一种考虑基础冲击的航空发动机双转子整机模拟试验器
The aero-engine dual-rotor whole-machine simulation tester with segmented design and squirrel cage elastic support solves the problem that existing testers cannot simulate impact loads, and realizes the dynamic study and load transfer path analysis of the dual-rotor-support-casing system.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
- Filing Date
- 2025-01-20
- Publication Date
- 2026-07-17
AI Technical Summary
Existing dual-rotor test equipment for aero-engines cannot realistically simulate typical axial and radial impact loads, nor can it study the transmission law of impact loads within the dual-rotor-support-casing system.
The aero-engine dual-rotor whole-machine simulation test instrument with segmented design features thin walls, circumferential bolt connections and squirrel cage elastic support, with the connection surface acting as a reinforcing rib to transfer vibration loads and monitor dynamic characteristics through sensors.
Vibration testing of a dual-rotor-support-casing system was achieved, enabling the study of dynamic characteristics and load transfer mechanisms under impact, meeting the experimental requirements of different turntable assemblies, and adjusting the critical speed to a safe range.
Smart Images
Figure CN119643155B_ABST