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Superalloys

Monel 400, Monel K-500/K500, Waspaloy, L605 (HS 25), Haynes 188, Haynes 230,
Haynes 263, HYMU 80/ HY MU 80

Sheet, Plate, Bar

You can
send RFQs by filling out the RFQ form below. Or you can
fax RFQs to 800-707-3439. We will get back to you ASAP.

* Inconel/Incoloy and Monel are
Registered Trademarks of Special Metals Corporation and its subsidiaries.

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**Superalloys**

Superalloys are simply defined as "alloys
developed for elevated temperature service, usually based on group VIIA
elements, where relatively severe mechanical stressing is encountered and high
surface stability is frequently required". Three classes of alloys have
appeared: cobalt-base, nickel-base, and iron-base to meet this definition.

**
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****Superalloys:**
Monel 400,
Monel K-500/K500,
Waspaloy,
L605 (HS 25),
Haynes 188,
Haynes 230,
Haynes 263,
HYMU 80/ HY MU 80

**
1)
Monel 400**

Monel is resistant to corrosion and acids, and
some alloys can withstand a fire in pure oxygen. It is commonly used in
applications with highly corrosive conditions. The good resistance against
corrosion by acids and oxygen makes monel a good material for the chemical
industry.

* Monel 400 Sheet, Plate Per QQ-N-281 CL A, AMS
4544, ASTM-B-127 * Thickness: 0.018"~3.000", Width: 12"~60", Length: 36"~192"

* Monel 400 Tubing is offered in a variety of requested sizes.

**
2)
Monel K-500 /K500**

Small additions of aluminium and titanium form an
alloy (K-500) with the same corrosion resistance but with much greater
strength due to gamma prime formation on aging.

* Monel K-500/K500 Sheet, Plate Per QQ-N-286 * Thickness: 0.040"~1.000", Width: 36"~48", Length: 60"~180"

**
3)
Waspaloy**

* Waspaloy Sheet, Plate Per AMS 5544, Chem AMS
5706 5707 5708 5709 * Thickness: 0.012"~1.000", Width: 12"~48",
Length: 36"~120"

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**
4)
L605 (HS 25)
**

Alloy L605 has excellent strength, good oxidation resistance, very good
sulfidation resistance, and relatively good resistance to wear and galling.
Used in gas turbine parts, bearings, and various industrial applications.

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UNS R30605/
**
Haynes 25

* L605 Sheet, Plate Per AMS 5537, B50T26, B50A460, Thickness: 0.010"~1.500" , Width: 36"~48", Length: 76"~120"

* L605 (HS 25) Vac Melt Bar Per AMS
5759, Diameter: 0.205"~6.5", Length: 144" Random Length

**
5)
Haynes 188
**

Haynes 188 Alloy is a Cobalt-Nickel-Chromium-Tungsten Alloy that combines
excellent high temperature strength with very good resistance to oxidizing
environments.

UNS R30188/ Alloy 188

* Haynes 188 Sheet, Plate Per AMS 5608, B50A712,
B50TF59, Thickness: 0.010"~2.000", Width: 36"~48", Length: 36"~144"

* Haynes 188 Bar Per AMS 5772, B50TF74, Diameter: 0.400"~7.000", Length: 144"
Random Length

**
6)
Haynes 230
**

Haynes 230 has best balance of strength, thermal stability, oxidation
resistance, thermal cycling resistance and fabricability of any major
high-temperature alloy. Used in gas turbine combustors and other key
stationary components. Also used for heat treating and industrial heating
applications, and in the chemical/petrochemical process industry and in fossil
energy plants.

UNS
N06230/ Haynes 230 Alloy

* Haynes 230 Sheet, Plate Per AMS 5878,
ASTM-B-435, B50TF246, Thickness: 0.016"~1.500", Width: 36"~48",
Length: 36"~144"

* Haynes 230 Bar Per AMS 5891, ASTM-B-572, EMS
55474, Diameter: 0.500"~4.500", Length: 144"
Random Length

**
7)
Haynes 263
**

* Haynes 263 Sheet, Plate Per AMS 5872, B50A771A, Thickness: 0.063"~0.385", Width: 36"~48", Length: 120"~144"

**
8)
HYMU 80 / HY MU 80**

* HYMU 80 / HY MU 80 Sheet, Plate Per Capable of
Mil-N-14411 Comp 1, ASTM-A-753 Type 4, Thickness: 0.004"~1.500", Width: 12"~30", Length: 60"~120"

* HYMU 80 / HY MU 80 Bar Per Capable of
Mil-N-14411 Comp 1, ASTM-A-753 Type 4, Diameter: 0.250"~2.500", Length: 144"
Random Length

