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Superalloy Castings Hot Isostatic Pressing Supplier

Table of Contents
Trusted HIP Processing for High-Performance Superalloy Castings
What HIP Achieves in Superalloy Casting
Superalloys Commonly Processed by HIP
Case Study: HIP of Inconel 713C Turbine Nozzle Castings
Project Background
Typical HIP-Processed Components and Industries
HIP Benefits for Cast Superalloy Components
HIP Processing Standards and Parameters
Results and Verification
HIP Execution
Post-HIP Processing
Inspection
FAQs

Trusted HIP Processing for High-Performance Superalloy Castings

Hot Isostatic Pressing (HIP) is an essential post-casting process for high-temperature superalloy castings used in aerospace, power generation, and industrial gas turbine applications. By applying high pressure and temperature in an inert atmosphere, HIP eliminates internal porosity, heals microshrinkage, and enhances fatigue life—making cast components more robust and inspection-ready.

Neway AeroTech is a specialized HIP supplier for superalloy parts made from Inconel, Rene alloys, Hastelloy, and CMSX single crystal materials. Our HIP service supports investment castings, welded repairs, and pre-machined components in compliance with AMS 2774 and aerospace OEM standards.

superalloy-castings-hot-isostatic-pressing-supplier

What HIP Achieves in Superalloy Casting

HIP restores casting quality by improving density, microstructure, and high-temperature fatigue resistance—essential for blades, vanes, combustors, and seals.

  • Removes internal voids and microporosity caused during cooling in vacuum investment casting

  • Increases fatigue and creep life under sustained thermal cycling

  • **Supports post-HIP machining and TIG welding without deformation

  • Prepares surfaces for better coating adhesion and dimensional control

HIP is typically performed before heat treatment and final CNC machining.

Superalloys Commonly Processed by HIP

Alloy

Max Temp (°C)

HIP Temp (°C)

Application

Inconel 713C

950

1210

Nozzle segments, blade castings

Rene 80

1050

1230

Turbine blades, vane shrouds

Hastelloy X

1175

1170

Combustion cases, support rings

CMSX-4

1140

1260

Single crystal turbine airfoils

All HIP cycles are customized to OEM alloy specifications and casting geometry.

Case Study: HIP of Inconel 713C Turbine Nozzle Castings

Project Background

A client submitted 240 equiaxed Inconel 713C nozzle segments for HIP. Each part was 8 mm thick with complex cooling channels. HIP was performed at 1210°C, 100 MPa for 4 hours. X-ray and SEM confirmed full porosity elimination, and parts passed ultrasonic testing and CMM dimensional inspection.

Typical HIP-Processed Components and Industries

Component Model

Description

Alloy

Industry

NGV-310

Nozzle guide vane with film cooling

Rene 80

Power Generation

HPC-400

Combustor casing with integral flange

Hastelloy X

Energy

BLD-710

First-stage blade with 25 mm fir-tree root

CMSX-4

Aerospace

EXH-580

Exhaust vane with cross-ribbed structure

Inconel 713C

Oil and Gas

All parts were HIPed, heat-treated, machined, and coated for service at ≥950°C.

HIP Benefits for Cast Superalloy Components

  1. Eliminates >99% of porosity, improving ultrasonic inspection and high-cycle fatigue resistance

  2. Prevents crack propagation by healing microvoids and closing shrinkage cavities at grain boundaries

  3. Enhances dimensional stability, critical for post-HIP CNC finishing

  4. Improves bond strength of downstream TBC coatings

  5. Restores weld-repaired parts, enabling extended turbine component service life

HIP Processing Standards and Parameters

  1. HIP temperature range: 1170–1300°C, depending on alloy composition

  2. Pressure range: 100–200 MPa in argon, fully enclosed chamber

  3. Cycle duration: 2–6 hours based on wall thickness and porosity levels

  4. Cooling rate: ≤10°C/min to avoid residual stress and distortion

  5. **Inspection: X-ray, SEM, CMM after HIP to confirm effectiveness

Results and Verification

HIP Execution

Parts were HIPed at 1210°C and 100 MPa for 4 hours. Cooling was controlled at 5°C/min to prevent overaging or cracking.

Post-HIP Processing

Blades and vanes underwent heat treatment per AMS 5662, followed by CNC machining and optional TBC coating depending on end-use application.

Inspection

X-ray inspection verified full porosity closure. CMM confirmed profile tolerances within ±0.008 mm. SEM analysis validated grain integrity and void elimination.

FAQs

  1. Which superalloy grades benefit most from HIP treatment?

  2. Is HIP mandatory before machining or welding turbine parts?

  3. What quality standards are used to validate HIP effectiveness?

  4. Can you perform HIP on single crystal, equiaxed, and welded components?

  5. What is the typical turnaround time for HIP processing?