 | 42.7 |
| (.051) | 36 | 2.25 | 54.0 |
| (.064) | 36 | 2.82 | 67.6 |
| (.081) | 36 | 3.56 | 85.4 |
| (.091) | 36 | 4.00 | 96.0 |
| 1/8 (.125) | 36 | 5.51 | 132.2 |
| Thickness In. | Width In. |
Lbs. Per Sq. Ft. |
Lbs. Per Sheet |
|---|---|---|---|
| 3/16 | (.187) | 36 | 8.26 |
| 1/4 (.250) | 36 | 11.1 | 266 |
| 3/8 (.375) | 36 | 16.6 | 399 |
| 1/2 (.500) | 36 | 22.2 | 532 |
| 5/8 (.625) | 36 | 27.7 | 665 |
| 3/4 (.750) | 36 | 33.3 | 798 |
| 1 (1.000) | 36 | 44.4 | 1065 |
| 1 1/2 (1.500) | 36 | 66.5 | 1596 |
| 2 (2.000) | 36 | 88.7 | 2129 |
Brass Sheets and Plates Chemical Composition
| Brass Sheet Supercedes BS 2870. |
||||
| BS | ISO | EN | Description & Uses | |
| CZ101 | Cu Zn 10 | CW501L | Gilding metal used for architectural metalwork, imitation jewellery etc. | |
| CZ106 | Cu Zn 30 | CW505L | 70/30 Brass. Deep drawing and spinning quality. | |
| CZ108 | Cu Zn 37 | CW508L | “Common” Brass, a general purpose alloy suitable for simple forming etc. | |
ASTM / ASME SB 163 UNS 2200 ( NICKEL 200 )
ASTM / ASME SB 163 UNS 2201 (NICKEL 201 )
ASTM / ASME SB 163 / 165 UNS 4400 (MONEL 400 )
ASTM / ASME SB 464 UNS 8020 ( ALLOY 20 / 20 CB 3 )
ASTM / ASME SB 704/705 UNS 8825 INCONEL (825)
ASTM / ASME SB 167 / 517 UNS 6600 (INCONEL 600 )
ASTM / ASME SB 167 UNS 6601 ( INCONEL 601 )
ASTM / ASME SB 704 /705 UNS 6625 (INCONEL 625)
ASTM / ASME SB 619/622/626UNS 10276 ( HASTELLOY C 276 )
| International Specifications | Nickel 200 Sheet / Plate | Nickel 200 Round Bar | Nickel 200 Pipe | Nickel 200 Tube | Nickel 200 Fittings | Nickel 200 Forgings |
| BS 3072, BS 3073, BS 3074, BS 3075, BS 3076, NA11 DIN 17740,17750, 17751,17752, 17753, 17754. Werkstoff Nr. 2.4060, 2.4066 |
ASME SB-168 | ASME SB-160 | ASME SB-161 ASME S B-829 ASME SB-775 ASME SB-725 | ASME SB-161 ASME SB-163 ASME SB-730 ASME SB-751 | ASME SB-366 | ASME SB-564 |
| Seamless Pipes / Tubes | ASTM-B-161/163 |
| Welded Pipes / Tubes | ASTM-B-725/730 |
| Plates/Sheets | ASTM-B-162 |
| Bars | ATM-B-160 |
Standard for Nickel 200/201
| Alloy Designation | UNS | BS | EN | Basic | DIN | JIS | Trade Name | ASTM |
| Nickel 200 | N02200 | 3074 / NA 11 | 2.4066 | Pure Ni | Ni99.2 | NW2200 (JIS H4552) | B163 | |
| Nickel 201 | N02201 | 3074 / NA 12 | 2.4068 | Pure Ni-Low C | LC-Ni99 | NW2201 (JIS H4552) | B163 |
| MATL | UNS | g/cm | PIPE | TUBE | Plate~ | RND | Forging | Fitting | |||
| NO. | SMLS | Welded | SMLS | Welded | Strip | BAR | |||||
| H A S T E L L O Y |
Hastelloy B-2 | N10665 | 9.22 | B622 | B619 | B622 | B626 | B333 | B335 | B564 | B366-WPHB2 |
| Hastelloy C-276 | N10276 | 8.89 | B622 | B619 | B622 | B626 | B575 | B574 | B564 | B366-WPHC276 | |
| Hastelloy C-4 | N06455 | 8.64 | B622 | B619 | B622 | B626 | B575 | B574 | B564 | B366-WPHC4 | |
| Hastelloy C-22 | N06022 | 8.69 | B622 | B619 | B622 | B626 | B575 | B574 | B564 | B366-WPHC22 | |
| Hastelloy G | N06007 | 8.3 | B622 | B619 | B622 | B626 | B582 | B581 | B564 | B366-WPHG | |
| Hastelloy G-3 | N06985 | 8.3 | B622 | B619 | B622 | B626 | B582 | B581 | B564 | B366-WPHG3 | |
| Hastelloy G-30 | N06030 | 8.22 | B622 | B619 | B622 | B626 | B582 | B581 | B564 | B366-WPHG30 | |
| Hastelloy X | N06002 | 8.22 | B622 | B619 | B622 | B626 | B435 | B572 | B564 | B366-WPHX | |
| M O N E L |
Monel 400 | N04400 | 8.83 | B165 | B725-EFW | B163 | - | B127 | B164 | B564 | B366-WPNC |
| Monel R-405 | N04405 | 8.83 | - | - | - | - | - | B164 | - | - | |
