Compressor rotor (400WP - first stage)
CN310070094SActive Publication Date: 2026-07-03ZHEJIANG HUAQING AERO ENGINE TECH CO LTD
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- ZHEJIANG HUAQING AERO ENGINE TECH CO LTD
- Filing Date
- 2025-12-16
- Publication Date
- 2026-07-03
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Figure 000007_ABST
Abstract
1. Name of the product in this design: Compressor Rotor (400WP-First Stage). 2. Purpose of this design: As an accessory for the compressor in an aircraft engine. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.
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