一种基于飞行任务剖面的核心机试验方法
By adopting a core engine testing method based on flight mission profile design, the problem that traditional testing methods cannot fully verify the core engine performance and structural strength has been solved, realizing full-process verification of the core engine and improving the accuracy and authenticity of the test.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- AECC SHENYANG ENGINE RES INST
- Filing Date
- 2026-06-18
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional core engine heating and pressurization test methods only assess discrete typical states, failing to fully verify the performance and structural strength changes of the core engine in the time and process dimensions. This leads to differences between the test results and those under actual flight missions, making it difficult to expose the risk of performance degradation or structural failure.
The core engine test method based on flight mission profile design improves the accuracy and rationality of the test by determining multiple consecutive typical working stages, calculating the rate of change of inlet conditions, and integrating them into a test procedure that simulates the flight profile of the whole machine.
It enables full-process verification of core machine performance and structural strength, improves the authenticity and accuracy of test results, and can better expose potential performance degradation or structural failure risks.
Smart Images
Figure CN122409201A_ABST