Nickel Haynes 188 (tm)

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Applications

While primarily employed in the aerospace industry, this alloy has found uses in commercial industrial applications including land-based gas turbines. Generally found in hot sections of engines in burner cans, ducting and afterburner components. In recent years, it has been eclipsed by Alloy 230 for many applications due to improved properties.

Cold Workability

This alloy can be readily cold formed using all common techniques. Its high work hardening rate will require intermediate annealing for extensive deformation.

Forgeability

Soak thoroughly at 2150 F (1175 C), followed by rapid post-work cooling.

Formability

This alloy has good ductility and may be readily formed by all conventional methods. Because the alloy is stronger than regular steel it requires more powerful equipment to accomplish forming. Heavy-duty lubricants should be used during cold forming. It is essential to thoroughly clean the part of all traces of lubricant after forming as embrittlement of the alloy may occur at high temperatures if lubricant is left on. The alloy will work harden rapidly and intermediate annealing may be required for extensive forming operations.

Heat Treatability

Solution heat treat at 2150 F (1175 C) and cool rapidly. Annealing at temperatures below this may cause carbide precipitation resulting in deleterious effects on properties.

Machinability

Conventional machining techniques used for iron based alloys may be used. This alloy does work-harden during machining and has higher strength and "gumminess" not typical of steels. Heavy duty machining equipment and tooling should be used to minimize chatter or work-hardening of the alloy ahead of the cutting. Most any commercial coolant may be used in the machining operations. Water-base coolants are preferred for high speed operations such as turning, grinding, or milling. Heavy lubricants work best for drilling, tapping, broaching or boring. Turning: Carbide tools are recommended for turning with a continuous cut. High-speed steel tooling should be used for interrupted cuts and for smooth finishing to close tolerance. Tools should have a positive rake angle. Drilling: Steady feed rates must be used to avoid work hardening due to dwelling of the drill on the metal. Rigid set-ups are essential with as short a stub drill as feasible. Heavy-duty, high-speed steel drills with a heavy web are recommended. Feeds vary from 0.0007 inch per rev. for holes of less than 1/16" diameter, 0.003 inch per rev. for 1/4" dia., to 0.010 inch per rev. for holes of 7/8"diameter. Milling: To obtain good accuracy and a smooth finish it is essential to have rigid machines and fixtures and sharp cutting tools. High-speed steel cutters such as M-2 or M-10 work best with cutting speeds of 30-40 feet per minute and feed of 0.004"-0.006" per cutting tooth. Grinding: The alloy should be wet ground and aluminum oxide wheels or belts are preferred.r 1/4" dia., t0 degrees to the joint. For Short-Circuiting-Transfer GMAW a typical voltage is 18-22 with a current of 75-150 amps and a wire feed of 8-10 inches per minute. Submerged-Arc Welding: Generally submerged-arc welding should be avoided. This weld process involves high heat input and may lead to cracking of the alloy workpiece.

Principle Design Features

This is a cobalt-nickel-chromium-tungsten alloy designed for high temperature strength and resistance to oxidation at temperatures up to 2000 F(1095 C).

Weldability

This alloy can be readily welded using MIG, TIG, electron beam and resistance techniques.

Known Forms

Coil

Coil

Disc

Disc

Flat Bar

Flat Bar

Foil

Foil

Hollow Bar

Hollow Bar

Pipe

Pipe

Plate

Plate

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Strip

Strip

Additional Data

Specifications

5608,5772,B50A712,B50TF74,B50TF74A,1042,R330188

Chemical Elements

Boron0.015 nom
Carbon0.05 - 0.15
Chromium20 - 24
CobaltBalance
Iron3 max
Lanthium0.02 - 0.12
Manganese1.25 max
Nickel20 - 24
Silicon0.2 - 0.5
Tungsten13 - 15

Physical Properties

Density: 0.324lb/in³Density

Electrical Resistivity: 554µΩ·cmElectrical Resistivity

Melting Point: 2425°FMelting Point

Specific Gravity: 8.97Specific Gravity

Specific Heat: 0.101BTU/lb·°FSpecific Heat

Mechanical Properties

Modulus of Elasticity – Tension: 33.6MSIModulus of Elasticity – Tension

Thermal Conductivity

ConditionTemperatureConductivity
Annealed70 °F7.2 BTU/hr·ft·°F

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed70 °F200 °F6.5 μin/in·°F
Annealed70 °F400 °F7 μin/in·°F
Annealed70 °F800 °F7.7 μin/in·°F
Annealed70 °F1000 °F8.2 μin/in·°F
Annealed70 °F1400 °F9 μin/in·°F
Annealed70 °F1800 °F9.9 μin/in·°F
Annealed70 °F2000 °F10.2 μin/in·°F

Rupture Test Data

ConditionFormTemperatureTimeRupture Strength
Solution AnnealedSheet1600 °F100 hrs15 KSI
Solution AnnealedSheet1400 °F100 hrs33 KSI

Mechanical Test Data

FormSheet
ConditionSolution Annealed
Temperature70°F
Elongation56%
Tensile Strength139 KSI
Yield Strength70 KSI
FormSheet
ConditionSolution Annealed
Temperature1200°F
Elongation61%
Tensile Strength103 KSI
Yield Strength44 KSI
FormSheet
ConditionSolution Annealed
Temperature1400°F
Elongation43%
Tensile Strength92 KSI
Yield Strength42 KSI
FormSheet
ConditionSolution Annealed
Temperature1600°F
Elongation73%
Tensile Strength61 KSI
Yield Strength38 KSI
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