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How Inconel 718 works: a practical explanation

Inconel 718 is a nickel chromium super alloy that holds strength at high temperature It is used for turbine, downhole and high temperature parts where creep and oxidation set the limit. Typical values: tensile strength 1

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How Inconel 718 works: a practical explanation

How Inconel 718 works: a practical explanation

Source:Product Encyclopedia / Time:2026-09-16

How Inconel 718 works: a practical explanation

Inconel 718 is a nickel chromium super alloy that holds strength at high temperature. It is used for turbine, downhole and high temperature parts where creep and oxidation set the limit. This entry explains what it is, what the numbers on a data sheet mean, and what to put on a drawing.

It is written from the point of view of the buyer and the drawing office: the values that are realistic in production, the ones that cost money, and the way the result is verified. Where an industry sets the requirement, oil and gas is used as the example: materials that work harden and still have to be certified.

How it works, step by step

  1. The part or the material is prepared, and the datum features are established.
  2. Inconel 718 is applied under the parameters below, with the result checked against the drawing.
  3. The measured value is fed back as an adjustment, so the next part starts from a known condition.
  4. The finished work is inspected and documented: dimensional inspection with a certificate review.

The numbers that matter

SpecificationTypical value
Tensile strength1,275 MPa aged
Yield strength1,035 MPa aged
Hardness35 to 40 HRC
Density8.19 g/cm³
Machinabilityvery poor: it work hardens and cuts at high pressure
Service temperatureup to 650 °C

Where it stops working

Every process has a limit, and for Inconel 718 the practical one is cost. Tool consumption and cutting time, so a specification that pushes past it is usually a specification that should be written differently.

Inconel 718 – application detail

Applications

Inconel 718 is used for turbine, downhole and high temperature parts where creep and oxidation set the limit, and in practice it appears most often in turbine components, downhole tools, exhaust hardware, high temperature fasteners.

How it fits into a machining route

Inconel 718 is chosen at the drawing stage, and everything downstream follows from it: the tool geometry, the cutting data, the heat treatment and the certificate. Changing the grade later is a different part, not a different quote.

The route is fixed before the first part is cut, and it is the route rather than the individual setting that holds the result: tool consumption and cutting time. Where a drawing calls for something the route cannot hold economically, that is raised at quotation rather than after the parts are made.

Standards, documentation and what is issued

The documentation requirement is EN 10204 3.1 with a full melt trace. Material is supplied against a certificate where the application calls for it, inspection results are recorded with the job, and the records are kept so that a repeat order can be compared with the first instead of being measured from scratch.

Dimensional inspection with a certificate review is the verification step. Where a customer format or a standard report is required, it is agreed before the batch starts, because a report written after the event is a report nobody can use.

Frequently asked questions

What tolerance should be specified for Inconel 718?

±0.02 mm is realistic in production. Tightening it beyond the functional requirement increases cost without improving the part.

Which material is usually used?

Inconel 718 is the usual choice, supplied against EN 10204 3.1 with a full melt trace.

How is the result verified?

Dimensional inspection with a certificate review, with the results recorded so a repeat order can be compared with the first.

What is the most common mistake?

Planning a lead time as if it were steel.

How long does it take and what does it cost?

A realistic cycle is very slow cutting, a small number of parts per tool, and the cost driver is tool consumption and cutting time.

Inconel 718 – inspection and packing

Related capability

If you are specifying Inconel 718 on a drawing and want a second opinion on the route, send the model and the quantity. The first response is a manufacturability review with the likely risk points and a quotation, so the decision can be made on facts rather than on a price alone.

Machining, inspection and documentation are handled in one place, which is why the dimensional report and the material certificate arrive with the parts rather than after them.

Related entries

These entries sit next to Inconel 718 in the encyclopedia: C3604 Brass, Duplex 2205 Stainless Steel, Bearing Housings. Reading them together gives a fuller picture of how the process, the material and the measurement affect each other.