| Monel K-500 | N05500 | 8.46 | - | - | - | - | - | - | - | - | |
| I N C O L O Y |
Inconel 60 | N06600 | 8.42 | B167 | B517 | B163 | B516 | B168 | B166 | B564 | B366-WPNCI |
| Inconel 601 | N06601 | 8.06 | - | - | - | - | - | - | - | - | |
| Inconel 617 | N06617 | 8.36 | - | - | - | - | - | - | - | - | |
| Inconel 625 | N06625 | 8.44 | B444 | B705 | B444 | B704 | B443 | B446 | - | - | |
| Inconel 690 | N06690 | 8.19 | B167 | - | B163 | - | B168 | B166 | - | - | |
| Inconel 718 | N07718 | 8.19 | - | - | - | - | B670 | B637 | B637 | - | |
| Inconel X-750 | N07750 | 8.25 | - | - | - | - | - | B637 | B637 | - | |
| I N C O L O Y |
Incoloy 800 | N08800 | 7.95 | B407 | B514 | B163 | B515 | B409 | B408 | B564 | B366-WPNIC |
| Incoloy 800H | N08810 | 7.95 | B407 | B514 | B163 | B515 | B409 | B408 | B564 | B366-WPNIC10 | |
| Incoloy 800HT | N08811 | 7.95 | B407 | B514 | B163 | B515 | B409 | B408 | B564 | B366-WPNIC11 | |
| Incoloy 825 | N08825 | 8.14 | B432 | B705 | B163 | B704 | B424 | B425 | - | B366-WPNICMC | |
| Nickel 200 | N02200 | 8.89 | B161 | B725 | B163 | B730 | B162 | B160 | - | B366-WPN | |
| Nickel 201 | N02201 | 8.89 | B161 | B725 | B163 | B730 | B162 | B160 | - | B366-WPNL | |
| ALLOY 20 | N08020 | 8.00 | B729 | B464 | B729 | B468 | B463 | B473 | B462 | B366-WP20CB | |
| TITANIUM (Ti) | 4.51 | B337 | B337 | B338 | B338 | B265 | B348 | B381 | B363-WPT(Gr) | ||
| ZIRCONIUM (Zr) | 6.51 | B658 | B658 | B523 | B523 | B551 | B550 | B493 | B653-PZ(Gr) | ||
| TANTALUM (Ta) | 16.66 | - | - | B521 | B521 | B708 | B365 | - | - | ||
| Cu-Ni 70/30(C71500) | 8.94 | B466 | B467 | B111 | B543 | B171 | B151 | - | - | ||
| Cu-Ni 90/10(C70600) | 8.91 | B466 | B467 | B111 | 543 | B171 | B151 | - | - | ||
| Duplex2205(S31803) | 7.83 | A790 | A790 | A789 | A789 | A240 | A276 | A182-F51 | A815 | ||
| 904L (N08904) | 8.05 | B677 | B673 | B677 | B674 | B625 | B649 | - | - | ||
Duplex Pipes & Tubes
Standard for Duplex
| Alloy Designation | UNS | BS | EN | Basic | DIN | JIS | Trade Name | ASTM |
| Alloy 2205 | S31803 | 1.4462 | 22Cr-5Ni-3Mo-0.15N | X2CrNiMoN22-5-3 | SUS329L3L (JIS G3463) | SAF 2205 22Cr | ||
| Alloy 2205 | S32205 | 1.4462 | 22.5Cr-6Ni-3Mo-0.2N | SAF 2205 22Cr | A789 |
Super Duplex Pipes & Tubes
| Alloy Designation | UNS | BS | EN | Basic | DIN | JIS | Trade Name | ASTM |
| Alloy 2205 | S32750 S32760 | 1.4410 | 25Cr-7Ni-4Mo-0.3N | SAF 2507 | A789 |
Inconel Pipes & Tubes
Inconel 600, UNS N06600, 3074 / NA 14, 2.4816, NiCr 15 Fe, 15Cr-8Fe-Ni, B163,NCF600(JISG4904)
Inconel 600 is a nickel-chromium alloy used for applications that require corrosion and high temperature resistance. This nickel alloy was designed for service temperatures from cryogenic to elevated temperatures in the range of 2000° F. It is non-magnetic, has excellent mechanical properties, and presents the desirable combination of high strength and good weldability under a wide range of temperatures. The high nickel content in Inconel 600 enables it to retain considerable resistance under reducing conditions, makes it resistant to corrosion by a number of organic and inorganic compounds, gives it excellent resistance to chloride-ion stress-corrosion cracking and also provides excellent resistance to alkaline solutions. Typical applications of this nickel alloy include the chemical, pulp and paper, aerospace, nuclear engineering and heat treating industries.
