Aero-Engine High-Temperature Alloy Structural Components
Product Description
High-temperature alloy casings and hot-section structural parts for compact turbojet engines (TJ-378 series), precision-machined to aviation-grade dimensional tolerances.
Product Features
- TJ-378 compact turbojet engine application
- Casing tolerance φ147 ± 1 mm
- High-temperature alloy CNC machining
- Custom drawing-based production
Our aero-engine high-temperature alloy structural components are manufactured from premium aerospace-grade heat-resistant alloys and processed by high-precision CNC machining. Designed for compact turbojet engine applications, all products undergo strict dimensional inspection, high-temperature resistance testing and mechanical fatigue testing to meet aviation industry standards.
Reference Application — Compact Turbojet Engine (TJ-378)
| Overall Length | 378 ± 1.5 mm |
|---|---|
| Main Casing Length | 285 ± 1 mm |
| Casing Diameter | φ147 ± 1 mm |
| Exhaust Diameter | φ71.5 ± 0.3 mm |
These components are widely used in turbojet engine main assemblies and high-temperature working sections, supporting stable long-term operation under extreme thermal conditions. Custom manufacturing based on customer drawings is supported.