trouble shooting tips No. 5 The Noisy Pump That Does not PumpPublished August 1988 VAPOR PRESSURE AND ITS EFFECT ON PUMPING WITH A SUCTION PUMP
There seems to be some confusion and possibly a lack of knowledge over what many call " VAPOR Lock" in pumping systems. We are going to attempt, we hope, to clarify and not confuse the situation, and maybe pass on some information you did not have before.
"VAPOR Lock" is really a misnomer as nothing is "locked". It may seem that the pump has quit pumping but it has not. What has happened is that the Gasoline has turned from a liquid to a gas (or VAPOR). Because the Pump unit can no longer get liquid it "Gravitates", becoming very noisy, with vibration and slows its delivery dramatically.
However as most Service Station Pumps are positive displacement pumps (this means they must move something or something breaks) they are in fact pumping and what they are pumping is the gas or vapor. This gas or vapor is being discharged through the air eliminator if it is working properly, and is visible under right light conditions. It would be highly visible if you ignited it! Therefore it is not a condition where you want to leave the pump running.
Why did the liquid Gasoline turn to a gas? Well each liquid has a given "VAPOR Pressure" at given temperatures. This VAPOR Pressure is the lowest pressure which must be maintained on the liquid for the current temperature to keep it in liquid state.
What makes the situation confusing is that this pressure increases with temperature, and varies from liquid to liquid. Gasolines have a variety of VAPOR Pressures dependent upon the additives in them. Thus unleaded are different than leaded, premiums different than regular and winter grades different than summer grades.
A plus factor however is that at most ambient temperature ranges the VAPOR Pressure of Gasolines is less than normal atmospheric pressure, thus it will stay in liquid state without additional pressure being applied to it. This is not the case with liquids such as Propane which must be kept in a pressurized container to keep them liquid as atmospheric pressure alone will not do it.
Back to our Service Station Pump unit that is noisy and slow; how can we determine if we have gone below VAPOR Pressure?The pump will cavitate if It can not get liquid.
A pump that is cavitatinq is:To determine if we in fact are trying to pump below the VAPOR Pressure of the liquid we need the following information:Noisy
Full of vibration
experiencing a fluctuating or high Vacuum reading on Suction side.
experiencing a Low Pressure reading on Discharge side.
has extremely low flow If any.
A. The VAPOR Pressure of the Fuel and its current temperature.The temperature should be measured at the discharge of the pump as the temperature in the pump and the lines will probably be higher than in the tank, particularly if there is not much cover, and asphalt instead of concrete over the lines. However it would be of interest to know the temperature in the tank as well.
The fuel supplier can give us the VAPOR Point of the fuel. They usually express it in terms of Reid VAPOR Pressure which is normally a 1 or 2 digit number. If they can give you a true VAPOR Pressure Curve for Various temperatures it would be better. However our Figure 1 will give you a rough conversion for some of the Reid VAPOR numbers to PSI absolute for some temperatures.
APPROXIMATE VAPOR PRESSURE - PSI Absolute
MOTOR GASOLINE WINTER GASOLINE SUMMER GASOLINE AVIATION JET FUEL & KEROSENE TEMPERATURE REID VAPOR PRESSURE 14 REID 12 REID 10 REID 8 REID 40F 4.8 4.0 3.4 2.8 2.2 0.9 50F 5.9 4.9 4.1 3.4 2.8 1.0 60F 7.4 6.0 5.0 4.1 3.5 1.0 70F 8.9 7.4 6.0 5.0 4.2 1.2 80F 10.7 9.0 7.1 5.9 5.1 1.4 90F 12.8 10.6 8.6 7.0 6.2 1.7 100F 14.0 12.0 10.0 8.0 7.4 2.0
It should be noted that the VAPOR pressures are getting higher in the newer fuels and higher in winter fuels than summer fuels. Therefore it is a good to idea to check when the fuel was delivered (in some cases the delivery slip will give the Reid VAPOR Pressure of the fuel). For our example let us say we are given Reid #12 and we measure its temperature as 78 deg. F.
