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Recent content by frogcurry

  1. frogcurry

    TUBE/SHELL HEAT EXCHANGER

    Don't forget to revisit all pressure relief (fire, blowdown, burst tube/ tubesheet rupture) calcs in light of the design pressure change if you proceed with this.
  2. frogcurry

    Location of PSV on Shell & Tube Heat Exchanger

    What jcaiken says is correct as I understand it. the Institute of Petroleum has some guidance published on this. For the relief backpressure, the line/ disk sizing methodology is based on the backpressure produced by the slug of seawater pushed ahead of the expanding gas, as per API 520/521.
  3. frogcurry

    centrifugal compressor response to a block discharge line

    If a centrifugal compressor has its discharge blocked in then it will recycle at its anti-surge control point. Flow isn't zero.
  4. frogcurry

    PSV Discharge Header - Sizing Assumptions

    If sizing for relief valves lifting on blocked outlet, then the gas relieving from compressor A can't be also simultaneously coming out compressor B, if the order is A>B>C in series. Since after all blocked outlet on A is blocked inlet on B. Its not feasible to have A and B both pushing open...
  5. frogcurry

    Heat exchanger design using HYSYS

    Effects of pressure drop depend on whats in the tubes and conditions... If you want to use a program to design heat exchangers use HTFS-TASC. Or buy a book.
  6. frogcurry

    Crane vs ISA; K velocity head coefficient eqn for contraction

    Ahem... that theta is of course an angle of convergence in Crane, so the 60 degree theta is for a 30 degree slope on the wall.
  7. frogcurry

    Crane vs ISA; K velocity head coefficient eqn for contraction

    After reading your last post I did some quick analysis in Excel of this using Cranes method for gradual reducers as well as sudden reduction: const beta factor result Crane 0.5 0.75 1 0.375 ISA 0.5 0.5625 1 0.2812 2-13 0.8 0.75 0.258 0.1552 2-13 refers to the...
  8. frogcurry

    Crane vs ISA; K velocity head coefficient eqn for contraction

    The ISA eqn quoted above is just for the inlet reducer.
  9. frogcurry

    Vessel Capacity check & Equiment Sizing

    Use the Shell DEPs if you have them.
  10. frogcurry

    Crane vs ISA; K velocity head coefficient eqn for contraction

    ISA S75.01-1985 quotes for an inlet reducer (Eq 6, pg 15): K1 = 0.5 * (1 - (d^2/D^2))^2 Crane 410M page 2-11, eqn 2-10 quotes K1 = 0.5 * (1 - (d^2)/(D^2)) These would appear to be equivalent concepts but there is a difference - ISA quotes an additional squared at the end of the eqn. So, am I...
  11. frogcurry

    vacuum seawater deaeration pumps -seawater gas concs.

    Hi, I'm attempting to assess (at a preliminary stage) whether a vacuum pump system (liquid ring pump and ejector operating in two stages) is adequate for an increase in duty in the seawater flow. I have a pump curve for the liquid ring pump but no other information. It gives a curve of torr...
  12. frogcurry

    Calculate Nitrogen Gas Flow From PCV

    Please clarify - an orifice for going from 3 psig to 1 psig or an orifice to go from 5 psig to 3 psig? Whats your intended downstream enduser pressure?
  13. frogcurry

    Hazard from object in motion due to differential pressures (forces)

    Thanks. What you describe is exactly the sort of scenario that the Loss Prevention Bulletin describes save that the pressure differential driving the pig was on the order of 400 psig for a 12 in pig... When you're doing this do you have any estimation techniques you use for assessing how fast...
  14. frogcurry

    Hazard from object in motion due to differential pressures (forces)

    This is a tricky question to define as its not a specific item or system, but a generic concept. While reading the Loss Prevention Bulletin article this month on pigs, I read a comment about "20 tons of force" driving a pig out of a pipeline which had its pig reciever open causing the pig to be...
  15. frogcurry

    pig system design

    The LPB article referenced by cawse001 is a very good place to check, particularly for the design of proper depressurisation locations.

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