Design and experiment of hot gas duct for the HTR-10
Introduction
The modular high temperature reactor (HTR-module) concept developed by Siemens/Interatom in 1981 was the first small, modular-type reactor concept to be proposed worldwide; the thermal output of the pebble bed HTR-module is 200 MW (Lohnert and Reutler, 1983, Lohnert, 1990).
The hot gas duct is a unique component exclusively found in this type of reactor where both the nuclear core and the power conversion unit are placed into two pressure vessels, which need a connecting duct. Passing through the HTR-module core, hot helium gas is conveyed via the liner tube of the horizontal hot gas duct to the steam generator. After being cooled down, the cold helium gas is returned to the lower section of the reactor pressure vessel via a passage between the coaxial inner tube and pressure vessel of the hot gas duct.
The 10 MW High Temperature Gas-cooled Reactor—Test Module (HTR-10) is the first high temperature gas-cooled reactor developed at the Institute of Nuclear Energy Technology (INET) of the Tsinghua University, China (Wang et al., 1991). Its basis is the HTR-module design. The pebble type fuel elements pile naturally in a cavity built by laying graphite blocks, forming a cylindrical pebble bed core. Helium gas is used as the coolant. The helium gas pressure in the primary loop is 3.0 MPa. The inlet helium temperature of the core is 250 °C and the outlet helium temperature of the core is 700 °C (the corresponding inlet/outlet temperatures are 300 and 950 °C in the secondary project stage of the HTR-10). The reactor core is located inside the reactor pressure vessel, while the steam generator and the helium circulator are in the adjacent vessel, i.e. the steam generator vessel. The two vessels are connected together by a hot gas duct (Fig. 1). The cold helium gas of 250 °C flows out of the helium circulator, passes through the annual space between the inner tube and the duct pressure vessel, goes up along the inner surface of the reactor pressure vessel, then flows through the core from the top to the bottom. After being heated up in the core to the 700 °C, the hot helium gas flows into the steam generator through the liner tube of the hot gas duct.
The hot gas duct has to operate at high temperature and medium pressure condition for a long time. Its performance of thermal insulation between hot and cold helium flow, its ability to resist temperature cycles and pressure cycles, and to sustain total structure integrity at high temperature and medium pressure conditions will play an important role in the long-term safe operation of the HTR-10.
Detailed structure design and strength evaluations of the hot gas duct have been carried out. A hot gas duct test section with the same structure and dimensions as the prototype was fabricated, and an engineering simulating experiment was carried out on helium gas test loop.
Section snippets
Hot gas duct design
The structure of HTR-10 hot gas duct is shown in Fig. 2, its one end connects to the reactor pressure vessel by a flange; the other end connects to the steam generator vessel by a flange also. The duct has the following functions:
- 1
transporting the hot helium gas from the core to the steam generator;
- 2
transporting the cold helium gas from the steam generator to the core;
- 3
providing thermal compensations and avoiding large thermal stresses in various operating conditions.
The hot gas duct is a
Thermal compensation of bellows
The distance between the axes of the reactor pressure vessel and the steam generator pressure vessel is 7099 mm, the temperature rise of the components of the primary loop boundary under accident conditions is conservatively taken to the 250 °C, and the thermal expansion coefficient of ferritic steel is as follows:
Therefore, the calculated maximum thermal expansion between the axes of the reactor pressure vessel and the steam generator pressure vessel is as follows:
The
Experimental study of hot gas duct
Researchers in Germany and Japan did a lot of design analyses and test studies on hot gas ducts with different structures (Broeckerhoff, 1978, Broeckerhoff, 1981, Broeckerhoff et al., 1984, Harth et al., 1990, Hishida et al., 1984, Hishida et al., 1987, Ioka et al., 1994). Their methods and results were very valuable for INET and were used as guidelines for an experimental study for the hot gas duct of the HTR-10.
Conclusion
Detailed structure design and mechanical strength evaluations of the hot gas duct for the HTR-10 were carried out. A full-scale hot gas duct test section was investigated for its thermal performance in a helium test loop. The effective thermal conductivity of the thermal insulation in the hot gas duct was obtained. The cumulative hot operation for the hot gas duct lasted 450 h; pressure cycles and temperature cycles were also repeatedly tested. After the hot gas duct was disassembled, hot test
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