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{{Adams
{{Adams
| number = ML13350A219
| number = ML003739418
| issue date = 02/28/1977
| issue date = 03/31/1978
| title = Stress Allowables for the Design of Shipping Cask Containment Vessels
| title = (Revision 1), Design Criteria for Structural Analysis of Shipping Cask Containment Vessels
| author name =  
| author name =  
| author affiliation = NRC/RES
| author affiliation = NRC/RES
Line 10: Line 10:
| license number =  
| license number =  
| contact person =  
| contact person =  
| document report number = RG-7.006
| document report number = RG-7.6 Rev 1
| document type = Regulatory Guide
| document type = Regulatory Guide
| page count = 4
| page count = 4
}}
}}
{{#Wiki_filter:*. .:..G) .(ou@ U.~...I NUCLEAO REG"LATORY
{{#Wiki_filter:Revision 1 March 1978 U.S. NUCLEAR REGULATORY COMMISSION
COMMISSION'" n e l eibruaryh1977
                                      REGULATORY GUIDE
*OFFICE OF STANDARDS  
                                      OFFICE OF STANDARDS DEVELOPMENT
:DEV ELOPM ENT-REGULATORY  
                                                                      REGULATORY GUIDE 7.6 DESIGN CRITERIA FOR THE STRUCTURAL ANALYSIS OF
GUIDE-7.8 STRESS ALLO WABLES FOR THE DESIGN OF:SHIPPING.
                                                    SHIPPING CASK CONTAINMENT VESSELS
 
CASK CONTAINMENT  
VESSELS'


==A. INTRODUCTION==
==A. INTRODUCTION==
aind thev allowthe use, of superposition in stimming loaiding týffcfls.
those given in this guide on a case-by-case basis.


De~sign stress ifltefsitiesar dL usel.Se.'tions
Sections 71.35 and 71.36 of 10 CFR Part 71,
7 a.35:and ,,1136 Of 10 CFR Part 7.. h-bCauseLestablished naterial V tlutsfor this use ist ,...ackaging..of Radioactive .NMtaterial for Tranisport. -in',Iih4 th 1 E'.d. C and,.bccause this impproach is...: Tr tnsport of b icUd aeon hI i niaxixmunif shear stress the~or-...'h;i6  Certa.un reqirementst "t h"huni sh0,"n to .he ia cnserv ivL cSt mainttcLfthe stress"" Oi.ekaAsusd:i6?
  "Packaging of Radioactive Material for Transport                                            Section III of the ASME Boiler and Pressure Code t and Transportation of Radioactive Material Under                                        contains requirements for the design of nuclear power Certain Conditions," require that packages used to                                      plant components. Portions of the Code that use a transport radioactive materials meet the normal and                                      "design-by-analysis" approach for Class 1 compo I ypothetical accident conditions of Appendices A and                                    nents have been adapted in this guide to form accept B, respectively, to Part 71. This guide describes de                                    able design criteria for shipping cask containment sign criteria acceptable to the NRC staff for use in the                                  vessels. The design criteria for normal transport con structural analysis of the containment vessels of Type                                    ditions, as defined in 10 CFR Part 71, are similar to B packages used to transport irradiated nuclear fuel.                                     the criteria for Level A Service Limits (formerly Alternative design criteria may be used if judged ac                                      called "normal conditions") of Section III, and the ceptable by the NRC staff in meeting the structural                                      design criteria for accident conditions are similar to requirements of §§71.35 and 71.36 of 10 CFR Part                                          those for Level D Service Limits (formerly called
tr'amsp0r.
71.                                                                                      "faulted conditions"). However, Section III was de veloped for reactor components, not fuel casks, and many of the Code's requirements may not be appli


radi'active materials,;-:z tha-iUep istic de re it v , ,-must."mt:
==B. DISCUSSION==
under~normal- and.hypothettcal',accident. ,to,,cxerimntal data- ,,:::: :*0h iti5sUTis uid nios tmib es'd sign criteria ac- :' '," ...-.: ..." "" -'= -, .." ".con ition
cable to fuel cask design.
 
