FREE BOOKS

Author's List




PREV.   NEXT  
|<   26   27   28   29   30   31   32   33   34   35   36   37   38   39   40   41   42   43   44   45   46   47   48   49   50  
51   52   53   54   55   56   57   58   59   60   61   62   63   64   65   66   67   68   69   70   71   72   73   74   75   >>   >|  
the proper screw adjustment. Main Bearings The bearings which support the rotor are shown at F F in Fig. 34 and in detail in Fig. 41. The bearing proper consists of a brass tube B with proper oil grooves. It has a dowel arm L which fits into a corresponding recess in the bearing cover and which prevents the bearing from turning. On this tube are three concentric tubes, C D E, each fitting over the other with some clearance so that the shaft is free to move slightly in any direction. These tubes are held in place by the nut F, and this nut, in turn, is held by the small set-screw G. The bearing with the surrounding tubes is placed inside of the cast-iron shell A, which rests in the bearing pedestal on the block and liner H. The packing ring M prevents the leakage of oil past the bearing. Oil enters the chamber at one end of the bearing at the top and passes through the oil grooves, lubricating the journal, and then out into the reservoir under the bearing. The oil also fills the clearance between the tubes and forms a cushion, which dampens any tendency to vibration. [Illustration: FIG. 41] The bearings, being supported by the blocks or "pads" H, are self-alining. Under these pads are liners 5, 10, 20, and 50 thousandths in thickness. By means of these liners the rotor may be set in its proper running position relative to the stator. This operation is quite simple. Remove the liners from under one bearing pad and place them under the opposite pad until a blade touch is obtained by turning the rotor over by hand. After a touch has been obtained on the top, bottom, and both sides, the total radial blade clearance will be known to equal the thickness of the liners transferred. The position of the rotor is then so adjusted that the radial blade clearance is equalized when the turbine is at operating temperature. On turbines running at 1800 revolutions per minute or under, a split babbitted bearing is used, as shown in Figs. 42a and 42b. These bearings are self-alining and have the same liner adjustment as the concentric-sleeve bearings just described. Oil is supplied through a hole D in the lower liner pad, and is carried to the oil groove F through the tubes E E. The oil flows from the middle of this bearing to both ends instead of from one end to the other, as in the other type. [Illustration: FIG. 42A] [Illustration: FIG. 42B] Packing Glands Where the shaft passes through the casing at either end
PREV.   NEXT  
|<   26   27   28   29   30   31   32   33   34   35   36   37   38   39   40   41   42   43   44   45   46   47   48   49   50  
51   52   53   54   55   56   57   58   59   60   61   62   63   64   65   66   67   68   69   70   71   72   73   74   75   >>   >|  



Top keywords:
bearing
 

clearance

 

liners

 

proper

 

bearings

 

Illustration

 
adjustment
 

radial

 

passes

 
obtained

prevents

 

turning

 

alining

 

grooves

 
concentric
 

position

 

running

 
thickness
 

stator

 

relative


simple

 

opposite

 
Remove
 

bottom

 

operation

 

carried

 
groove
 

middle

 
supplied
 
casing

Glands

 

Packing

 

sleeve

 

turbine

 

operating

 

temperature

 

turbines

 

equalized

 

transferred

 
adjusted

revolutions
 

minute

 

babbitted

 

cushion

 
slightly
 

direction

 

Bearings

 
inside
 

surrounding

 

fitting