一种高温气冷堆主氦风机等效试验方法

By measuring and calculating the operating parameters of the main helium blower at normal temperature and pressure, and combining the gas characteristics to calculate the helium pressure at the hot test temperature, the problem that the main helium blower of the high-temperature gas-cooled reactor could not be tested at full speed was solved, and safe testing was achieved across the entire speed range.

CN116608145BActive Publication Date: 2026-07-17XIAN THERMAL POWER RES INST CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
XIAN THERMAL POWER RES INST CO LTD
Filing Date
2023-05-30
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

When the main helium blower of the high-temperature gas-cooled reactor is running at 100% rated speed, the flow resistance decreases, which leads to an increase in flow rate and causes the current to exceed the limit, affecting safe operation and making it impossible to conduct a full-speed test.

Method used

The operating parameters of the main helium blower at normal temperature and pressure are obtained through actual test measurements. The theoretical parameters at different speeds are calculated. The helium pressure at the hot test temperature is calculated in combination with the gas characteristics. Equivalent tests are conducted to simulate the operating parameters across the entire speed range. If overload or overcurrent conditions occur, the pressure is reduced for adjustment.

Benefits of technology

The main helium blower was tested at full speed within the range of 0%-100% of its rated speed, effectively preventing overload operation and ensuring that the test was completed under safe and stable conditions.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明涉及高温气冷堆主氦风机试验技术领域,具体涉及一种高温气冷堆主氦风机等效试验方法,包括:通过真实试验测量获得主氦风机的第一运行参数,计算常温下主氦风机额定满功率和100%额定转速的空气压力,进而计算主氦风机在常温、上述空气压力下不同转速的第一理论参数;通过真实试验测量获得主氦风机的第二运行参数,计算主氦风机在额定热态试验温度、100%额定转速、额定满功率工况下的氦气压力,计算主氦风机在额定热态试验温度、上述氦气压力下不同转速的第二理论参数;通过真实试验测量获得主氦风机的第三运行参数,进而获得等效状态下主氦风机在全转速范围内真实试验参数。利用此降压的等效试验方法,最终实现主氦风机全转速范围的全部试验。
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