====s. This ====
-gudd rtei C,*. .ceptah.to .the.,N.RCstaforuse the structura
.'In current designs for the nent issels ol th:Icontainment vessels of-type B fuel casks. the nature or t d pressure:p ickages: u sed to transpo r t irradiated nuclear :fuel. loads and the y.c.l i ,,,i (stainle.s MAlternativedesign criteria may"be used if judged ac, steel) re such tha c rle fracture ru not.cptah!-,by the NRC.staff in meeting the structural considered to p I P let Thermal ratchetting requirementsofli§7L.35 and 71.36of 10CFR Part 71. is nol consi ere Iau. I ficulies in cyindrical


==B. DISCUSSION==
At present, there are no design standards that can be directly used to evaluate the structural integrity of                                      The criteria in this guide reflect the designs of re the containment vessels of shipping casks for ir                                          cently licensed shipping casks. The containment ves radiated fuels. This guide presents containment ves                                        sels having these designs were made of austenitic sel design criteria that can be used in conjunction                                        stainless steel, which is ductile even at low temper with an analysis which considers the containment                                          atures. Thus, this guide does not consider brittle frac vessel and other principal shells of the cask (e.g.,                                      ture. Likewise, creep is not discussed because the outer shell, neutron shield jacket shell) to be linearly                                  temperatures of containment vessels for irradiated elastic. A basic assumption for the use of this guide                                      fuel are characteristically below the creep range, is that the principle of superposition can be applied to                                  even after the hypothetical thermal accident require determine the effect of combined loads on the con                                          ment of 10 CFR Part 71. The nature of the design tainment vessel. However, use of this guide does-not                                      cyclic thermal loads and pressure loads is such that preclude appropriate nonlinear treatment of other                                        thermal ratchetting is not considered a realistic fail cask components (e.g., impact limiters and lead                                          ure mode for cylindrical containment vessels. Con shielding).                                                                              tainment vessel designs that are significantly differ Design criteria for nonlinear structural analyses are                                ent from current designs (in shape, material, etc.)
I*N o ' ''"ions 3 and 7 ensure that failure At nresent. there are no desien standards thatican .'e;tt~r ined vieldint.
not presented in this guide because of the present lack                                  may necessitate the consideration of the above failure of data sufficient to formulate substantial nonlinear                                    modes.


hlid ket,* 0..,;.he directly used toevaluate the structurhl integrity or f:Affil ticcur. Secondarv stresses (i.e.. stiesse: the -contairieinnt
criteria. The NRC staff will review criteria other than                                      Copies may be obtained from the American Society of
%lessels of shippingcaksfrr not considered to cause....radiated ruecls. How-vcr. "Section AIl or~he. A E ""-T~l' ieidingar
*Lines indicate substantive changes from previous issue.                                   Mechanical Engineers, United Engineering Center, 345 East
'ni nsiee oc's radiated.fuel.
                                                                                          47th Street, New York, N.Y. 10017.


H eergro s unrestrained Ni-ldbng-hut.
USNRC REGULATORY GUIDES                                          Comments should be sent to the Secretary of the Commission, US. Nuclear Re u latory Commission. Washington, DC. 20555, Attention            Docketing and Servie
                                                                                                                                                                            9 Regulatory Guides are issued to describe and make available to the public methods  Branchy acceptable to the NRC staff of implementing specific parts of the Commission's regulations, to delineate techniques used by the staff in evaluating specific problems The guides are issued in the following ten broad divisions or postulated accidents, or to provide guidance to applicants, Regulatory Guides are not subsirtutes for regulations, and compliance with them is not required          1. Power Reactors                            6  Products Methods and solutions different from those set out in the guides will be accept able if they provide a basis for the fidigs  requisite to the issuance or continuance  2. Research and Test Reactors                7. Transportation of a        or        by the Commiision.


