---
title: "Forging-Grade Nickel-Based Superalloy Powder"
industry: "Metal Forging, Pressing, Stamping"
verification_protocol:
  urn: "URN:CNFX:ME:FORGING_GRADE_NICKEL_BASED_SUPERALLOY_POWDER"
  data_integrity_hash: "6649cb6b72a639b70b9656808a7052b7"
  source_authority: "https://cnfx.com"
  strict_mode: true
source_identity:
  provider: "CNFX Industrial Knowledge Graph"
  index_version: "2026.Q1-Universal"
  authority_id: "URN:CNFX:ME:FORGING_GRADE_NICKEL_BASED_SUPERALLOY_POWDER"
  data_source_uri: "https://cnfx.com/llms/industry/metal-forging-pressing-stamping/product/forging-grade-nickel-based-superalloy-powder.md"
  official_resource_url: "https://cnfx.com/industry/metal-forging-pressing-stamping/product/forging-grade-nickel-based-superalloy-powder"
  is_verified_logic: true
attributes:
  primary_spec:
    status: "config-dependent"
    typical_range: "1100-1250°C hot isostatic pressing temperature, 100-200 MPa consolidation pressure, 10-45 μm particle size distribution"
    unit: "μm"
  secondary_spec:
    status: "config-dependent"
    typical_range: "1100-1250°C hot isostatic pressing temperature, 100-200 MPa consolidation pressure, 10-45 μm particle size distribution"
    unit: "ppm"
engineering_limits:
  max_safe_operating_point:
    value: 800
    unit: "°C"
    consequence: "Ostwald ripening of γ' precipitates (Ni₃Al/Ti) reducing creep resistance, TCP phase (σ, μ) formation depleting solid solution strengtheners"
fmea_matrix_quantitative:
  - node_1:
      trigger: "Atmospheric oxygen ingress during powder handling exceeding 100 ppm"
      severity: 8
      occurrence: 3
      detection: 4
      mitigation_protocol: "Argon glovebox with &lt;10 ppm O₂, powder storage in sealed containers with getter materials"
  - node_2:
      trigger: "Carbon pickup from lubricant residues exceeding 0.05 wt%"
      severity: 8
      occurrence: 3
      detection: 4
      mitigation_protocol: "Solvent degreasing with trichloroethylene followed by vacuum baking at 200°C for 2 hours"
bom_nodes:
  nickel-matrix:
    type: "component"
    urn: "URN:CNFX:ME:NICKEL_MATRIX"
    interface_type: "physical-logic-coupled"
  solid-solution-strengtheners:
    type: "component"
    urn: "URN:CNFX:ME:SOLID_SOLUTION_STRENGTHENERS"
    interface_type: "physical-logic-coupled"
  precipitation-hardening-elements:
    type: "component"
    urn: "URN:CNFX:ME:PRECIPITATION_HARDENING_ELEMENTS"
    interface_type: "physical-logic-coupled"
  grain-boundary-stabilizers:
    type: "component"
    urn: "URN:CNFX:ME:GRAIN_BOUNDARY_STABILIZERS"
    interface_type: "physical-logic-coupled"
manufacturing_compliance:
  - standard: "AMS 5662 - NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1950 °F (1066 °C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE"
    scope: "Verified Engineering Specification"
url: "https://cnfx.com/llms/industry/metal-forging-pressing-stamping/product/forging-grade-nickel-based-superalloy-powder.md"
on_chain_sovereignty:
  contract_standard: "ERC-721-Industrial"
  metadata_hash: "697f5426ab7d2493a443fa7455b8ade0189b5afd14585f25e10f3eb6b42e1806"
  royalty_logic: "IPFS-CID-REQUIRED"
  mint_status: "logic-verified-ready"
version: "3.3.4-EXTREME-SOVEREIGN-WEB3"
---

