Page 238 - Handbook of Energy Engineering Calculations
P. 238

3
                                          3
               (1200/2)/60 = 2.952 ft /s (0.0084 m /s).
                  Then, the volumetric efficiency of this engine = actual charge drawn into
               the cylinder/engine displacement = 2.45/2.952 = 0.8299, or 82.99 percent.


               Related Calculations. Use this general procedure to determine the volumetric
               efficiency  of  reciprocating  internal-combustion  engines—both  gasoline  and

               diesel. The procedure is also used for determining the fuel consumption of
               such engines, using test data from actual engine runs.



               AIR-COOLED  I-C  ENGINE  CHOICE  FOR  INDUSTRIAL
               USES




               Choose a suitable air-cooled gasoline engine to replace a 10-hp (7.46-kW)

               electric motor driving a municipal service sanitary pump at an elevation of
               8000 ft (2438 m) where the ambient temperature is 90°F (32.2°C). Find the
               expected load duty for this engine; construct a typical load curve for it.


               Calculation Procedure:



               1. Determine the horsepower (kW) rating required of the engine
               Electric  motors  are  rated  on  an  entirely  different  basis  than  are  internal-
               combustion engines. Most electric motors will deliver 25 percent more power
               than  their  rating  during  a  period  of  1  or  2  hours.  For  short  periods  many
               electric motors may carry 50 percent overload.

                  Gasoline engines, by comparison, are rated at the maximum power that a
               new  engine  will  develop  on  a  dynamometer  test  conducted  at  an  ambient
               temperature of 60°F (15.6°C) and a sea-level barometric pressure of 29.92 in

               (759.97 mm) of mercury. For every 10°F (5.56°C) rise in the intake ambient
               air temperature there will be a 1 percent reduction in the power output. And
               for every 1-in (2.5-cm) drop in barometric pressure there will be a 3.5 percent
               power output loss. For every 1000 ft (304.8 m) of altitude above sea level a
               3.5 percent loss in power output also occurs.

                  Thus, for average atmospheric conditions, the actual power of a gasoline
               engine is about 5 to 7 percent less than the standard rating. And if altitude is a
               factor, the loss can be appreciable, reaching 35 percent at 10,000-ft (3048-m)
   233   234   235   236   237   238   239   240   241   242   243