are :considered in Boiler*and Pressure Vessel Code.* n a fatiuu and shakedow n .mnlmls*ments.for thi design of nuclear power it. n corm nents. "The staff has.adaptcd pbrtions of S tion lOf Regulatory Position 4 ensures that fatigue failure"r d csnt Positio 5n cmtr ensure., the to'form acceptabled eria oe notoccur and Reulat Position..for shippiing c, k containment.:vessels.
fermnt  r                                        3, Fuels and Materials Facilities            8. Occupational Health ncense                              4. Environmental and Siting                  9  Antitrust Review
                                                                                          5. Materials and Plant Protection          10,  General Comments and suggestions for improvements in these guides are encouraged at all        Requests for single copies of issued guides which may be reproduced) yr for place times, and guides will be revised, as appropriate, to accommodate comments and          ment on an automatic distribution list for single copies of future guides in specilic to reflect new information or experience. This guide was revised as a result of        divisions should be made in writing to the U.S. Nuclear Regulatory Commission substantive comments received from the public and additional staff review.             Washington, 0.C      20555, Attention      Director. Division of Document Control


In I.I guide. .that- the structureswill shake down to elastic behavior criteria for.s mcask containment Vest :after afew c\ cles. Both of these positions deal only*.st~ls ~r..normal conditii ( fined in 10 CFR Part ..ithehstress rane of normal operation.
Regulatory positions 2 and 6 ensure that failure                    than load-controlled, and these stresses decrease as due to gross unrestrained yielding across a solid sec                  yielding occurs.


A reduc-71). are'.similar Ntgcdi r ctr, ia-in Section III of tion. in the aIIowitble stress for-lire exceeding.10' -cv-the ASME.Co fo 'as. components under nor- : ces is specificd:in, Reulator, Position 4 since:use of* al condj* n and I de ign criteria for.* accident the~ 10:Cvclycvalue for greater lives* mnia not preserve condit'fr those for-faulted conditions an amdequate design margin for all cases.inw the ý' Co .. a, :) :': : The desit criteria :.presented hcre arc based primnarily on lin ear elastic analyses.
tion does not occur. Secondary stresses (i.e., stresses that are self-limiting) are not considered to cause                        The bending stress at a gross structural discon gross unrestrained yielding but are considered in                      tinuity, such as where a cylindrical shell joins a flat fatigue and shakedown analyses.                                         head, is generally self-limiting and is considered to be a secondary stress. However, when the edge mo Regulatory position 3 ensures that fatigue failure                  ment at the shell and head junction is needed to pre does not occur, and regulatory position 4 ensures that                  vent excessive bending stresses in the head, the stress the structure will shake down to elastic behavior after                at the junction is considered a primary stress. The a few cycles. Both of these positions address only the                 bending stress at a joint between the walls of a rec stress range of normal operation. Recent studies 2                      tangular cross-section shell is considered a primary have shown that fatigue strength decreases beyond                      stress.


Linear.. elastic analyses are simpler than truc elastic-plastic analyses."'Copies may be obtained;
10' cycles for certain material
from. the American.


Society or Mechanical Engineers, United Engineering Center. 345 East 47th Street. New York. N.Y. 10017.Regulatory Position 8 places a limit on the extreme rance of.tht tot ilstresses due to initial fahrication and the norial: opr ating and accident states ol" the containment vesseL The followking terms are presented with the delini-tions used in this guide: U N CREGULATORY
====s. Regulatory position====
G IDES, t~i C~lnik'tn
3.b addresses the possibility of fatigue strength re                      4. Primary membrane stress means the average duction beyond 10' cycles.                                             normal primary stresses across the thickness of a solid section. Primary bending stresses are the com Regulatory position 5 states that buckling of the                  ponents of the normal primary stresses that vary containment vessel should not occur. While it is rec                    linearly across the thickness of a solid section.
011411IdW
-1 14.1~ , 111:- Slwict..9l v I IN Ot,:t.'-.'
icfJ;.'tt.


