Structural integrity assessment and stress measurement of CHASNUPP-1 fuel assembly

التفاصيل البيبلوغرافية
العنوان: Structural integrity assessment and stress measurement of CHASNUPP-1 fuel assembly
المؤلفون: null Waseem, Ghulam Murtaza, Ashfaq Ahmad Siddiqui, Syed Waseem Akhtar
المصدر: EPJ Nuclear Sciences & Technologies. 2:18
بيانات النشر: EDP Sciences, 2016.
سنة النشر: 2016
مصطلحات موضوعية: Materials science, 020209 energy, Specified load, Zirconium alloy, 02 engineering and technology, Nuclear reactor, 01 natural sciences, Rod, 010305 fluids & plasmas, law.invention, Stress (mechanics), law, 0103 physical sciences, Ultimate tensile strength, 0202 electrical engineering, electronic engineering, information engineering, Composite material, Stress intensity factor, Strain gauge
الوصف: Fuel assembly of the PWR nuclear power plant is a long and flexible structure. This study has been made in an attempt to find the structural integrity of the fuel assembly (FA) of Chashma Nuclear Power Plant-1 (CHASNUPP-1) at room temperature in air. The non-linear contact and structural tensile analysis have been performed using ANSYS 13.0, in order to determine the fuel assembly (FA) elongation behaviour as well as the location and values of the stress intensity and stresses developed in axial direction under applied tensile load of 9800 N or 2 g being the fuel assembly handling or lifting load [Y. Zhang et al., Fuel assembly design report, SNERDI, China, 1994]. The finite element (FE) model comprises spacer grids, fuel rods, flexible contacts between the fuel rods and grid's supports system and guide thimbles with dash-pots and flow holes, in addition to the spot welds between spacer grids and guide thimbles, has been developed using Shell181, Conta174 and Targe170 elements. FA is a non-straight structure. The actual behavior of the geometry is non-linear due to its curvature or design tolerance. It has been observed that fuel assembly elongation values obtained through FE analysis and experiment [SNERDI Tech. Doc., Mechanical strength and calculation for fuel assembly, Technical Report, F3.2.1, China, 1994] under applied tensile load are comparable and show approximately linear behaviors. Therefore, it seems that the permanent elongation of fuel assembly may not occur at the specified load. Moreover, the values of stresses obtained at different locations of the fuel assembly are also comparable with the stress values of the experiment determined at the same locations through strain gauges. Since the results of both studies (analytical and experimental) are comparable, therefore, validation of the FE methodology is confirmed. The stress intensity of the FE model and maximum stresses developed along the guide thimbles in axial direction are less than the design stress limit of the materials used for the grid [ASTM, Standard specification for precipitation hardening nickel alloy (UNSN07718) plate, sheet, and strip for high temperature service, B 670-80, USA, 2013], fuel rod [ASTM, Standard specification for wrought zirconium alloy seamless tubes for nuclear reactor fuel cladding, B 811-02, USA, 2002] and the guide thimble [ASTM, Standard specification for seamless stainless steel mechanical tubing, A 511-04, USA, 2004]. Therefore, the structural integrity criterion of CHASNUPP-1 fuel assembly is fulfilled safely at the specified tensile load.
تدمد: 2491-9292
الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_________::fa54bbb920c776ace60e4dfbfeec5ce4Test
https://doi.org/10.1051/epjn/2016008Test
حقوق: OPEN
رقم الانضمام: edsair.doi...........fa54bbb920c776ace60e4dfbfeec5ce4
قاعدة البيانات: OpenAIRE