Inconel 600 is a nickel-chromium alloy used for applications that require corrosion and high temperature resistance. This nickel alloy was designed for service temperatures from cryogenic to elevated temperatures in the range of 2000° F. It is non-magnetic, has excellent mechanical properties, and presents the desirable combination of high strength and good weldability under a wide range of temperatures. The high nickel content in Inconel 600 enables it to retain considerable resistance under reducing conditions, makes it resistant to corrosion by a number of organic and inorganic compounds, gives it excellent resistance to chloride-ion stress-corrosion cracking and also provides excellent resistance to alkaline solutions. Typical applications of this nickel alloy include the chemical, pulp and paper, aerospace, nuclear engineering and heat treating industries.
Inconel 601, UNS N06601, 2.4851, NiCr 23 Fe, 23Cr-1.4Al-Ni, B163
Inconel 601 is a nickel-chromium alloy used for applications that require resistance to corrosion and heat. This nickel alloy stands out due to its resistance to high temperature oxidation, remaining highly resistant to oxidation through 2200° F. Alloy 601 develops a tightly adherent oxide scale which resists spalling even under conditions of severe thermal cycling. This nickel alloy has good high temperature strength, and retains its ductility after long service exposure. It has good resistance to aqueous corrosion, high mechanical strength, and is readily formed, machined and welded. Inconel 601’s properties make it a material of broad utility in fields like thermal processing, chemical processing, pollution control, aerospace, and power generation. However, alloy 601 is not suggested for use in strongly reducing, sulfur bearing environments.
Inconel 601 is a nickel-chromium alloy used for applications that require resistance to corrosion and heat. This nickel alloy stands out due to its resistance to high temperature oxidation, remaining highly resistant to oxidation through 2200° F. Alloy 601 develops a tightly adherent oxide scale which resists spalling even under conditions of severe thermal cycling. This nickel alloy has good high temperature strength, and retains its ductility after long service exposure. It has good resistance to aqueous corrosion, high mechanical strength, and is readily formed, machined and welded. Inconel 601’s properties make it a material of broad utility in fields like thermal processing, chemical processing, pollution control, aerospace, and power generation. However, alloy 601 is not suggested for use in strongly reducing, sulfur bearing environments.
Inconel 660A, S66286
Alloy A286® has high strength and good corrosion resistance; therefore, it is used for applications at temperature up to 1300° F. Alloy A286® can be hardened and strengthened by heat treatment. Alloy A286® has been used in jet engines, superchargers, turbine wheels, blades, casings, afterburner parts, and fasteners. Available forms are seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, pipe fittings and flanges.
Alloy A286® has high strength and good corrosion resistance; therefore, it is used for applications at temperature up to 1300° F. Alloy A286® can be hardened and strengthened by heat treatment. Alloy A286® has been used in jet engines, superchargers, turbine wheels, blades, casings, afterburner parts, and fasteners. Available forms are seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, pipe fittings and flanges.
Inconel 718, Alloy 718, Haynes® 718, Nicrofer® 5219, Allvac® 718, Altemp® 718, ASTM B637, B 670, B 906, UNS N07718
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 718’s composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 718’s composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Inconel 825, 20Cr-35Ni-2Mo-3Cu-Nb, N08825, B163, 2.4858, NCF825(JISG4904), 3074 / NA 16, NiCr 21 Mo
Incoloy 825 is a nickel-iron- chromium alloy with titanium, copper, and molybdenum. Incoloy® 825's chemical composition provides great resistance to many corrosive environments, such as pitting, crevice corrosion, intergranular corrosion, and stress- corrosion cracking. Incoloy 825 has good mechanical properties from moderately to high temperatures. The hot - working range for Incoloy 825 is 1600 to 2150° F. The material has good weldability by all conventional processes.
These inconel 825, alloy 825 and incoloy 825 available in various forms like seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, fasteners, cap, elbow, erw pipes, reducer, round bar, tee, tube, pipe fittings and flanges like inconel 825 plate, inconel 825 erw pipes, inconel 825 flange, inconel 825 cap, inconel 825 elbow, inconel 825 reducer, inconel 825 sheet, inconel 825 tube etc.
Also offers uns n08825 flange, alloy 825 fittings, uns n08825 reducer, alloy 825 cap, uns n08825 plate, alloy 825 tube and many more.
Wide range of alloy 825 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube.
UNS N08825 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube.
Incoloy 825, alloy 825 and inconel alloy 825 is a nickel-iron-chromium alloy with additions of molybdenum, copper and titanium. The resistance of Incoloy 825 to general and localized corrosion under diverse conditions gives the alloy broad usefulness.
Incoloy 825 is a nickel-iron- chromium alloy with titanium, copper, and molybdenum. Incoloy® 825's chemical composition provides great resistance to many corrosive environments, such as pitting, crevice corrosion, intergranular corrosion, and stress- corrosion cracking. Incoloy 825 has good mechanical properties from moderately to high temperatures. The hot - working range for Incoloy 825 is 1600 to 2150° F. The material has good weldability by all conventional processes.
These inconel 825, alloy 825 and incoloy 825 available in various forms like seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, fasteners, cap, elbow, erw pipes, reducer, round bar, tee, tube, pipe fittings and flanges like inconel 825 plate, inconel 825 erw pipes, inconel 825 flange, inconel 825 cap, inconel 825 elbow, inconel 825 reducer, inconel 825 sheet, inconel 825 tube etc.