**<Cobalt
Alloy>**

L605 L-605Sheet, Plate: AMS 5537

**
L605 L-605 Bar, Alloy # 25**, AISI 670: AMS 5759, AMS 5796

**<Super / High Temperature Alloys>**

**Invar 36 HRAP Plate:** ASTM B-753, MIL-S-16598A AMD 2, **Kovar: **AMS 7726, AMS
7727, AMS 7728, MIL-I-23011 C1-1

Hastelloy
Alloys

Hastelloy is a superalloy known for its resistance to high temperatures and
stress in severely corrosive environments. Forged primarily from nickel, some
types of Hastelloy alloys are common in nuclear reactors, chemical reactors
and pipes & valves in chemical installations. Hastelloy X is also used for
components such as combustion chambers, tail pipes in aircraft and land-based
gas turbine engines.

Nickel-based specialty metal Super Alloy Hastelloy X AMS 5536 is the common
Sheet and Plate specification.

UNS N06002/ Hastelloy/ Hastelloy X/ Alloy X

**
**

**Hastelloy X, Hastelloy X-750:** AMS 5754, AMS 5798, AMS 5536, AMS 5587

**Hastelloy C 276: **AMS 5530, AMS 5750, Hastelloy W, S, N: AMS 5755, AMS
5711, AMS 5607

**
**

**Waspaloy: **AMS 5706, AMS 5707, AMS 5708, AMS 5709, AMS 5828, AMS 5706, AMS 5544

**Maraging 300: **AMS 6514, 4750: AMS 7718

**Nickel 200:** ASTM-B-160, Nickel 400, Nickel 405, Nickel K-500: AMS 4544,
AMS 4574, AMS 4575, AMS 4576, AMS 4674, AMS 4675, AMS 4730, QQ-N-281 A,
QQ-N-281 B

**Rene 41:**
AMS 5545, AMS 5712, AMS 5713, AMS 5800

**Haynes 188:** AMS 5772, AMS 5801, AMS 5608, AMS 5807

**N-155:** AMS 5769, AMS 5794, AMS 5532, AMS 5585

**Monel K500: **QQ-N-286, Inconel 706: AMS 5701, AMS 5702, AMS 5703, Inconel 722: AMS 5684

**Inconel 909:** AMS 5884, AMS 5892, AMS 5893, Inconel 925: NACE MR-01-75 Round
Bar

**Nimonic 75:** BS HR5, HR203, HR403, HR504, Nimonic 90: BS HR2, HR202, HR501,
HR502, Nimonic 263: AMS 5872, AMS 5882

**MP35N:**
AMS 5758, AMS 5844, AMS 5845, Alloy 31: AMS 5545, 5712, N155 (Multimet): AMS 5532

**Alloy 188: **AMS 5608, AMS 5772 ,HY MU-80: AMS 7701, MIL-N-14411, MU
METAL-ANNEALED HALF HARD, 1/2H: AMS 7701, AMS 7702

**M-36:** AMS 7711, M-27: AMS 7712, M-4, M-5, M-6: AMS 7716

* Nitronic 60, also considered a Super Alloy, is
designed to be the best non-galling stainless steel.

**Beryllium Copper:** ASTM B194, B196, B197,
B534

Copper beryllium alloys are used for their high
strength and good electrical and thermal conductivities. There are two groups
of copper beryllium alloys, high strength alloys and high conductivity alloys.
Beryllium-copper alloys have desirable properties facilitating their use in a
variety of demanding applications. The high-strength alloys (C17200 and
C17000) are less dense (.298 lbs./cu. in.) than conventional specialty
coppers. This often results in a yield of up to 7 percent more feet per pound
than high-strength phosphor bronze. The high-conductivity beryllium-copper
alloys (C17500 C17510 and C17410) are ideally suited to applications requiring
high operating temperatures, or high strength and conductivity.

**C17200 Beryllium Copper:** ASTM B196, AMS
4533

Most commonly utilized beryllium copper alloy and
is notable for exhibiting the highest strength and hardness compared to
commercial copper alloys. Its strength and hardness is similar to that of
steel. C17200 ultimate tensile and Rockwell hardness properties in a peak aged
condition are in the 200 ksi range and RC 45 respectively (electrical
conductivity 22% IACS minimum).

**C175 - C17500 Beryllium Copper: **ASTM B441, ASTM B534

C17500/C17510 offer a combination of high electrical and thermal conductivity
with good strength compared to most copper based alloys. C17500 alloy is the
mirror image of alloy C17510 in terms of its properties and characteristics.
The alloys differ in that C17500 specifies a cobalt alloying addition
(2.40-2.70%) and alloy 17510 specifies a nickel alloying addition
(1.40-2.20%), but their performance are the same.

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