Material Haynes 75

Technical Reference Library

Haynes 75

Form Wrought Type Ni-Cr Solid-Solution UNS N06075

Material Overview

Haynes 75 is a trade name for the 80/20 nickel-chromium solid-solution alloy also widely known as Nimonic 75 — the two names refer to essentially the same material. Like Haynes 600, it relies on solid-solution strengthening rather than gamma-prime hardening, but Haynes 75 carries no significant iron or molybdenum addition; it is a comparatively simple nickel-chromium alloy with small, controlled additions of titanium and carbon to refine grain structure and stabilize carbides.

The result is a moderate-strength alloy (usable to roughly 1200°F / 650°C) with excellent oxidation and scaling resistance and very good fabricability — it forms, welds, and machines more predictably than higher-alloyed superalloys. It is most commonly supplied and used as sheet for fabricated components: combustion chambers, flame tubes, furnace fixtures, heat-treatment equipment, and other parts that need to hold up to repeated thermal cycling in oxidizing atmospheres without carrying heavy mechanical load.

International Designation Equivalents

Standard Designation
UNS N06075
Other Trade Names Nimonic 75, Alloy 75

Published sources disagree on the Werkstoff number for this alloy (2.4630 and 2.4951 both appear across suppliers) — rather than publish a possibly-wrong figure, it has been omitted here pending a single authoritative source.

Chemical Composition

Element Content
Nickel (Ni) Balance (~76%)
Chromium (Cr) 20.0%
Iron (Fe) 5.0% max
Carbon (C) 0.11%
Titanium (Ti) 0.4%
Aluminum (Al) 0.4% max
Cobalt (Co) 1.0% max
Manganese (Mn) 1.0% max
Silicon (Si) 1.0% max

Nominal values from published alloy datasheets. These are close to, and confirm, the figures on the old page for this material.

Machinability Explained

Haynes 75 is among the more machinable alloys in the nickel superalloy family, since it carries no gamma-prime hardening and only a modest 20% chromium content — there is no abrasive precipitate structure and comparatively little solid-solution hardening compared to higher-chromium grades like Haynes 690. Even so, it shares the fundamental nickel-alloy machining constraints: thermal conductivity is low, so cutting heat concentrates at the tool edge rather than dissipating into the chip, and the alloy work-hardens under mechanical deformation from the cutting action itself.

Because the alloy is soft, tough, and ductile in its typical mill-annealed sheet condition, chip control and built-up edge are often the more practical challenges rather than raw tool wear — long, stringy chips and galling against the cutting edge are common if speeds or feeds are mismatched to the tool geometry. Sharp, positive-rake cutting edges, consistent chip loads to avoid dwelling in the deformation zone, and adequate coolant are the standard approach, with somewhat more latitude on speed than the higher-alloyed, higher-chromium grades in this family.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 60 – 180 200 – 590
Milling 45 – 135 150 – 440
Parting 40 – 115 130 – 380
Grooving 55 – 160 180 – 520
Drilling 55 – 160 180 – 520

General starting-point ranges for heat-resistant Ni/Co-based alloys. Actual optimal speeds depend on tool grade, coating, rigidity, and coolant strategy.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 - S10
FM2533 CVD S15

Parting / Grooving

Grade Operation Coating ISO Application Range
FM2543 Parting CVD S20
FM2553 Parting CVD S30
FM2533 Grooving CVD S10

Milling

Grade Coating ISO Application Range
FM125 PVD S15 - S35

Ready to cut Haynes 75? Shop FM Carbide inserts engineered for nickel-chromium solid-solution alloys.

Shop Turning & Grooving Inserts Shop Milling Inserts

Recommended Insert Cutting-Edge Geometry

Parameter Value
Honing Size 0.02-0.05 mm / 0.001-0.002"
Rake Angle 13° - 18°
Land Angle Neutral
Land Width 0.10-0.20 mm / 0.004-0.008"
Ground Insert Recommended