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CoCr22Ni22W14 · UNS R301882.4683 · Alloy 188 / Haynes 188

Cobalt-base sheet — combustors and afterburner cans, 1100 °C class

HaynesCobalt superalloys
Units
Tensile Rm
862
MPa · ≥ std. min
Yield Rp0.2
379
MPa · ≥ std. min
Elongation A
45
% · ≥ std. min
Service limit
1100
°C · indicative max
Density
8.98
g/cm³

Chemical composition

Co 38%Cr 22%Ni 22%W 15%Si 0.35%C 0.10%La 0.07%Minor & residual 3%

Nominal: mid-range where both limits are given, the cap where only a maximum is, balance takes the remainder. Exact specified ranges below.

ElementName Content %
Main elements7 elements
Co CobaltBal.
Cr Chromium20 – 24%
Ni Nickel20 – 24%
W Tungsten13 – 16%
Si Silicon0.2 – 0.5%
C Carbon0.05 – 0.15%
La Lanthanum0.02 – 0.12%
ElementName Content %
Minor & residual2 elements
Fe Iron≤ 3%
B Boron≤ 0.015%

Mechanical minima by form

Guaranteed values differ by form, size and delivery condition; quotations confirm the specification, form, size and condition.

FormCondition Rm MPaRp0.2 MPaA ≥ %Other requirements and notes
Bar and forgings
Bar, forgings and flash-welded ringsSolution treated at 1177 ± 14 °C ≥ 862 (125 ksi) ≥ 379 (55 ksi) ≥ 45 Also specified: Hardness ≤ 302 HBW / 32 HRC
Plate, sheet and strip
Plate, sheet and strip (over 0.51 mm)Solution treated at 1163-1232 °C, air cooled or faster ≥ 862 (125 ksi) ≥ 379 (55 ksi) ≥ 45
Sheet and strip (>0.25-0.51 mm)Solution treated at 1163-1232 °C, air cooled or faster ≥ 862 (125 ksi) ≥ 379 (55 ksi) ≥ 40
Foil and ultra-thin sheet (≤0.25 mm)Solution treated at 1163-1232 °C, air cooled or faster ≥ 862 (125 ksi) ≥ 379 (55 ksi) —
Plate, sheet and strip over 0.51 mm — elevated-temperature tensileTested at 649 ± 3 °C, held at least 20 min ≥ 621 (90 ksi) ≥ 248 (36 ksi) ≥ 50

Where this grade is recommended

Matched in 3 service conditions; ranks and scores computed from the condition-scoring matrix.

Service conditionIndustry TemperatureRankScore
Exhaust & afterburner Aerospace 700 – 950 °C 1 / 8 93
Engine hot section Aerospace 650 – 900 °C 4 / 9 89
Gas-turbine hot section Power & Nuclear 800 – 950 °C 3 / 10 88

Designations & equivalents

W.Nr. (Germany)2.4683
EN designationCoCr22Ni22W14
Trade name(s)Haynes 188
AMS (SAE aerospace)5608 / 5772 / 5801

Cross-references are common near-equivalents for search and shortlisting; substitution across standards requires clause-by-clause verification. All grades in one cross-reference table →

Applicable standards

3 specifications. Name the standard and its edition on the order.

Guaranteed values and required tests differ between specifications — see Mechanical minima by form for the figures per form.

Frequently asked questions

What is Alloy 188 · UNS R30188?

Alloy 188 · UNS R30188 — Cobalt superalloys. Cobalt-base sheet — combustors and afterburner cans, 1100 °C class

What is the maximum service temperature of R30188?

Typically about 1100 °C; the practical limit depends on media, stress and design life — acceptance per the governing standard.

What is the tensile strength of R30188?

The specified minimum tensile strength is 862 MPa for the main product form. Minima for other forms and sizes are listed under "Mechanical minima by form" on this page.

Which standards cover R30188?

SAE AMS5608 HS188 UNS R30188, SAE AMS5772 HS188 UNS R30188, SAE AMS5801 HS188

Where is R30188 typically used?

Exhaust & afterburner (Aerospace); Engine hot section (Aerospace); Gas-turbine hot section (Power & Nuclear)

In which forms is R30188 available?

Tube, plate, strip, bar, forgings, wire and other forms — sizes and delivery condition confirmed per order, with EN 10204 3.1 / 3.2 certification.

Same series

Download PDF datasheet

This grade’s datasheet as an A4 PDF — for filing, printing or forwarding to colleagues.

Download PDF datasheet

Supply & enquiry

Tube & pipeφ1 – 219 × 0.25 – 25 mmPlate4.76 – 80 mmBarφ8 – 300 mmWire & filler metalsφ0.01 – 8 mm

For this grade we can supply, against your service conditions:

Or email us: info@kochlin.com