thu~itr ie l! iý" ~totE ,git,,meine!
ognized that local or gross buckling of the contain ment vessel could occur without failure (i.e., leak                        5. Alternating stress intensity, Sait, means one age), the stress and strain limits given in this guide                  half the maximum absolute value of S'2, Sý3, S;,, for are based on linear elastic analysis and are inappro                    all possible stress states i and j where 0-, 0"2 , and ("3 priate for determining the integrity of a postbuckled                    are principal stresses and vessel. If the analysis of a containment vessel indi cates the likelihood of structural instability, the de                              S'12 = (o1i -    G"1,)  - (0"'i  0-2 i)
jiý tiaks~e a uiart~.t the pulcmethodss~
sign criteria of this guide should not be used.                                    Sý3 =  (0r 2 i - 92i) -   (o` 3 1 S'31 = (0-3i -   0-3 i) - (0'H
faluly o40tt4ih"llI
    Regulatory position 7 places a limit on the extreme range of the total stresses due to the initial and fabri
.,2blA-1-1D~
                                                                        0-7, etc., follow the principal stresses as their direc cation states (see definition 9 below) and the normal tions rotate if the directions of the principal stresses operating and accident states of the containment ves at a point change during the cycle.
!";--11S1 1tS t ottt Jet4 lt .iii ffl ttvttil In, the. 4 fl4in to aliln Slc ii Rt, ittn Gublern.;a'! nut ast.etit uvts fto re 0 4 llt tons, antl 0.tintI.iflrp wilth tt14Cm isno, rftwified.


1. I'owl,- flea Jtu% I.. Pttoijur'l v1,1 tiltsoulno4s dif1levent front thousi %410nutin itte,?quitil" will ile .IVcet.t 2. Rnse..11t It,%. Tlst R,,ictms 7. T ,s~~ttc, A .bif .th tI~novie a~~, I t,,u In, the Instltitjs mln~us~tp
sel. The 10-cycle value of Sa (taken from the ASME
4 tho tim sulatee or conflniiunce
design fatigue curves) is used. Because this value is                      6. Stresses caused by stress concentrations means in the extreme low-cycle range, this regulatory posi                    stress increases due to local geometric discontinuities tion is actually a limit on strain rather than stress.                 (e.g., notches or local thermal "hot spots"). These stresses produce no noticeable distortions.
3., Fuets ntrol Maim ,,ts F itte a .de ocuil.outn.t11 I at peri or jw., Ir itm Coirmivor, -..4, Env,,tinnwntatl anti Sitirnl 9, Anfn,,ttstH'
Corntnnts an'l %urfgvit tris Inimpntfltewtflit%-
iti ttiev- Otatidi .14 encautav.id at all fim. and.rpotle.


o ,nflf.ix:t.,u, t*-4. tlnnt ti1av. Cotl -nimiatS cieihls d R...ttess It, Is~nifle.
Design criteria for bolted closures are not pre sented in this guide. Insufficient information exists,                     7. Type B quantity is defined in §71.4(q) of 10
particularly for response to impact loading, to estab                  CFR Part 71. Normal conditions of transport and lish such criteria.                                                     hypothetical accident conditions are defined in Ap pendices A and B, respectively, to 10 CFR Part 71.


1r-o1nýIII-W
The following terms are presented with the defini tions used in this guide:                                                  8. Containment vessel means the receptacle on which principal reliance is placed to retain the
ii-0 swet ll t 4wr % As,,rh 116v, Iii4.!~w,'it t 41 .to 1,41 lectri" Inom to orniwrrv.
    1. Stress intensity means twice the maximum shear radioactive material during transport.


