一种氢氧燃烧热环境试验装置及方法
By designing a hydrogen-oxygen combustion thermal environment test device, and using pre-tightened bolts to simulate the centrifugal load of turbine blades and achieve sealing, the problem of simulating the mechanical load of turbine blades under high temperature and high pressure environment was solved, and the flexible adjustment and sealing effect of the flow channel were realized.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING AEROSPACE PROPULSION INST
- Filing Date
- 2023-10-20
- Publication Date
- 2026-07-17
AI Technical Summary
Existing technologies make it difficult to safely and reliably simulate mechanical loads on aerospace impact turbine blades under high-temperature and high-pressure hydrogen-oxygen combustion environments, especially for smaller blades that are difficult to simulate centrifugal mechanical loads using fatigue testing machines.
A hydrogen-oxygen combustion thermal environment test device was designed, including a main body, a concave baffle, a convex baffle, a combustion chamber connection device, a tail connector, a tail fixing baffle, and pre-tightening bolts. The pre-tightening bolts are used to apply pre-tightening force to simulate the centrifugal load of the blades, and the reaction force of the pre-tightening bolts is used for sealing.
It achieves safe and reliable mechanical load simulation of turbine blades under high temperature and high pressure hydrogen-oxygen combustion environment. The flow channel design can be quickly replaced according to needs, with good sealing effect and precise mechanical load control.
Smart Images
Figure CN117629786B_ABST