NUMERICAL AND EXPERIMENTAL STUDY OF ICE ACCRETION PROCESS AND ICE PROTECTION ON TURBO-FAN ENGINE SPLITTER

摘要

The splitter, a steady component in the downstream of fan blades in the turbo-fan engine, will be exposed to an icing environment when the engine is working in icing conditions. An anti-icing system should be used on the splitter in order to make the engine work well and not be affected by icing. In this study, both of experiments and CFD simulations were applied to acquire icing characteristics and the electronic anti-icing system' energy requirement for this component. Factors of icing conditions varied from attacking angle, ambient temperature and pressure, air velocity and droplet factors. Experiments were performed in the AVIC Aerodynamics Research Institute Icing Wind Tunnel (FL-61). The test component was a combination of an arc segment of splitter and seven pieces of inlet guide vanes, covered by electrical heating film. The experiment was carried out under different icing conditions in the icing wind tunnel. Ice profiles, the results of icing experiment, were collected by 3D scanner. Anti-icing surface temperature profiles were collected by thermocouples. The CFD results of icing process were compared with the experimental data for validation, and showed that the droplet collection of on the lower surface of splitter was significant. The CFD simulation was established on the two-phase flow analysis conducted by ANSYS-CFX and Fensap-ice for the prediction on ice accretion, and a coupled simulation method was introduced to replace the conjugate simulation method for thermal analysis with a higher working efficiency in engineering design. Through the icing simulation, an estimated external boundary condition was applied on the thermal model of the test piece and the temperature field on the test piece was calculated.