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UNS N07719

Inconel Alloy
718SPF

UNS N07719
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  3. Inconel 718SPF
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Introduction
Main Standards
Chemical Composition
Data Sheet
Applications
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Inconel 718SPF Introduction

logo of precipitation strengthened alloy

Precipitation
Strengthened Alloy

Nickel
Chromium
Iron
Niobium
Corrosion
Resistance
81
Mechanical
Behavior
91
Purity
94

Overview

As a leading supplier & manufacturer in China, AEETHER supply cost-effective Inconel 718SPF Products.

INCONEL® alloy 718SPF is a specifically "tailored" version of INCONEL alloy 718, designed for the superplastic forming process. The alloy is optimized for the process by rigorous control of composition, melt practice and rolling conditions.

INCONEL alloy 718SPF was developed to meet the need for a nickel-base alloy suitable for manufacture into complex shaped components subject to a combination of high temperature, high temperature corrosion and high stress. INCONEL alloy 718SPF meets all the mechanical property requirements of AMS 5596G, as annealed plus aged, as well as all requirements of AMS 5950, which is specific to INCONEL alloy 718SPF.

Superplastic forming, now highly sophisticated and used extensively for producing commercial and military aircraft components, is an ideal process for manufacturing complex shaped parts. Use of superplastic forming can enhance component performance and reliability while lowering overall manufacturing cost by reducing the need for extensive welding or other joining methods, lowering the inventory of parts and simplifying the manufacturing process.

Mechanical Properties

INCONEL alloy 718SPF is produced with an annealed temper. The alloy is produced to a grain size of ASTM No. 10 (0.01 mm/0.0004 in) or finer. As produced, INCONEL alloy 718SPF sheet meets the strength and ductility requirements of AMS 5596G, as annealed plus aged.

Corrosion Resistance

INCONEL alloy 718SPF, like alloy 718, has excellent resistance to corrosion in many media. This characteristic, similar to that of other nickel-chromium alloys, is a function of its composition.

Nickel contributes to a resistance to corrosion by many inorganic and organic compounds, other than those that are strongly oxidizing, throughout wide ranges of acidity and alkalinity. It is also useful in providing resistance to chloride- ion stress-corrosion cracking. Chromium imparts an ability to withstand attack by oxidizing media and sulfur compounds. Molybdenum is know to contribute to resistance to pitting in many media.

Above all, INCONEL alloy 718SPF is important for its strength and corrosion resistance at high operating temperatures.

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Inconel 718SPF Standards

SAE AMS 5914
Sheet
SAE AMS 5950
Sheet

Inconel 718SPF Chemical Composition

Data Sheet

Physical Properties

Density g/cm3 8.22
lb/in.3 0.297
Melting Range °F 2300 - 2437
°C 1260 - 1335
Specific Heat Btu/lb-°F 0.104
J/kg-°C 435
Curie Temperature °F -170
°C -113
Permeability at 200 oersted 15.9 kA/m 1.0011

Mechanical Properties

INCONEL alloy 718SPF
Annealed
AMS 5596G Solution
Annealed
AMS 5950 Solution
Annealed
Room Temperature Tensile Properties
0.2% Y.S., ksi (MPa) 120 (829) 80 (552) max. 155 (1069) max.
U.T.S., ksi (MPa) 162 (1117) 140 (965) max. 185 (1276) max.
Elongation, % 31 30 min. 20 min.
Hardness, Rc 24 25.5 max. 34 max.
Grain Size, ASTM No. 12 10 or finer
Aged
0.2% Y.S., ksi (MPa) 202 (1393) 150 (1034) min. 148 (1020) min.
U.T.S., ksi (MPa) 225 (1551) 180 (1241) min. 180 (1241) min.
Elongation, % 16 12 min. 12 min.
Hardness, Rc 45 36 min. 36 min.
1200°F (649°C) Tensile Properties Aged
0.2% Y.S., ksi (MPa) 160 (1103) 120 (827) min. 120 (827) min.
U.T.S., ksi (MPa) 177 (1220) 145 (1000) min. 145 (1000) min.
Elongation, % 22 5 min. 5 min.
1200°F (649°C) /100 ksi (690 MPa) Stress Rupture Properties Aged
Life, h 95 23.0 min. 23.0 min.
Elongation, % 11.2 4 min. 4 min.
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Inconel 718SPF Applications