CHoff07
Mechanical
- Aug 14, 2012
- 15
I'm looking to explore the Pro's and Con's of various HPRT designs as it relates to long term reliability.
It seems like different vendors offer different solutions and I'd like hear from people on the types of machine they have installed and the availability of the HPRT. All discussion will be around HPRT which are "pumps in reverse". Though "true turbine" designs exist, I believe the flow rates I'm looking at (<2500 gpm) are below what would make this an economically viable solution.
Option 1: Straight Through
Issues I believe exist.
1. High axial thrust due to impeller stack - mitigated with proper thrust bearing selection and limitation on # of impellers
2. If balance piston wears (due to flashing/dry running)thrust may increase - mitigated by monitoring pressure differential between new and worn
Option 2: Back to Back
Issues I believe exist.
1. In theory axial thrust is balanced but this may not be true due to vapor formation at lower pressure stages. This vapor formation will force higher pressure drops due to the expanding volume of the liquid at the lower pressure stages leading to imbalance. - Mitigated by - UNKNOWN
2. Inter-stage bushing may run dry if liquid is flashing across it. Same concerns as item 1 about, how do I know what the pressure across this will be if the pressure profile across the pump is not uniform? - Mitigated by - UNKNOWN, no way to monitor this bushing...
Feel free to comment on any or all of these issues or present additional concerns as you see fit.
***As important as it is, I will ignore seal aspect of the HPRT because we've standardized on API PLAN 53B to eliminate any flashing issues at the seal faces. If people have objections to this or have experienced issues, please include that in your replies.
It seems like different vendors offer different solutions and I'd like hear from people on the types of machine they have installed and the availability of the HPRT. All discussion will be around HPRT which are "pumps in reverse". Though "true turbine" designs exist, I believe the flow rates I'm looking at (<2500 gpm) are below what would make this an economically viable solution.
Option 1: Straight Through
Issues I believe exist.
1. High axial thrust due to impeller stack - mitigated with proper thrust bearing selection and limitation on # of impellers
2. If balance piston wears (due to flashing/dry running)thrust may increase - mitigated by monitoring pressure differential between new and worn
Option 2: Back to Back
Issues I believe exist.
1. In theory axial thrust is balanced but this may not be true due to vapor formation at lower pressure stages. This vapor formation will force higher pressure drops due to the expanding volume of the liquid at the lower pressure stages leading to imbalance. - Mitigated by - UNKNOWN
2. Inter-stage bushing may run dry if liquid is flashing across it. Same concerns as item 1 about, how do I know what the pressure across this will be if the pressure profile across the pump is not uniform? - Mitigated by - UNKNOWN, no way to monitor this bushing...
Feel free to comment on any or all of these issues or present additional concerns as you see fit.
***As important as it is, I will ignore seal aspect of the HPRT because we've standardized on API PLAN 53B to eliminate any flashing issues at the seal faces. If people have objections to this or have experienced issues, please include that in your replies.