Mike4chemic
Chemical
- Oct 9, 2004
- 71
Hello,
We design a Vapor Recovery Unit, which its main part is a screw vacuum pump. The system will be located at a site in South America (elevation is about 2,000 m above sea level. The required vacuum level is 0.069 bara.
Based on the pump's operation curve, which was received from a vendor, the maximum vacuum level which can be achieved at sea level by this pump is 29 in HgV (0.03 bara).
I try to evaluate, whether the required vacuum level of 0.069 bara can be achieved at 2000 m above sea level by this pump. I used the following methodology:
This vacuum pump with a maximum capability of 29 in HgV at sea level is rated of 97%.
(29 in HgV/29.92 in HgV)= 0.97
Then, I assumed the 97% rating can be used to the vacuum pump to determine its performance at 2000 m above sea level. The ambient pressure at 2000 m above sea level is about 0.763 bara.
Therefore, the pump’s performance at 2000 m is 0.763 bara X 0.97= 0.74 bara.
Based on this, the vacuum pump can only achieve a maximum absolute pressure of 0.273 bara (1.013 bara-0.74 bara). It means the required vacuum level of 0.069 bara can’t be achieved at 2000 m above sea level.
I asked this question a pump’s vendor. Based on his evaluation, the maximum vacuum level which can be achieved with the pump is 0.023 bara (0.763 bara- 0.74 bara), and therefore he don’t see any problem to achieve the vacuum required level of 0.069 bara.
I'm a little confused. Who is right?
Thanks in advance, Mike