Hello Patrick,
I may be useful to review the discussion of the allowable stress range concept in a previous thread:
http://www.coade.com/ubb/Forum1/HTML/000057.html As Anindya points out, if you have a calculated stress range magnitude of 65ksi, you can't rationalize it away - it does not comply to the requirements of the current B31.1 Code regardless of the number of cycles in its lifetime. Also, the pipe material will actually yield before this "calculated" (ergo, fictitious) stress is realized.
Some things to think about:
What is the failure mechanism that you are trying to protect the systems against? The B31 Codes are fatigue-based codes (since 1955) and the (allowable stress range) rules therein will provide protection against fatigue failures as long as the system "shakes down" to elastic response in a FEW operating cycles. If you are really seeing calculated stresses that exceed yield upon the application of the design temperature, then it is possible that you will have plastic deformation of the pipe during the blow-down event. Then there is the possibility that you will have a stress reversal when the system temperature returns to ambient and this might result in a reversed plastic deformation ("cold"). If this happens once a year, you might wonder how many years it would take for the alternating plastic response to cause enough racheting to fail the pipe.
Is the temperature RANGE (delta T) really from the (theoretically "stressless") installed temperature (e.g., 70 degrees F) to the 500 degree design temperature (delta T = 430 degrees)? Or does it include the contraction temperature excursion from "installed temperature" to (system shut down on a cold winter night) say -20 degrees F. (delta T = 520 degrees)? According to the Code, you do have to evaluate the 520 degree F. temperature stress range but this "Code analysis" assumes that the system will "shake down" to elastic response in a few cycles. If the installed to 500 degree temperature excursion does not result in a stress greater than (hot material) yield and the installed to -20 degree temperature excursion does not result in a stress greater than (cold material) yield then it is likely that racheting will not occur. Then, the fatigue rules would apply but you still would have to show a calculated stress range that is less than the Code allowable stress range. It is interesting to consider that the total temperature excursion from -20 degrees F. to 500 degrees F. is the REAL full temperature cycle. How often does this really happen? All lesser (than 520 degrees F.) temperature excursions ( say 70 degrees F. to 500 degrees F.) are "partial" cycles and the paragraph 102.3.2 (C) rules for "equivalent full temperature cycles" apply.
The B31 Mechanical Design Committee passed rules several years ago that will allow (with small numbers of thermal cycles) stress range "reduction" factors (i.e., "F") greater than 1.0. It remains to be seen when if ever this will get into the various "book sections".
I think that you are going to have to simply accept the limit on allowable stress range as the Code presents it and "build the church for the Easter crowd" by redesigning to get
your "once per year" stress range below the Code allowable stress range.
Just my opinion.