SEAMLESS PIPES

A seamless pipe, as the name suggests, is a pipe without a seam or a weld-joint. Seamless pipes are thought to be able to withstand higher pressure, higher temperatures, higher mechanical stress and a corrosive atmosphere. It can be found in a wide range of applications such as in oil and gas, refinery, Petrochemical, chemical, fertilizer, power, automotive, bearing, mechanical and structural.

The production of our seamless steel pipes is tightly regulated and all of the pipes we stock have been fully tested to international standards to ensure we only supply the highest quality products.

As a leading supplier of seamless stainless tubular products, we offer

• Seamless Stainless Steel Pipe
• Seamless Duplex Steel Pipe
• Seamless Super Duplex Steel Pipe
• Seamless Nickel Alloy Pipe

Our seamless pipes are manufactured in l in accordance with:

• ASTM A790 • ASTM A312 • ASTM A409
• ASTM A269 • ASTM B423 • ASTM B444

Dimensions in accordance with:

• ANSI B36.19 • ANSI B36.10

For more information about our range of seamless pipes, call your nearest Anita Steel & Metals sales office.

Alloy MP35N® (AMS 5844/AMS 5845/ NACE MR0175)

Chemical Composition Limits

Weight %

Ni

Co

Cr

Mo

Ti

Fe

Si

Mn

P

B

S

C

MP35N®

33-37

Bal

19-21

9-10.5

1 max

1 max

0.15 max

0.15 max

0.015 max

0.010 max

0.010 max

0.03 max

MP35N® is a registered trademark of SPS Technologies Inc.

MP35N® is a multi-phase alloy containing Nickel, Cobalt, Chromium and Molybdenum with a unique range of properties - ultra high strength, toughness, bio-compatibility and corrosion resistance. It is produced by vacuum induction melting and vacuum arc re-melting (VIM-VAR) and is then strengthened by work hardening and aging, giving hardness's of up to 55-60 Rockwell C and strength levels as high as 260-300 KSI.

Due, to this unique combination of properties, MP35N® has many applications in such industries as oil and gas, aerospace and medical. MP35N can be effectively used at cryogenic temperatures without embrittlement and maintain its properties at temperatures up to 600°F, and is also suitable for medical implants and orthodontic/prosthetic devices.

MP35N® is able to resist corrosion to most mineral acid, hydrogen sulfide and seawater environments whilst exhibiting excellent resistance to stress corrosion cracking and hydrogen embrittlement, even at high strength levels. NACE MR0175 allows a hardness of up to 51 HRC for material that has been work strengthened and aged by one of the processes listed in the table below.

Anita Steel & Metals supplies MP35N® in round bar certified to either AMS 5844 (0.270" - 1.520" diameter) or NACE MR0175 (0.5" - 2.5" diameter), as well as sheet, strip and plate products suitable for medical applications.

Typical Mechanical Properties

Material	Condtion	Ultimate Tensile Strength ksi	0.2 % Yield Strength ksi	Elongation %	Reduction of Area %	Hardness HRC
MP35N ® AMS 5844	Solution Heat Treated and Work Strengthened	255	225	12	50	45
MP35N® AMS 5845	Solution Heat Treated and Work Strengthened and Aged	260	230	8	35	38 min

AMS 5844 is Solution Treated and Cold Worked. The AMS specification only requires that the hardness shall not be lower than 38 HRC or equivalent. However other typical mechanical properties of AMS 5844 are detailed above.

Material	Condtion	Tensile Strength ksi	Yield Strength ksi	Elongation %	Reduction of Area %	Hardness HRC
MP35N® NACE MR0175	Age @ 1300°F/ 4 hrs	220	210	10	40	51 max
MP35N® NACE MR0175	Age @ 1350°F / 4hrs	210	200	10	40	51 max
MP35N® NACE MR0175	Age @ 1425°F / 6hrs	190	180	10	40	51 max
MP35N® Properties as per NACE MR0175 - Cold Drawn - Reduced Strength (min properties, round bar under 2" dia)

Availability
Alloy MP35N® is available in Round Bar, Tube, Wire, Sheet and Plate. For all stock availability contact Sales.

Specifications
UNS R30035

AMS 5758 - MP35N® VIM-VAR Bar
Solution heat treated @1900-1925°F for 4 to 8 hours

AMS 5844 - MP35N® VIM-VAR Bar
Solution heat treated @1900-1925°F for 4 to 8 hours and Work Strengthened

AMS 5845 - MP35N® VIM-VAR Bar
Solution heat treated @ 1900-1925°F for 4 to 8 hours, Work Strengthened & Aged @ 1000-1200°F for 4 hours

NACE MR0175
ASTM F-562 - Surgical Implant Applications
BS 7252-6 Surgical Implant Applications
ISO 5832-6 Surgical Implant Applications

MP35N® is a registered trademark of Standard Pressed Steel (SPS) Technologies Inc.

