A propeller thrust measuring scale test device for turboprop engine ground test bed

By designing a scaled-down test device for measuring propeller tension on a turboprop engine ground test stand, the problems of high cost, long cycle, and equipment interference in the existing technology have been solved. It realizes accurate tension measurement with low cost and short cycle, and is suitable for propeller tension evaluation on turboprop engine ground test stands.

CN122409197APending Publication Date: 2026-07-17AECC HUNAN AVIATION POWERPLANT RES INST
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
AECC HUNAN AVIATION POWERPLANT RES INST
Filing Date
2026-03-31
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

The lack of mature ground test stand propeller thrust measurement technology for turboprop engines in the current technology leads to high test costs, long test cycles, and results that are easily affected by test stand equipment, making it difficult to accurately reflect the propeller thrust of the integrated propeller and generator.

Method used

Design a scaled-down test device for measuring propeller tension on a ground test stand for turboprop engines. The device includes a scaled-down test chamber, a scaled-down test stand, a scaled-down propeller, a scaled-down air intake, a rotating force balance, etc. The model is scaled down according to a set ratio. Combining similarity theory and a measurement and control system, the device simulates the engine air intake process and avoids equipment vibration interference.

Benefits of technology

It enables low-cost, short-cycle propeller thrust measurement, accurately assesses the thrust of propeller-generator integrated units, avoids interference from test bench equipment, and improves the accuracy and efficiency of measurement.

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Abstract

本发明属于涡桨发动机试验装置技术领域,公开一种涡桨发动机地面试车台螺旋桨拉力测量缩尺试验装置,包括缩尺试车间、缩尺台架、缩尺螺旋桨、缩尺进气道、缩尺发动机迎风圈、旋转测力天平、涡轮空气马达和支架;缩尺台架设置在缩尺试车间内,支架的底部与缩尺试车间固定连接,支架为中空结构,涡轮空气马达固定设置在支架的内部顶端,涡轮空气马达的传动轴通过旋转测力天平与缩尺螺旋桨固定连接,缩尺发动机迎风圈套设在支架顶端外壁,缩尺进气道与支架固定连接。本发明的缩尺试验装置按设定的缩尺比例整体缩小,具有简单易行、成本低、周期短等优点,同时能够避免原型试验中可能受试车台设备振动干扰以及试车间工艺设备的影响。
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