B. The Suction needed to pull the fuel from the Tank to the Pump.This can measured directly with Vacuum Gauge but will only be accurate if the problem is a blocked line or vent where you will get a steady high reading.C. The Current Atmospheric Pressure.a. Height from center line of the pump to the level of the liquid in the tank.To calculate our suction Lift:
b. The length and size of the suction line including the equivalent length of pipe caused by fittings. (see figure 2 at end of document)
c. The normal flow rate of the pump.For our example lets assume (see drawing A at end of document)a. Height from C/L to liquid level is measured at 11 feet. From Curve (figure 3 at end of document) we see this is equal to 6.6 in. Hg.(Mercury).
b. We determine that there is 60 feet of 2 in. pipe with 6 - 2 in 90 Deg. SR elbows. From Figure 2 we can determine that each elbow is equal to 5 feet of pipe. This gives us:Total pipe = 60 feetc. The normal flow rate of the pump from the name plate we find is 10 USGPM
Equiv. pipe from
fittings = 6 x 5 = 30 feet
Total = 90 feet1. Static Lift (C/L pump to liq. level) = 6.6 in.Hg.Using the formula 1 in.Hg. = 0.489 PSI we get:
2.Total equivalent length pipe = 90 feet
From figure 4 at 10 USGPM we need
0.2 in.Hg per 100 feet of pipe to overcome
friction loss in the pipe> Therefore to
calculate 90 feet/100 feet x 0.2 In. Hg. = 0.18 in.Hg.
Total suction lift = 6.78 in.Hg.6.78 in.Hg. x 0.489 = 3.32 PSIA quick phone call to you local weather office will give you this.A call to our local hot line today gave me a current atmospheric pressure of 100.9 KPa (Kilopascals). The conversion to PSI is: 1 KPa = 0.145 PSITo calculate If we have lowered the Pressure on the Gasoline below its VAPOR Pressure we use the following formula:
Therefore our current atmospheric pressure is 100.9 KPa x 0.145 = 14.63 PSI,ATMOSPHERIC PRESSURE - SUCTION LIFT = PRESSURE ON FUELIf However at B. where we calculated our Suction Lift as 6.78 in.Hg. Vacuum, with a Vacuum gauge we actually measured vacuum as high as 12 in.Hg. We would then come to the following result:
Therefore from our example: 14.63 PSI - 3.32 PSI = 11.31 PSI
Now from our Figure 1 we determine that the VAPOR Pressure of our Reid #12 fuel at 78 deg. F is approx. 8.7 PSI and thus we are 11.31 PSI - 8.7 PSI = 2.61 PSI over the VAPOR Pressure point of the fuel and it should not be turning to a gas.12 in.Hg. x 0.489 = 5.87 PSI (Actual Suction Lift)At this point we should look for a blockage in our Suction or Vent lines, or a high spot in the suction line.
14.63 PSI - 5.87 PSI = 8.76 PSI (Pressure on liquid)
8.7 PSI - 8.76 PSI = -0.06 PSI (Pressure below VAPOR Pressure)
But remember to first determine if there is an appreciable difference between the calculated Vacuum and the Actual Vacuum.
If you do this procedure you will save a lot of time looking for blocked lines that are not there when the problem could simply be a fuel with too high a VAPOR Point being too hot on a day with low atmospheric pressure.
An important note is that the most significant thing affecting the Suction Lift or Vacuum is the Static or Vertical lift and not the length of pipe. This means if you are having the problem on a tank that is low in fuel, simply filling it may eliminate the problem.
A couple of helpful manuals to get your hands on are Blackmer Pump's Bulletin 33 "Hydraulic Data for Pump Applications" and Marlow Pump's ITT "Engineering Manual".
Good luck on figuring these situations out!
Typical Installation Diagram
Shown in approximate equivalent length of straight pipe in feet
Type of Fitting 1 1/2in 2in 3in Gate Valve - Fully Open 0.95 1.2 1.7 Globe Valve - Open 42 51 80 Angle Valve - Open 20 30 40 Standard Tee - through side outlet 9 12 16 Standard Tee - straight through 2.8 3.5 5 Standard Elbow 4.5 5.0 8 Medium Sweep Elbow 3.5 4.5 7 Long Sweep Elbow 2.8 3.5 5
Specific Gravity 0.72
Reading in inches of mercury (in.Hg.)
10 0.2 15 0.2 20 0.4 25 0.8 30 1.0 35 1.4 40 1.8 45 2.4 50 2.9 60 4.1 70 5.5 80 6.9 90 9.0 100 11.0 120 15.1