Ho 'w .C4 1t n on th is q idjif men!,t 0n .40 *tunslntiidtt t i lml4.1 4ti Ii timtli SI t. tt,, , ilIthlefittS
stress and is equal to the largest algebraic difference between any two of the three principal stresses.                            9. Fabrication means the assembly of the major components of the casks (i.e., the inner shell, shield
nett.autt ott tt,. t.4 eil tor an .6irv s.it,. W.0st~o .. U.C, 205!bg. Al ttrit-ri ., -U,. ,twt .ofit Dot T11i.111en
    2. Primarv stress means a stress that is necessary ing, outer shell, heads, etc.) but not the construction to satisfy the laws of equilibrium of forces and mo of the individual components. Thus, the phrase fab ments due to applied loadings, pressure loadings, and ricationstresses includes the stresses caused by inter body (inertial) loadings. Primary stresses are not ference fits and the shrinkage of bonded lead shield self-limiting because local yielding and minor distor ing during solidification but does not include the re tions do not reduce the average stress across a solid sidual stresses due to plate formation, welding, etc.
11:.1,oo,, 0 .
I. Stress intensity'
is defined as twice the maximum shear stress and is equal to the largest algebraic dif-ference between any two of the three principal stres-ses.2. A primary stress is a stress that is necessary to satisfy the laws of equilibrium of forces and moments due to applied loadings, pressure loadings, and body (inertial)  
loadings.


Primary stresses are not self-limiting because local yielding and minor distortions do not reduce the average stress across a solid sec-tion.3. A secondary stress is a stress that is self-limiting.
section.


Thermal stresses are considered to be secondary stresses since they are strain-controlled rather than load-controlled, and these stresses decrease as yielding occurs.The bending stress at a gross structural discon-tinuity, such as where a cylindrical shell joins a flat head, is generally self-limiting and is considered to be a cecondary stress. However. when the edge moment at the shell and head junction is needed to prevent ex-cessive bending stresses in the head, the stress at the junction is cons'idered to be a primary stress. The bending stress at a joint between a rectangular shell and a flat head is unrestrained by hoop effects and will be considered to be a primary stress.4. Primary membrane stresses are the average nor-mal primary stresses across the thickness of a solid section. Primar.1 bendingk stresses are the components of the normal primary stresses that vary linearly across the thickness of a solid section.5. The alternating stress intensity.
The prefabrication 2tate is designated as the initial
    3. Secondary stress means a stress that is self                     state and is treated as having zero stress.


Salt- is defined as one-half the maximum absolute value of S 12, S,)., S'I. for all possible stress states i and j where oa., a02 and u 3 irc principal stresses and SC2= (Oi -frlj) -(o2i -'2j)S!3 = (a -a2j )" (03i -a3)Sit. (3i -a3j)-(ali
limiting. Thermal stresses are considered to be sec
-Or1j)* 1, etc., follow the principal stresses as their direc-tions rotate if the directions of the principal stresses at a point change during the cycle.6. The phrase stresses caused b ' stress concentra- tions refers to increases in stresses due to local geometric discontinuities (e.g., notches or local ther-mal "hot spots"). These stresses produce no noticeable distortions.
                                                                            10. Shakedown means the absence of a continuing ondary stresses since they are strain-controlled rather cycle of plastic deformation. A structure shakes down if, after a few cycles of load application, the deforma
2 C. E'. Jaske and W. J. O'Donnell, 'Fatigue Design Criteria for      tion stabilizes and subsequent structural response is Pressure Vessel Alloys,' ASME Paper 77-PVP-12.                         elastic.


