| Parameter | Value |
| Operating temperature | 800–2,000 °C (typically 1,100–1,250 °C for steels) |
| Operating pressure | 100–200 MPa (isostatic) |
| Working medium | Argon (inert atmosphere) |
| Achievable density | ≥ 99.9% of the theoretical value |
| Dimensional change after HIP | depending on the porosity of the input material |
| Cycle duration | 8–24 hours (including heating and controlled cooling) |
| Equipment | Quintus QIH 21 (in-house) |
| Material compatibility | Steels, titanium, nickel/cobalt superalloys, ceramics, cermets |
| PM HIP – maximum part weight | depending on the equipment |
| Heat treatment in a cycle | Possible (combined HIP cycle and others) |
| Process certification | AMS 2801, AMS 7000, ASTM F3122, EN 9100 |
| Batch traceability | From raw material to HIP cycle report |
HIP – Hot Isostatic Pressing
Isostatic hot pressing – elimination of porosity, maximum material density.
Comparison table – HIP vs. the main alternatives
| Parameter | HIP (completion) | PM HIP | Standard TZ | Fittings | Impregnation |
| Sealing of internal pores | yes | Yes | no | no | surface only |
| Improvement in fatigue strength | +300–400 % | high | no | medium | no |
| Isotropy of properties | absolute | absolute | high | medium | no |
| Geometric stability | depending on the porosity of the input material | Near-net shape | yes | machining required | yes |
| Material utilisation | ~90 % | ~90 % | ~100% | ~60–70 % | ~100 % |
| Tolerance | ±0.1% | ±0.1% | - | ±0.5 % | - |
| Suitability for ceramics / cermets | yes | no | no | no | no |
| Achievable density | ≥ 99.9% | ≥ 99.9% | 95–98 % | 99%+ | ~95% (surface) |
| Max. part weight | depending on the equipment | depending on the machine | unlimited | unlimited | unlimited |
Why Vibrom?
Our own Quintus QIH 21 HIP equipment – in-house
We carry out isostatic hot pressing in-house, using our own industrial equipment. The customer does not need to worry about finding an external partner or arranging the transport of parts to a third party. Delivery times are under our control.
The complete MIM → HIP process chain
For customers who have us manufacture MIM parts, HIP is a natural next step requiring no external collaboration. We take full responsibility for the final part – from the feedstock through to the HIP protocol and the final certificate.
Certified cycles and the development of custom parameters
We work with certified HIP cycles in accordance with AMS and ASTM standards. At the same time, we develop our own sets of parameters for non-standard alloys in collaboration with research institutions – including the Czech Academy of Sciences.
Defectoscopy and full batch documentation
Each batch is documented: temperature and pressure logs, dimensional measurements before and after processing, and metallographic analysis of a representative sample. For aerospace and medical applications, we carry out X-ray or ultrasonic non-destructive testing as a standard part of the process.
ISO 9001
Traceability from the batch of input material through to dispatch. The quality management system covers the entire process chain. Every component is identifiable throughout the entire manufacturing process.
Design to cost
We are involved in the design of the part to eliminate unnecessary costs even before the mould is manufactured. Changing the geometry in a PDF is inexpensive; changing it in the mould is not.
What you might find interesting about HIP
HIP is economically viable when internal porosity significantly affects the performance or reliability of a component. Typical examples include: components subjected to cyclic or dynamic loading (fatigue), components for the aerospace or medical industries, and castings made from superalloys or titanium alloys.
CIP operates at room temperature and is used to compact powders prior to sintering – it is a forming process, not a method of eliminating internal porosity. HIP combines heat and pressure to seal defects by diffusion – it is applied to parts that have already been sintered or cast.
Yes. The combined HIP cycle (HIP + solution annealing + ageing) is the standard approach in the aerospace industry. It saves one heat treatment and ensures uniform properties throughout the entire component.