ASTM A860

Spread the love

ASTM A860 – Wrought High-Strength Low-Alloy Steel Butt-Welding Fittings

Grade: WPHY42  WPHY46  WPHY52  WPHY60  WPHY65  WPHY70

Chemical Compositions (max, %) Heat analysis

C Mn P S Si Ni Cr Mo Cu Ti V Cb V+Cb Ti
0.20 1.00-1.45 0.030 0.010 0.15-0.40 0.50 0.30 0.25 0.35 0.05 0.10 0.04 0.12 0.06

1.The carbon equivalent as calculated by the follwing formula, shall not exceed 0.42%:CE=C+Mn/6+(Cr+Mo+V)/5+(Ni+Co)/15.

2.If vacuum carbon deoxidation is used, silicon chall not exceed 0.10% by heat analysis and 0.12% by product analysis.1.The carbon equivalent as calculated by the follwing formula, shall not exceed 0.42%:CE=C+Mn/6+(Cr+Mo+V)/5+(Ni+Co)/15.

3.The sum of Ni+Cr+Mo+Cu shall not exceed 1.0%.

 

Mechanical Requirements

Property Grade
WPHY 42 WPHY 46  WPHY 52 WPHY 60 WPHY 65 WPHY 70
Yield strength, minA 0.2 % offset, ksi [MPa] 42 [290] 46 [315] 52 [360] 60 [415] 65 [450] 70 [485]
Tensile strength, ksi [Mpa] 60 [415] −85 [585] 63 [435]   − 88 [605] 66 [455]     − 91 [625] 75 [515]     − 100 [690] 77 [530]      − 102 [705] 80 [550]  −105 [725]
Elongation:
Standard round specimen, or small-size proportional specimen, min, % in 4D
25 25 25 20 20 20
Rectangular specimen, for section thickness 5⁄16 in. [7.94mm] and over, and for all small sizes tested in full section; min, % in 2 in. [50 mm]. 32 32 32 28 28 28
Rectangular specimen for thickness less than 5⁄16 in. [7.94mm]; min, % 2 in. [50 mm]. Width of specimen 11⁄2 in. [40mm]. B B B B B B

Toughness: Cv energy absorption C; measured at −50°F [−46°C].

Size, mm Average/min, ft·lbs[J] Lateral Expansion min, MLS[mm]
10 × 10 30/25 [40/34] 25 [0.64]
10 × 7.5 25/21 [34/28] 21 [0.53]
10 × 5 20/17 [27/23] 13 [0.33]

A) Actual yield strength shall not exceed specified minimum by more than 15 ksi [105 MPa].

B) For each 1⁄32-in. [0.79 mm] decrease in section thickness below 5⁄16 in. [7.94 mm], a deduction of 1.5 % from the elongation value of specimens above 5⁄16 in. [7.94mm] is permitted. When the section thickness lies between two values defined above, the minimum elongation value is determined by the following equation: E = 48t + 15.00

where: E = elongation % in 2 in. [50 mm], and t = actual thickness of specimen

C) These requirements are intended to minimize fracture initiation. The requirements are not intended to give assurance against fracture propagation.

 

Hardness Requirements

Fittings shall have a maximum hardness of 22 HRC (235 HB).