TITANIUM TI6AL4V GRADES

Tiatanium TI6AL4V

Grade 5, also known as Ti6Al4V, Ti-6Al-4V, Ti 6-4 or R56400 is the most commonly used titanium alloy. It has a chemical composition of 6% aluminium, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. Grade 5 is used extensively in Aerospace, Medical, Marine, and Chemical Processing. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties. Among its many advantages, it is heat treatable. This grade has an excellent combination of strength, corrosion resistance, weld and fabricability. In consequence, its uses are numerous such as for military aircraft or turbines. It is also used in surgical implants. Generally, it is used in applications up to 400 degrees Celsius. Its properties are very similar to those of the 300 stainless steel series, especially 316. Ti-6Al-4V is a two phase alpha + beta grade of titanium and is the most widely used of all the titanium grades.

Alloy 625 (Inconel®)

Alloy 625 (Inconel®*) is a nickel-chromium-molybdenum alloy with a small niobium and tantalum addition. It is an excellent general purpose material for elevated temperature use in high strength, oxidation problem areas and finds particular application in the aerospace and offshore oil & gas industries. Alloy 625 shows excellent resistance to a variety of corrosive media.

Alloy 625 demonstrates excellent resistance to pitting, crevice corrosion, stress corrosion, corrosion fatigue and erosion corrosion whilst maintaining its mechanical properties up to about 450 ºC. It is highly resistant to a wide range of organic and mineral acids combined with good corrosion resistance to high temperature sulphides and chlorides. The niobium and tantalum within the matrix act in conjunction with the molybdenum to provide a high strength alloy without the need for additional heat treatment.

Related Specifications of Alloy 625 (Inconel®*)

• NA21
• N06625
• NACE MR 0175
• ISO 15156-3
• AMS 5666
• ASTM B446
• 2.4856
• NiCr22Mo9Nb (EU)

Nominal Composition of Alloy 625 (Inconel®*)

Ni 61.0%, Cr 21.5%, Mo 9.0%, Nb & Ta 3.6%

Mechanical Properties of Alloy 625 (Inconel®*)

Ultimate Tensile Strength (N/mm²)	Proof Stress (N/mm²)	Elongation (%)	Hardness (HB)
690	275	30

Key Features of Alloy 625 (Inconel®*)

• Strength retained up to 450ºC
• Very good resistance to corrosion fatigue
• High pitting, crevice and stress corrosion resistance
• Excellent oxidation resistance

Applications of Alloy 625 (Inconel®*)

Offshore & marine | Components where exposure to sea water and high mechanical stresses are required; oil and gas production where hydrogen sulphide and elementary sulphur exist at temperature in excess of 150C; flare stacks; hydrocarbon processing from tar-sand and oil-shale recovery projects

Chemical processing | Flue gas desulphurisation plant, flare stacks, offshore sour oil and gas production, waste incineration, phosphoric acid production and nuclear fuel processing

Anita Steel & Metals- a leading supplier of Alloy 625 (Inconel®*)

With decades of experience and a huge range of stock, Anita Steel & Metals is an industry leader in the supply of Alloy 625 (Inconel®*) and other high quality specialist engineering alloys.

To buy or learn more about Alloy 625 (Inconel®*) contact us now, or fill in the enquiry form on the right hand side and we will be in touch shortly.

*Inconel® is a registered trademark of the INCO family of companies

NICKEL ALLOYS
	Related Specifications				Mechanical Properties
Alloy Name	BS	UNS	BS EN	Others	Ultimate Tensile Strength N/mm²	Minimum Yield Strength N/mm²	Elongation %	Hardness HB
Al­lo­y 60­0	NA­14	N0­66­00		BS­30­76	55­0	24­0	30
Al­lo­y 62­5 (I­nc­on­el­®)	NA­21	N0­66­25		AM­S 56­66	69­0	27­5	30
Al­lo­y 71­8		N0­77­18		AM­S 56­62­, 56­63­, 56­64	10­34	82­7	17	31­3-35­4
AP­I6­A7­18		N0­77­18		AP­I6­A7­18	10­34	82­7	17	31­3-35­4
Al­lo­y 82­5	NA­16	N0­88­25		BS­30­76	59­0	22­0	30
Ha­st­el­lo­y C2­76		N1­02­76		HA­ST­EL­LO­Y®	69­0	28­3	40
Al­lo­y 80­A	BS­30­76 NA­20	N0­70­80		BS­2 HR­1	10­00	62­0	20
Mo­ne­l Al­lo­y 40­0	NA­13	N0­44­00		BS­30­76	48­0-60­0	17­0-41­5	20-35	35 HR­C ma­x
Mo­ne­l Al­lo­y K5­00	NA­18	N0­55­00		BS­30­76	97­0-10­00	69­0-76­0	15-20	27-35 HR­C