Also offers uns n08825 flange, alloy 825 fittings, uns n08825 reducer, alloy 825 cap, uns n08825 plate, alloy 825 tube and many more.
Wide range of alloy 825 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube.
UNS N08825 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube.
Incoloy 825, alloy 825 and inconel alloy 825 is a nickel-iron-chromium alloy with additions of molybdenum, copper and titanium. The resistance of Incoloy 825 to general and localized corrosion under diverse conditions gives the alloy broad usefulness.
Inconel 800, 800H, 800HT, ASTM B 409, B 408, B 407, B 564, UNS N08800/N08810/N08811, 20Cr-30Ni, B163, 1.4558, 1.4876, NCF800(JISG4904), NCF800H(JIS4904), 3074 / NA 15, X 10 Ni Cr-AlTi 32 20
Incoloy 800 is a combination of nickel and chromium alloy that has excellent tensile strength and resistance to oxidation as well as carburzation properties. This alloy is extremely functional as it maintains a stable structure, even when exposed to high temperature. The Inconel is extremely resistant to corrosion, even in acidic environment.
This inconel 800, alloy 800 and incoloy 800 can be availed in many forms like seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, fasteners, cap, elbow, erw pipes, reducer, fasteners, cap, elbow, erw pipes, reducer, round bar, tee, tube, round bar, tee, tube, forgings, pipe fittings and flanges like inconel 800 plate, inconel 800 fasteners, incoloy 800 seamless pipes, inconel 800 plate, inconel 800 tube, inconel 800 fittings, inconel 800 round bar, incoloy 800 round bar, alloy 800 tube, incoloy 800 tube, incoloy 800 tee etc.
Also offers alloy 800 seamless pipes, uns n08800 erw pipes, alloy 800 tee, uns n08800 elbow, alloy 800 sheet, uns n08800 plate, inconel 600 pipes, inconel 625 seamless pipes and many more.
Wide range of alloy 800 is manufactured and exported in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube. Alloy 800 is a widely used material of construction for equipment that must resist corrosion, have high strength or resist oxidation and other harmful effects of high-temperature exposure.
Inconel Alloy 800 is used for process piping, heat exchangers, heating-element sheathing, carburizing equipment, and nuclear steam-generator tubing. UNS N08800 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube at industrial rate.
Incoloy 800 is a combination of nickel and chromium alloy that has excellent tensile strength and resistance to oxidation as well as carburzation properties. This alloy is extremely functional as it maintains a stable structure, even when exposed to high temperature. The Inconel is extremely resistant to corrosion, even in acidic environment.
This inconel 800, alloy 800 and incoloy 800 can be availed in many forms like seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, fasteners, cap, elbow, erw pipes, reducer, fasteners, cap, elbow, erw pipes, reducer, round bar, tee, tube, round bar, tee, tube, forgings, pipe fittings and flanges like inconel 800 plate, inconel 800 fasteners, incoloy 800 seamless pipes, inconel 800 plate, inconel 800 tube, inconel 800 fittings, inconel 800 round bar, incoloy 800 round bar, alloy 800 tube, incoloy 800 tube, incoloy 800 tee etc.
Also offers alloy 800 seamless pipes, uns n08800 erw pipes, alloy 800 tee, uns n08800 elbow, alloy 800 sheet, uns n08800 plate, inconel 600 pipes, inconel 625 seamless pipes and many more.
Wide range of alloy 800 is manufactured and exported in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube. Alloy 800 is a widely used material of construction for equipment that must resist corrosion, have high strength or resist oxidation and other harmful effects of high-temperature exposure.
Inconel Alloy 800 is used for process piping, heat exchangers, heating-element sheathing, carburizing equipment, and nuclear steam-generator tubing. UNS N08800 is available in various forms like cap, elbow, erw pipes, fasteners, fittings, flange, plate, reducer, round bar, seamless pipes, sheet, tee and tube at industrial rate.
Monel Pipes & Tubes
Monel 400, Alloy 400, UNS N04400, 3074 / NA 13, 2.4360, NiCu 30 Fe
Monel 400 is a nickel-copper alloy (about 67% Ni – 23% Cu) that is resistant to sea water and steam at high temperatures as well as to salt and caustic solutions. Alloy 400 is a solid solution alloy that can only be hardened by cold working. This nickel alloy exhibits characteristics like good corrosion resistance, good weldability and high strength. A low corrosion rate in rapidly flowing brackish or seawater combined with excellent resistance to stress-corrosion cracking in most freshwaters, and its resistance to a variety of corrosive conditions led to its wide use in marine applications and other non-oxidizing chloride solutions. This nickel alloy is particularly resistant to hydrochloric and hydrofluoric acids when they are de-aerated. As would be expected from its high copper content, alloy 400 is rapidly attacked by nitric acid and ammonia systems. Monel 400 has great mechanical properties at subzero temperatures, can be used in temperatures up to 1000° F, and its melting point is 2370-2460° F. However, alloy 400 is low in strength in the annealed condition so, a variety of tempers may be used to increase the strength.
