Table of Contents Table of Contents
Previous Page  332 / 392 Next Page
Information
Show Menu
Previous Page 332 / 392 Next Page
Page Background

•

Calculation of the temperature field in nominal regime and corresponding stress field.

•

Calculation of stress and deformation fields of the turbine for crack lengths (20–75 mm).

•

Analysis of the influence of crack length on corresponding stress field as well as on the

stress intensity factor.

For temperature field calculation, the 2-D grid consisted of 4400 8-node elements.

Generated grid comprised the space of the turbine housing and insulation.

In Fig. 6 the stress field induced by temperature and internal pressure is shown. The

effective stress for 2-D turbine model without insulation, for crack length 30 mm, is

shown in Fig. 7.

a)

b)

Figure 6. a) 2D model for calculation of the temperature field;

b) Temperature field of the turbine housing and insulation

Figure 8 shows the relationship between stress intensity factor

K

I

and crack length. It

can be seen from Fig. 8 that by increasing crack depth from 20 mm to 40 mm, the stress

intensity factor increases 30%. With crack length increase of over 50 mm, the stress

intensity factor increases more rapidly.

328