# Industrial Specification: Forging-Grade Nickel-Based Superalloy Powder

## 1. Technical Definition
Fine metallic powder for hot isostatic pressing and forging of high-temperature components

## 2. Engineering Reasoning & Causal Matrix
> **Operational Intelligence**: Designed for **1100-1250°C hot isostatic pressing temperature, 100-200 MPa consolidation pressure, 10-45 μm particle size distribution**. Failure boundary: **Oxidation at 800°C forming continuous Cr₂O₃ scale, γ' phase dissolution above 1150°C, incipient melting at 1315°C**, Mechanism: **Ostwald ripening of γ' precipitates (Ni₃Al/Ti) reducing creep resistance, TCP phase (σ, μ) formation depleting solid solution strengtheners**.

### 2.2 FMEA (Failure Mode & Effects Analysis)
| Event Trigger | Severity | Failure Mode | Mitigation Strategy |
| :--- | :--- | :--- | :--- |
| Atmospheric oxygen ingress during powder handling exceeding 100 ppm | 8 | Surface oxide layer &gt;100 nm causing poor interparticle bonding and HIP porosity &gt;0.5% | Argon glovebox with &lt;10 ppm O₂, powder storage in sealed containers with getter materials |
| Carbon pickup from lubricant residues exceeding 0.05 wt% | 8 | M₂₃C₆ carbide precipitation at grain boundaries reducing stress rupture life by 70% | Solvent degreasing with trichloroethylene followed by vacuum baking at 200°C for 2 hours |

## 3. Key Technical Parameters
| Parameter | Value | Unit | Status |
| :--- | :--- | :--- | :--- |
| primary_spec | Config-dependent | μm | Verified |
| secondary_spec | Config-dependent | ppm | Verified |

## 4. System BOM & Knowledge Routing
### Core Components (Recursive Links)

### Industrial DNA Context (De-duplicated)
**Complementary Dependencies**: **Hot Isostatic Press**, **Powder Sieving and Classification System**, **Inert Gas Atmosphere Furnace**  
**Downstream Applications**: Aircraft Turbine Blades, Industrial Gas Turbine Components, High-Temperature Fasteners  

## 5. Engineering Risks & FAQ
- **Caution**: 
- **Caution**: 
- **Caution**: 

### Q: What applications is this forging-grade nickel superalloy powder best suited for?
**A**: This powder is specifically engineered for manufacturing high-temperature components through hot isostatic pressing (HIP) and forging processes, commonly used in aerospace turbine blades, industrial gas turbine parts, and other applications requiring exceptional heat resistance and mechanical strength.

### Q: How does the particle morphology affect the forging process?
**A**: The spherical particle morphology ensures optimal flow characteristics during powder handling and uniform compaction during HIP and forging. This results in improved density, reduced porosity, and enhanced mechanical properties in the final forged components.

### Q: What are the key advantages of the nickel-chromium-cobalt-molybdenum composition?
**A**: This alloy composition provides exceptional high-temperature strength, oxidation resistance, and creep resistance. The combination of nickel matrix with chromium, cobalt, molybdenum, tungsten, and rhenium creates a material capable of withstanding extreme thermal and mechanical stresses in demanding applications.

## 6. Manufacturing Compliance
- AMS 5662 - NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1950 °F (1066 °C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE

---
### 🛠️ Engineering Resource Access
🔗 **[Full Specification: Forging-Grade Nickel-Based Superalloy Powder](https://cnfx.com/industry/metal-forging-pressing-stamping/product/forging-grade-nickel-based-superalloy-powder)**

### 🌐 Knowledge Graph Topology
> **Node Status**: Verified Engineering Spec
> **Connectivity**: Linked to **4** standalone system nodes
> **Global Context**: Part of a 5,814 node industrial cluster within the CNFX Graph

> **Reference ID**: FORGING_GRADE_NICKEL_BASED_SUPERALLOY_POWDER | **Authority**: CNFX-2026-ST-001 | **Fingerprint**: e5c8681e