Monel 400 is a nickel-copper alloy (about 67% Ni – 23% Cu) that is resistant to sea water and steam at high temperatures as well as to salt and caustic solutions. Alloy 400 is a solid solution alloy that can only be hardened by cold working. This nickel alloy exhibits characteristics like good corrosion resistance, good weldability and high strength. A low corrosion rate in rapidly flowing brackish or seawater combined with excellent resistance to stress-corrosion cracking in most freshwaters, and its resistance to a variety of corrosive conditions led to its wide use in marine applications and other non-oxidizing chloride solutions. This nickel alloy is particularly resistant to hydrochloric and hydrofluoric acids when they are de-aerated. As would be expected from its high copper content, alloy 400 is rapidly attacked by nitric acid and ammonia systems. Monel 400 has great mechanical properties at subzero temperatures, can be used in temperatures up to 1000° F, and its melting point is 2370-2460° F. However, alloy 400 is low in strength in the annealed condition so, a variety of tempers may be used to increase the strength.
Monel K500, Alloy K-500, UNS N05500, 3074 / NA 18, 2.4375, NiCu 30 Al
Monel K500 is a precipitation-hardenable nickel-copper alloy that combines the excellent corrosion resistance characteristic of Monel 400 with the added advantage of greater strength and hardness. These amplified properties, strength and hardness, are obtained by adding aluminum and titanium to the nickel-copper base and by a thermal processing used to effect precipitation, typically called age hardening or aging. When in the age-hardened condition, Monel K-500 has a greater tendency toward stress-corrosion cracking in some environments than Monel 400. Alloy K-500 has approximately three times the yield strength and double the tensile strength when compared with alloy 400. Plus, it can be further strengthened by cold working prior to precipitation hardening. The strength of this nickel steel alloy is maintained to 1200° F but stays ductile and tough down to temperatures of 400° F. Its melting range is 2400-2460° F. This nickel alloy is spark resistant and non-magnetic to -200° F. However, it is possible to develop a magnetic layer on the surface of the material during processing. Aluminum and copper may be selectively oxidized during heating, leaving a magnetic nickel rich film on the outside. Pickling or Monel K-500 Barsbright dipping in acid can remove this magnetic film and restore the non-magnetic properties
Monel K500 is a precipitation-hardenable nickel-copper alloy that combines the excellent corrosion resistance characteristic of Monel 400 with the added advantage of greater strength and hardness. These amplified properties, strength and hardness, are obtained by adding aluminum and titanium to the nickel-copper base and by a thermal processing used to effect precipitation, typically called age hardening or aging. When in the age-hardened condition, Monel K-500 has a greater tendency toward stress-corrosion cracking in some environments than Monel 400. Alloy K-500 has approximately three times the yield strength and double the tensile strength when compared with alloy 400. Plus, it can be further strengthened by cold working prior to precipitation hardening. The strength of this nickel steel alloy is maintained to 1200° F but stays ductile and tough down to temperatures of 400° F. Its melting range is 2400-2460° F. This nickel alloy is spark resistant and non-magnetic to -200° F. However, it is possible to develop a magnetic layer on the surface of the material during processing. Aluminum and copper may be selectively oxidized during heating, leaving a magnetic nickel rich film on the outside. Pickling or Monel K-500 Barsbright dipping in acid can remove this magnetic film and restore the non-magnetic properties
Monel R-405, UNS N04405, 13Cr-Al, S40500, A268 TP405, 1.4002, SUS405(JISG3463)
Monel R405 is the free machining version of Monel 400. It is a nickel-copper alloy with a controlled amount of sulfur added to provide sulfide inclusions that act as chip breakers during machining. Like Monel 400, alloy R-405 is resistant to sea water and steam at high temperatures as well as to salt and caustic solutions. Monel R405 is a solid solution alloy that can only be hardened by cold working. This nickel alloy exhibits characteristics like good corrosion-resistance, good weldability and high strength. A low corrosion rate in rapidly flowing brackish or seawater combined with excellent resistance to stress corrosion cracking in most freshwaters, and its resistance to a variety of corrosive conditions led to its wide use in marine applications and other non-oxidizing chloride solutions. This nickel steel alloy is particularly resistant to hydrochloric and hydrofluoric acidswhenthey are de-aerated. As would be expected from its high copper content, alloy R-405 is rapidly attacked by nitric acid and ammonia systems. As with alloy 400, Monel R-405 is virtually immune to chloride ion stress corrosion cracking in typical environments. Generally, its corrosion resistance is very good in reducing environments, but poor in oxidizing conditions. It is not useful in oxidizing acids, such as nitric acid and nitrous. Nevertheless, it is resistant to most alkalis, salts, waters, food products, organic substances and atmospheric conditions at normal and elevated temperatures. Monel 400 and R-405 offer about the same corrosion resistance as nickel but with higher maximum working pressures and temperatures and at a lower cost due to its superior ability to be machined.