7. TIpe B quantitv isdefined in §71.4(q)of
L
10CFR Part 71. Normal conditions of transport and hypothetical accident conditions are defined in Appen-dices A and B, respectively, to 10 CFR Part 71.8. Containmeni vessel is defined as the receptacle on which principal reliance is placed to retain the radioactive material during transport.
                                                                  7.6-2


C. REGULATORY  
==C. REGULATORY POSITION==
POSITION The following design criteria are acceptable to the NRC staff for assessing the adequacy of designs for shipping cask containment vessels in meeting the structural requirements in §§71.35 and 71.36 of 10 CFR Part 71.I. The values for material properties.
4. The stress intensity, Sn, associated with the range of primary plus secondary stresses under nor The following design criteria are acceptable to the         mal conditions should be less than 3 Sm. The calcula NRC staff for assessing the adequacy of designs for           tion of this stress intensity is similar to the calcula containment vessels of irradiated fuel shipping casks          tion of 2 Salt; however, the effects of local stress con in meeting the structural requirements in §§7 1.35 and centrations that are considered in the fatigue calcula
  71.36 of 10 CFR Part 71. References to the ASME                tions are not included in this stress range.


design stress intensities (Sil), and design fatigue curves for Class I components given in Subsection NA of Section III of the ASME Boiler and Pressure Vessel Code should be used for the materials listed in that subsection.
Boiler and Pressure Vessel Code indicate the 1977 edition.                                                          The 3Sm limit given above may be exceeded if the following conditions are met (these conditions can I. The values for material properties, design stress       generally be met only in cases where the thermal intensities (Sm), and design fatigue curves for Class 1        bending stresses are a substantial portion of the total components given in Subsection NA of Section III               stress):
of the ASME Boiler and Pressure Vessel Code should                   a. The range of stresses under normal condi be used for the materials that meet the ASME specifi            tions, excluding stresses due to stress concentrations cations. For other materials, the method discussed in         and thermal bending stresses, yields a stress inten Article III -2000 of Subsection NA should be used to            sity, Sn, that is less than 3Sm.


For materials not listed there, the method discussed in Article 111-2000 of Subsection NA should be used to derive design stress intensity values. ASTM material properties should be used, if available, to derive design stress intensity values. The values of material properties that should be used in the structural analysis are those that correspond to the appropriate temperatures at loading.2. Strain-rate-sensitive material properties may be used in the evaluation of impact loading if the values used are appropriately considered in a dynamic time-dependent analysis and can be suitably justified in the license application.
derive design stress intensity values. ASTM material properties should be used, if available, to derive de                b. The value Sa used for entering the design sign stress intensity values. The values of material           fatigue curve is multiplied by the factor Kg, where:
properties that should be used in the structural analy            K. = 1.0, for Sn--3Sm sis are those values that correspond to the appropriate
                                                                          =1.0+n(m      -)(-m-   ), for 3Sm<Sn<3mSn temperatures at loading.


When strain rate sensitivity is considered in the structural response to a combination of static and dynamic loads, the static portion of the stresses and strains should be analyzed separately using static material properties and should meet the static design criteria.
-    , for Sn > 3mSm
    2. Under normal conditions, the value of the stress                  n intensity resulting from the primary membrane stress should be less than the design stress intensity, Si,          Sn is as described in regulatory position 4.a.


The total stress and strain state resulting from both static and dynamic loads should meet the design criteria for which strain-rate-sensitive material rroperties (e.g., yield strength)
and the stress intensity resulting from the sum of the             The values of the material parameters m and n are primary membrane stresses and the primary bending             given for the various classes of materials in the fol stresses should be less than 1.5Si.                             lowing table:
are substituted for static values.3. Under normal conditions the value of the stress intensity resulting from the primary membrane stres-ses should be less than the design stress intensity, Sm, and the stress intensity resulting from the sum of the primary membrane stresses and the primary bending stresses should be less than 1.5Sm.4. The fatigue analysis for stresses under normal conditions should be performed as follows: a. Salt is determined (as defined in the "Discus-sion"). The total stress state at each point in the nor-mal operating cycle should be considered so that a maximum range may be determined.
                                                                                                                  Tmax
    3. The fatigue analysis for stresses under normal                                               m    n    'F    &deg;C
conditions should be performed as follows:                     Low-Alloy Steel                    2.0  0.2  700  371 a. Sa1t is determined (as defined in the Discus         Martensitic Stainless Steel        2.0  0.2  700  371 sion). The total stress state at each point in the nor         Carbon Steel                        3.0  0.2  700  371 mal operating cycle should be considered so that a             Austenitic Stainless Steel          1.7  0.3  800  427 maximum range may be determined.                                Nickel -Chromium-Iron              1.7  0.3  800  427 b. The design fatigue curves in Appendix I of Section III of the ASME Boiler and Pressure Vessel Code should be used for cyclic loading less than or                    c. The temperatures do not exceed those listed equal to 106 cycles. Cornsideration should be given to          in the above table for the various classes of materials.


