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Centrifugal Pumps Design and Application 2nd ed - Val S. Lobanoff, Robert R. Ross (Butterworth-Heinemann, 1992)

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Table 18-3<br />

Balance Quality Grades for Various Groups of Representative<br />

Rigid Rotors<br />

Balance quality<br />

grades<br />

sw a>b<br />

G (mm/sec) Rotor types—General examples<br />

C 4 000 4 000 Crankshaft-drives* of rigidly mount<strong>ed</strong> stow marine ditto! engines with uneven number of<br />

cylinders. 1 *<br />

G t HO 1 600 Crankshaft-drives of rigidly mount<strong>ed</strong> large two-cycle engines.<br />

6 630 630 Crankshaft-drives of rigidly mourn<strong>ed</strong> largt four-ey<strong>ed</strong> engine*.<br />

CranksHaf l-drivm of elastically mount<strong>ed</strong> marine difMl engines.<br />

G *SQ 250 Crankshefl-drives of rigidly mount<strong>ed</strong> fast four-cylinder dieMl engines."<br />

C tOO 100 Crankshafl-drlvei of f*t1 dietel engine! with six or more cylinders.* 1<br />

Complete engines (gasoline or ditMl) for tin. trucks, »nd locomotives,*<br />

C 40 40 Car wheels. vvhe*l rim*, wheel sets, drive shafts<br />

Cranksheft-drivei of •iMtically mount<strong>ed</strong> fast four-cycle engines (gaioline or diesett with tix<br />

or more cyllnderf, 8<br />

Crankshaft-drive* for enginei of can, trucks, end locomotives,<br />

G '16 16 Drive thafti (propeller thiftt, cardan sh»(t>l whri ipeciai requirements.<br />

Parts of crushing machinery,<br />

Parn of agriculture! machinery. [<br />

Individual component* of ertB'nai (gatoline or dietel) for cars, truekt, <strong>and</strong> locomotMt.<br />

Crankshaft-drivei of engines with iix or more eylinderf under special requirements<br />

Slurry or dradge pump impeller.<br />

G 6.3 6,3 Parti or process plant machines.<br />

Marine main turbini geert (merchant service).<br />

Centrifuge drttmi.<br />

Fani.<br />

Assembl<strong>ed</strong> aircraft gat turbine rotort.<br />

Fly wheel!<br />

Pump impeileri.<br />

Machine-toot <strong>and</strong> general machinery pans.<br />

Normal electrical armatures.<br />

Individual components of engines under special requirements.<br />

G 25 !.'•> Get <strong>and</strong> (team turbines, including marina main turbines (merchant service).<br />

Rigid turbo-generator roiori.<br />

1<br />

Rotors.<br />

Turbo-compressor)<br />

Machine-tool drivet.<br />

M<strong>ed</strong>ium <strong>and</strong> large electrical armatures with special requirements.<br />

Small electrical ermaturei.<br />

Turbine-driven pumps.<br />

G t 1 Tape recorder <strong>and</strong> phonograph (gramophone) drives.<br />

Grino'ing-machine drives.<br />

Small electrical armatures with special requirements.<br />

G 0.4 0,4 Spindles. ditKs, <strong>and</strong> armatures at precision grinders.<br />

Gyroscopei.<br />

^^<br />

" w = 2vn/60 ** n/10, ifn is measur<strong>ed</strong> in revolutions per minute <strong>and</strong> w in radians per second.<br />

* In general, for rigid rotors with two correction planes, one-half of the recommend<strong>ed</strong> residual<br />

unbalance is to be taken for each plane, these values apply usually for any two arbitrarily chosen<br />

planes, but the state of unbalance may be improv<strong>ed</strong> upon at the bearings. (See Ses, 3.2 <strong>and</strong> 3.4.)<br />

for disk-shap<strong>ed</strong> rotors the full recommend<strong>ed</strong> value holds for one plane. (See Sec. 3.)<br />

c A crankshaft-drive is an assembly which includes the crankshaft, a flywheel, clutch, pulley,<br />

vibration damper, rotating portion of connecting rod, etc. (See Sec, 3.5.)<br />

d For purposes of this St<strong>and</strong>ard, slow diesel engines are those with a piston velocity of less than 9<br />

m/sec; fast diesel engines are those with a piston velocity of greater than 9 m/sec.<br />

' In complete engines, the rotor mass comprises the sum of all masses belonging to the<br />

crankshaft-drive describ<strong>ed</strong> in Note c above.

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