in this paper the study of a typical reaction turbine has been carried out. A reaction turbine is a

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IJSRD - International Journal for Scientific Research & Development| Vol. 4, Issue 05, 2016 | ISSN (online): 2321-0613

Result Analysis and Discussion of Stress and Strain on Turbine Shaft Sujata Deshmukh1 Asst. Prof. A.P.Ninawe2 Dr.A.V.Vanalkar3 1 P.G. Student 2Assistant Professor 3Professor 1,2,3 Department of Mechanical Engineering 1,2,3 K.D.K College of Engineering Abstract— in this study the effect of mechanical forces on the steam turbine rotor shaft is carried out. The steam turbine is a mechanical device in which thermal energy of the pressurized steam is converted into rotation of the turbine shaft. This is achieved by reducing the pressure of steam as it passes over turbine blade. Due to the action of this steam mechanical forces acts on the turbine shaft. Stresses are induced due to these forces. For smooth working of turbine the stresses are need to study. The stresses are estimated by analytically calculating the mechanical forces and then these forces are applied on a CAD software model of the turbine shaft . Along with forces the material properties, boundary conditions are updated on the CAD model and analysis is done in ANSYS. Key words: CAD, FEM I. INTRODUCTION In the steam turbine the thermal energy in the pressurized steam is converted into the mechanical energy of rotation of shaft. This pressurized steam exerts tangential and axial thrust on the turbine shaft. Also a centrifugal thrust is acting on the turbine shaft due to the rotation of disc. The shaft under study consists of High pressure (HP), Intermediate pressure (IP) and Low pressure (LP) turbine shaft. There are total 25 Stages of HP shaft. The IP shaft is double flow axial turbine and it has total 20 +20 stages on either side. The LP turbine has total 6 + 6 stages. The size of blade for it is increasing towards the end. II. ANALYTICAL CALCULATION

Tangential load in N

Axial load in N

Centrifugal load in N

Stage 1

33700

1431

8575920

2

34400

662

8695350

3

34000

661

8633772

4

35000

720

8662857

5

36660

660

8679466

6

37000

295

8882508

Lp turbine

Mechanical load on turbine shaft A. FEM Analysis: The FEM analysis is carried out by using ANSYS software. As the geometry under study is axis symmetric only one degree model is considered for the study. The model for HP, IP and LP shaft is converted into IGES format. The model of each shaft without blades is considered. The models are meshed using solid 187 element in ANSYS. Solid 187 is a higher order tetrahedral 3-D element having 10 nodes. It is most suitable for meshing irregular geometry. Then suitable boundary conditions are applied which simulate the actual working environment of turbine shaft. The analytically calculated forces are then applied on the slice of shaft. The forces are applied on the upper surface (grooves) of the shaft. III. RESULT AND DISCUSSION A static structural analysis is carried out and following results are obtained. For HP shaft

The tangential and axial forces are calculated by drawing velocity diagram per stage. The centrifugal force is calculated by using conventional formula. Mechanical load on turbine shaft The following table shows the tangential, axial and centrifugal forces per stage. Tangential load

Axial load

Centrifugal load

Hp turbine

Newton

N

N

(stage 1-25)

17380

880

926258

Stage 1

20680

440

1359823

2

20680

440

1695877

3

20300

220

1491986

4

20300

220

1524344

5

21120

440

1854589

6

21120

440

1917145

7

21560

660

1972720

8

21560

660

2042091

9

22000

550

2112644

10

22000

550

2184356

11

22550

880

2257297

12

22550

880

2331397

13

23100

660

2406679

14

23100

660

2497334

15

23540

1100

2575179

16

23540

1100

2639622

17

24200

660

2704854

18

24200

660

2770874

19

24640

440

2868032

20

24640

440

2951395

IP turbine

The equivalent stress (von –mises) is shown in the above fig. The maximum equivalent stress is 442.31Mpa. The distribution of stress is shown in the above fig. The value of stress is more at the upper portion of the shaft and it is reducing towards the central axis of shaft.

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