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Aerocoreparts

Variable Inlet Guide Vane Case

Variable Inlet Guide Vane Case

Regular price $7,200.00
Regular price Sale price $7,200.00
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The Variable Inlet Guide Vane Case is a critical component in modern turbofan engines, enabling dynamic control of inlet airflow by adjusting the angle of guide vanes. This advanced design optimizes aerodynamic performance across different flight conditions—takeoff, climb, cruise—enhancing engine efficiency, fuel economy, and stability.

📦Sample Information

  • Sample Material: 1Cr11Ni2MoV
  • Overall Dimensions: Diameter 800 mm  × Height 240 mm

📢 Important Notice

✓ This product is only available for production upon customer-supplied drawings or physical samples, and First Article Inspection (FAI) is required for confirmation.
✓ Sample production lead time: 5–7 working days
✓ Estimated shipping time: 3–7 days via air freight
✓ Delivery contents include: Finished parts, FAIR (First Article Inspection Report), Raw Material Certificates, Production Records, Inspection Records, Test Certificates, Shipping Documents, and complimentary items (if applicable)

🏗️ Technical Features

  • High-Temperature Strength Alloys
    Manufactured from nickel-based or titanium-based superalloys (e.g., Ti-6Al-4V, Inconel 718) to ensure structural integrity and prolonged service life under extreme operating environments.
    Compliance with AMS 4928 / AMS 5662 aerospace material standards.
  • Precision Forging & Heat Treatment
    Advanced precision forging and uniform heat treatment processes provide high material density, superior fatigue strength, and minimal stress concentration.
  • Complex Geometry Optimization
    Designed using 3D CAD/CAE modeling, the guide vane profiles and case geometry achieve an ideal balance between lightweight construction and aerodynamic performance.
  • Surface Enhancement Technologies
    Optional treatments such as laser cladding, nitriding, and ceramic coatings are available to improve corrosion and wear resistance under prolonged service.
  • Integrated Multistage Blade Design
    Supports multi-stage integrated vane architecture, enhancing engine power transmission stability and reducing vibration during high-speed operation.

🚀 Application Fields

  • Manufacturing of compressor and turbine disks for civil aircraft gas turbine engines
  • Core structural components for commercial and general aviation engines
  • R&D and serial production of next-generation high-performance aero engines
  • Engine maintenance, overhaul, and performance upgrade services
  • High-precision parts for aero engine performance validation and testing

🌍 Reference Applications

Engine Platform Application Role Key Performance Contributions
CFM LEAP-1A/B Inlet guide vane flow control structure Enhanced surge margin, better fuel burn efficiency
PW1100G-JM (GTF) Integrated adjustable inlet vane assembly Controls fan/compressor matching at low N1 speeds
GE Passport / GE9X Pre-compression airflow channeling Supports extreme bypass ratio and thermal margin
Chinese AECC Engines Domestic VIGV localization and substitution Ensures secure supply chain and aerodynamic tuning
MRO Centers (Global) Replacement or re-manufacturing of VIGV parts Extends engine life and reduces overhaul cost


🛡️ Quality Control Process

Certified to NADCAP / AS9100 / ISO 9001 standards

1️⃣ Raw Material Control

Key Control Points (KCP): Material Traceability / CoC

  • Materials sourced only from ASL-certified suppliers, with full heat number traceability
  • Accompanied by Mill Test Reports (MTRs), complying with AMS material standards
  • Incoming inspection includes chemical composition and mechanical properties validation

2️⃣ Process Control

KCP: Process Validation / Work Instructions / Special Process Oversight

  • All steps follow validated Process Flow Charts (PFCs) and detailed Work Instructions (WIs)
  • CAM toolpaths verified through simulation tools such as Mastercam and Siemens NX
  • Special processes performed by NADCAP-accredited subcontractors

3️⃣ First Article & In-Process Inspection

KCP: AS9102 FAI / SPC

  • First Article Inspection per AS9102 Rev. B
  • Statistical Process Control (SPC) applied to Critical-to-Quality (CTQ) features
  • CMM and measuring tools calibrated and traceable to national standards

4️⃣ Functional & Performance Testing

KCP: Test Plan / Acceptance Criteria

  • For rotating parts, dynamic rotor balancing and vibration tests are conducted
  • Mechanical testing includes tensile strength and fatigue evaluation
  • Blade profiles measured for aerodynamic accuracy

5️⃣ Special Process Management

KCP: NADCAP Accreditation / Operator Qualification

  • All special processes (e.g., EB welding, thermal barrier coating) handled by qualified partners
  • Each process is documented with Process Approval Records and Operator Certifications

6️⃣ Final Inspection

KCP: Dimensional & Surface Quality Check

  • Full dimensional inspection via CMM with CAD-based 3D models
  • Surface finish ≤ Ra 0.8μm, edge break radius verified
  • Certificate of Conformance (CoC) issued with shipment

7️⃣ Documentation & Traceability

KCP: Serial Number Tracking / Record Retention

  • Each VIGV case is uniquely identified with a serial number for full traceability
  • Documentation includes: Process Routers, QC Reports, MTRs, Test Results
  • All records are stored for minimum 10 years, in compliance with AS9100 Clause 7.5

Compliance Summary

Standard / System Key Requirements Met Status
ISO 9001:2015 Quality planning, continuous improvement, documentation ✅ Fully Compliant
AS9100D Aerospace QMS, FAI, risk-based thinking, traceability ✅ Fully Compliant
NADCAP (if applicable) Special process control (e.g., heat treat, coating, welding) ✅ Via Certified Partners
Customer Audit Checklist Full support for gap analysis, documentation mapping, and audit readiness ✅ Supported

 

We can prepare complete product documentation and quality-related files in accordance with specific customer requirements.

Sample, No Commercial Value, Not for Resale.

Send us your drawings or sample information via email, and we will reply within 24 hours!    Sales@aerocoreparts.com

FAQ

Q1:What is a Variable Inlet Guide Vane (VIGV) Case?

A1:A Variable Inlet Guide Vane (VIGV) Case is a front-end structural component of an aero engine that incorporates adjustable guide vanes to control the angle and pressure of incoming airflow before it reaches the compressor. This mechanism helps improve engine efficiency, prevents compressor stall, and optimizes performance across varying flight conditions.

Q2. What materials are used to manufacture VIGV cases?

A2:VIGV cases are typically made from high-performance aerospace alloys such as Ti-6Al-4V and Inconel 718, ensuring excellent strength and thermal resistance. All materials are sourced from ASL-certified suppliers and comply with standards like AMS 4928 and AMS 5662, with full heat lot traceability and Mill Test Reports (MTRs).

Q3. How do you ensure the quality of each VIGV case?

A3:Our VIGV cases undergo a comprehensive quality assurance process, including:

  • AS9102-compliant First Article Inspection (FAI)
  • Full dimensional verification using CMM and CAD-based inspection
  • Surface roughness checks (Ra ≤ 0.8μm)
  • Dynamic balance and vibration testing (if applicable)
    All steps are performed under AS9100D and NADCAP certified processes with full traceability documentation retained for at least 10 years.
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