Monel R405 is the free machining version of Monel 400. It is a nickel-copper alloy with a controlled amount of sulfur added to provide sulfide inclusions that act as chip breakers during machining. Like Monel 400, alloy R-405 is resistant to sea water and steam at high temperatures as well as to salt and caustic solutions. Monel R405 is a solid solution alloy that can only be hardened by cold working. This nickel alloy exhibits characteristics like good corrosion-resistance, good weldability and high strength. A low corrosion rate in rapidly flowing brackish or seawater combined with excellent resistance to stress corrosion cracking in most freshwaters, and its resistance to a variety of corrosive conditions led to its wide use in marine applications and other non-oxidizing chloride solutions. This nickel steel alloy is particularly resistant to hydrochloric and hydrofluoric acidswhenthey are de-aerated. As would be expected from its high copper content, alloy R-405 is rapidly attacked by nitric acid and ammonia systems. As with alloy 400, Monel R-405 is virtually immune to chloride ion stress corrosion cracking in typical environments. Generally, its corrosion resistance is very good in reducing environments, but poor in oxidizing conditions. It is not useful in oxidizing acids, such as nitric acid and nitrous. Nevertheless, it is resistant to most alkalis, salts, waters, food products, organic substances and atmospheric conditions at normal and elevated temperatures. Monel 400 and R-405 offer about the same corrosion resistance as nickel but with higher maximum working pressures and temperatures and at a lower cost due to its superior ability to be machined.
Hastelloy Pipes & Tubes
Hastelloy C-22, Alloy C-22, UNS N06022, 2.4602, Ni Cr 21Mo 14 W, 21Cr-13Mo-3W-Ni, B622, NW6022(JISH4552)
Hastelloy C22, also known as alloy C22, is a versatile austenitic nickel-chromium-molybdenum-tungsten alloy with enhanced resistance to pitting, crevice corrosion and stress corrosion cracking. The high chromium content provides good resistance to oxidizing media while the molybdenum and tungsten content give good resistance to reducing media. This nickel steel alloy also has excellent resistance to oxidizing aqueous media including wet chlorine and mixtures containing nitric acid or oxidizing acids with chlorine ions. Other corrosives Hastelloy C-22 has resistance to are oxidizing acid chlorides, wet chlorine, formic and acetic acids, ferric and cupric chlorides, sea water, brine and many mixed or contaminated chemical solutions, both organic and inorganic. This nickel alloy also offers optimum resistance to environments where reducing and oxidizing conditions are encountered in process streams. This is beneficial in multi- purpose plants where such “upset” conditions occur frequently.
This nickel alloy resists the formation of grain-boundary precipitates in the weld heat-affected zone, thus making it suitable for most chemical process applications in the as-welded condition. Alloy C-22 should not be used in service temperatures above 1250° F due to the formation of detrimental phases which form above this temperature.
Hastelloy C22, also known as alloy C22, is a versatile austenitic nickel-chromium-molybdenum-tungsten alloy with enhanced resistance to pitting, crevice corrosion and stress corrosion cracking. The high chromium content provides good resistance to oxidizing media while the molybdenum and tungsten content give good resistance to reducing media. This nickel steel alloy also has excellent resistance to oxidizing aqueous media including wet chlorine and mixtures containing nitric acid or oxidizing acids with chlorine ions. Other corrosives Hastelloy C-22 has resistance to are oxidizing acid chlorides, wet chlorine, formic and acetic acids, ferric and cupric chlorides, sea water, brine and many mixed or contaminated chemical solutions, both organic and inorganic. This nickel alloy also offers optimum resistance to environments where reducing and oxidizing conditions are encountered in process streams. This is beneficial in multi- purpose plants where such “upset” conditions occur frequently.
This nickel alloy resists the formation of grain-boundary precipitates in the weld heat-affected zone, thus making it suitable for most chemical process applications in the as-welded condition. Alloy C-22 should not be used in service temperatures above 1250° F due to the formation of detrimental phases which form above this temperature.
Hastelloy C-276, Alloy C-276, UNS N10276, 2.4819, NiMo 16Cr15W, 15.5Cr-16Mo-5Fe-Ni, B622, NW0276(JISH4552)
Hastelloy C276 is a nickel-molybdenum-chromium superalloy with an addition of tungsten designed to have excellent corrosion resistance in a wide range of severe environments. The high nickel and molybdenum contents make the nickel steel alloy especially resistant to pitting and crevice corrosion in reducing environments while chromium conveys resistance to oxidizing media. The low carbon content minimizes carbide precipitation during welding to maintain corrosion resistance in as-welded structures. This nickel alloy is resistant to the formation of grain boundary precipitates in the weld heat-affected zone, thus making it suitable for most chemical process application in an as welded condition.
Although there are several variations of the Hastelloy nickel alloy, Hastelloy C-276 is by far the most widely used. Alloy C-276 is widely used in the most severe environments such as chemical processing, pollution control, pulp and paper production, industrial and municipal waste treatment, and recovery of sour natural gas.
Hastelloy C276 is a nickel-molybdenum-chromium superalloy with an addition of tungsten designed to have excellent corrosion resistance in a wide range of severe environments. The high nickel and molybdenum contents make the nickel steel alloy especially resistant to pitting and crevice corrosion in reducing environments while chromium conveys resistance to oxidizing media. The low carbon content minimizes carbide precipitation during welding to maintain corrosion resistance in as-welded structures. This nickel alloy is resistant to the formation of grain boundary precipitates in the weld heat-affected zone, thus making it suitable for most chemical process application in an as welded condition.
Although there are several variations of the Hastelloy nickel alloy, Hastelloy C-276 is by far the most widely used. Alloy C-276 is widely used in the most severe environments such as chemical processing, pollution control, pulp and paper production, industrial and municipal waste treatment, and recovery of sour natural gas.
Hastelloy X, UNS N06002, DIN 2.4665
Hastelloy X is a nickel-chromium-iron-molybdenum superalloy with outstanding high temperature strength, oxidation resistance, and fabricability. Alloy X’s oxidation resistance is excellent up to 2200° F. This nickel steel alloy has also been found to be exceptionally resistant to stress-corrosion cracking in petrochemical applications. Matrix stiffening provided by the molybdenum content results in high strength in a solid-solution alloy having good fabrication characteristics. Although this nickel alloy is primarily noted for heat and oxidation resistance it also has good resistance to chloride stress-corrosion cracking, carburization, and excellent resistance to reducing or carburizing atmospheres. Two common conditions that often lead to early failure in high temperature alloys, carburization and nitriding, Hastelloy X resists.
Hastelloy X is a nickel-chromium-iron-molybdenum superalloy with outstanding high temperature strength, oxidation resistance, and fabricability. Alloy X’s oxidation resistance is excellent up to 2200° F. This nickel steel alloy has also been found to be exceptionally resistant to stress-corrosion cracking in petrochemical applications. Matrix stiffening provided by the molybdenum content results in high strength in a solid-solution alloy having good fabrication characteristics. Although this nickel alloy is primarily noted for heat and oxidation resistance it also has good resistance to chloride stress-corrosion cracking, carburization, and excellent resistance to reducing or carburizing atmospheres. Two common conditions that often lead to early failure in high temperature alloys, carburization and nitriding, Hastelloy X resists.
Hastelloy B-2, Alloy B-2, UNS N10665, 2.4617, Ni Mo 28
Hastelloy B2 is a solid solution strengthened, nickel-molybdenum alloy, with significant resistance to reducing environments like hydrogen chloride gas, and sulfuric, acetic and phosphoric acids. Molybdenum is the primary alloying element which provides significant corrosion resistance to reducing environments. This nickel steel alloy can be used in the as-welded condition because it resists the formation of grain-boundary carbide precipitates in the weld heat-affected zone. This nickel alloy provides excellent resistance to hydrochloric acid at all concentrations and temperatures. In additions, Hastelloy B2 has excellent resistance to pitting, stress corrosion cracking and to knife-line and heat-affected zone attack. Alloy B2 provides resistance to pure sulfuric acid and a number of non-oxidizing acids.
Hastelloy B2 is a solid solution strengthened, nickel-molybdenum alloy, with significant resistance to reducing environments like hydrogen chloride gas, and sulfuric, acetic and phosphoric acids. Molybdenum is the primary alloying element which provides significant corrosion resistance to reducing environments. This nickel steel alloy can be used in the as-welded condition because it resists the formation of grain-boundary carbide precipitates in the weld heat-affected zone. This nickel alloy provides excellent resistance to hydrochloric acid at all concentrations and temperatures. In additions, Hastelloy B2 has excellent resistance to pitting, stress corrosion cracking and to knife-line and heat-affected zone attack. Alloy B2 provides resistance to pure sulfuric acid and a number of non-oxidizing acids.
Hastelloy B-3, UNS N010675
Hastelloy B-3 is a nickel-molybdenum alloy with excellent resistance to pitting, corrosion, and stress-corrosion cracking plus, thermal stability superior to that of alloy B-2. In addition, this nickel steel alloy has great resistance to knife-line and heat–affected zone attack. Alloy B-3 also withstands sulfuric, acetic, formic and phosphoric acids, and other non-oxidizing media. Furthermore, this nickel alloy has excellent resistance to hydrochloric acid at all concentrations and temperatures. Hastelloy B-3’s distinguishing feature is its ability to maintain excellent ductility during transient exposures to intermediate temperatures. Such exposures are routinely experienced during heat treatments associated with fabrication.
Hastelloy B-3 is a nickel-molybdenum alloy with excellent resistance to pitting, corrosion, and stress-corrosion cracking plus, thermal stability superior to that of alloy B-2. In addition, this nickel steel alloy has great resistance to knife-line and heat–affected zone attack. Alloy B-3 also withstands sulfuric, acetic, formic and phosphoric acids, and other non-oxidizing media. Furthermore, this nickel alloy has excellent resistance to hydrochloric acid at all concentrations and temperatures. Hastelloy B-3’s distinguishing feature is its ability to maintain excellent ductility during transient exposures to intermediate temperatures. Such exposures are routinely experienced during heat treatments associated with fabrication.
| DIN | AFNOR | UNS | Others | |
| Hastelloy B-2 | 2.4882 GNiMo30 | - | N30012 | Hastelloy B-2(5) |
| Hastelloy B-3 | - | - | N10675 | Hastelloy B-3(5) |
| Hastelloy Hybrid BC1 | - | - | - | Hastelloy Hybrid BC1 |
| Hastelloy C-276 | 2.4686 GNiMo17Cr | - | N30002 | Hastelloy C-276 (5) |
| Hastelloy C-4 | 2.4610 NiMo16C616Ti (5) | NC16D16M | N26455 | Hastelloy C-4 (5) |
| Hastelloy C-22 | 9.4602 | - | N26022 | Hastelloy C-22 (5) |
| Hastelloy C-2000 | - | - | N26200 | Hastelloy C-2000 (5) |
| Hastelloy C-22HS | - | - | - | Hastelloy C-22HS (5) |
| Hastelloy G-30 | - | - | N06030 | Hastelloy G-30 (5) |
| Hastelloy G-35 | 2.4643 NiCr33Mo8 | - | N06035 | Hastelloy G-35 (5) |
Titanium Pipes & Tubes
- Grade 1 Unalloyed titanium, low oxygen.
- Grade 2 Unalloyed titanium, standard oxygen.
- Grade 2H Unalloyed titanium (Grade 2 with 58 ksi minimum UTS).
- Grade 3 Unalloyed titanium, medium oxygen.
- Grades 1-4 are unalloyed and considered commercially pure or "CP". Generally the tensile and yield strength goes up with grade number for these "pure" grades. The difference in their physical properties is primarily due to the quantity of interstitial elements. They are used for corrosion resistance applications where cost, ease of fabrication, and welding are important.
- Grade 5, also known as Ti6Al4V, Ti-6Al-4V or Ti 6-4, is the most commonly used alloy. It has a chemical composition of 6% aluminium, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabricability.
- Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 MPa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 MPa. And tempered 6061 aluminium alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively.
- Grade 6 contains 5% aluminium and 2.5% tin. It is also known as Ti-5Al-2.5Sn. This alloy is used in airframes and jet engines due to its good weldability, stability and strength at elevated temperatures.
- Grade 7 contains 0.12 to 0.25% palladium. This grade is similar to Grade 2. The small quantity of palladium added gives it enhanced crevice corrosion resistance at low temperatures and high pH.
- Grade 7H is identical to Grade 7 with enhanced corrosion resistance.
- Grade 9 contains 3.0% aluminium and 2.5% vanadium. This grade is a compromise between the ease of welding and manufacturing of the "pure" grades and the high strength of Grade 5. It is commonly used in aircraft tubing for hydraulics and in athletic equipment.
- Grade 11 contains 0.12 to 0.25% palladium. This grade has enhanced corrosion resistance.
- Grade 12 contains 0.3% molybdenum and 0.8% nickel.
- Grades 13, 14, and 15 all contain 0.5% nickel and 0.05%.
- Grade 16 contains 0.04 to 0.08% palladium. This grade has enhanced corrosion resistance.
- Grade 16H contains 0.04 to 0.08% palladium.
- Grade 17 contains 0.04 to 0.08% palladium. This grade has enhanced corrosion resistance.
- Grade 18 contains 3% aluminium, 2.5% vanadium and 0.04 to 0.08% palladium. This grade is identical to Grade 9 in terms of mechanical characteristics. The added palladium gives it increased corrosion resistance.
- Grade 19 contains 3% aluminium, 8% vanadium, 6% chromium, 4% zirconium, and 4% molybdenum.
- Grade 20 contains 3% aluminium, 8% vanadium, 6% chromium, 4% zirconium, 4% molybdenum and 0.04% to 0.08% palladium.
- Grade 21 contains 15% molybdenum, 3% aluminium, 2.7% niobium, and 0.25% silicon.
- Grade 23 contains 6% aluminium, 4% vanadium, 0.13% (maximum) Oxygen. Improved ductility and fracture toughness with some reduction in strength.
- Grade 24 contains 6% aluminium, 4% vanadium and 0.04% to 0.08% palladium.
- Grade 25 contains 6% aluminium, 4% vanadium and 0.3% to 0.8% nickel and 0.04% to 0.08% palladium.
- Grades 26, 26H, and 27 all contain 0.08 to 0.14% ruthenium.
- Grade 28 contains 3% aluminium, 2.5% vanadium and 0.08 to 0.14% ruthenium.
- Grade 29 contains 6% aluminium, 4% vanadium and 0.08 to 0.14% ruthenium.
- Grades 30 and 31 contain 0.3% cobalt and 0.05% palladium.
- Grade 32 contains 5% aluminium, 1% tin, 1% zirconium, 1% vanadium, and 0.8% molybdenum.
- Grades 33 and 34 contain 0.4% nickel, 0.015% palladium, 0.025% ruthenium, and 0.15% chromium .
- Grade 35 contains 4.5% aluminium, 2% molybdenum, 1.6% vanadium, 0.5% iron, and 0.3% silicon.
- Grade 36 contains 45% niobium.
- Grade 37 contains 1.5% aluminium.
- Grade 38 contains 4% aluminium, 2.5% vanadium, and 1.5% iron. This grade was developed in the 1990s for use as an armor plating. The iron reduces the amount of Vanadium needed as a beta stabilizer. Its mechanical properties are very similar to Grade 5, but has good cold workability similar to grade 9.
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