b. The design fatigue curves (Figures 1-9.0) of Section III of the ASME Boiler and Pressure Vessel Code should be used. These curves include the max-imum mean stress effect.7.6-2 c. Salt should be multiplied by the ratio of the modulus of elasticity given on the design fatigue curve to the modulus of elasticity used in the analysis to obtain a value of stress to be used with the design fatigue curves. The corresponding number of cycles taken from the appropriate design fatigue curve is the allowable life if only one type of operational cycle is considered.
further reduction in fatigue strength when loading ex                  d. The ratio of the minimum specified yield ceeds 10' cycles.                                               strength of the material to the minimum specified ul timate strength is less than 0.8.


If two or more types of stress cycles are considered to produce significant stresses, the rules for cumulative damage given in Article NB-3222.4 of Section III of the ASME Boiler and Pressure Vessel Code should be applied.d. In the analysis of high cycle fatigue where the number of cycles exceeds 104 cycles, the ASME design fatigue curves should be extended using a 4%decrease in the allowable stress per decade, starting from the IO0 cycle value. High cycle fatigue could be a potential problem due to vibration during transpor-tation.e. A value of 4 should be used as the maximum stress concentration factor in regions where this fac-tor is unknown.5. The stress intensity, Sn, associated with the range of primary plus secondary stresses under nor-mal conditions should be less than 3Sm. The calcula-tion of this stress intensity is similar to the calculation of 2 Salt; however, the effects of local stress con-centrations that are considered in the fatigue calcula-tions are not included in this stress range.The 3 Sm limit given above may be exceeded if the following conditions arc met (these conditions can generally be met only in cases where the secon-dary bending stresses are a substantial portion of the total stress): a. The range of stresses under normal condi-tions excluding stresses due to stress. concentrations and secondary bending stresses yields a stress inten-sity, Sn, that is less than 3 Sm.b. The value Sa used for entering the design fatigue curve is multiplied by the factor Ke, where: Ke = 1.0 (Snr < 3 Sm)(I-n) (Sn _ I=1.0+ n(m- ik3Sm 1_(3 Sm<Sn<3 mSm)=1 (Sn -.3 mSm)n n Sn is as described in a.The values of the material parameters m and n are given for the various classes of materials in the fol-lowing table: Low Alloy Steel Martensitic Stainless Stec Carbon Steel Austenitic Stainless Steel Nickel-Chromium-Iron m n Trnax.0 F 2.0 0.2 700 2.0 0.2 700 3.0 0.2 700 1.7 0.3 800 1.7 0.3 800 c. The temperatures do not exceed those listed in the above table for the various classes of materials.
c. SaIt should be multiplied by the ratio of the modulus of elasticity given on the design fatigue                   5. Buckling of the containment vessel should not curve to the modulus of elasticity used in the analysis        occur under normal or accident conditions. Suitable to obtain a value of stress to be used with the design        factors, should be used to account for eccentricities in fatigue curves. The corresponding number of cycles            the design geometry and loading. An elastic-plastic taken from the appropriate design fatigue curve is the         buckling analysis may be used to show that structural allowable life if only one type of operational cycle is        instability will not occur; however, the vessel should considered. If two or more types of stress cycles are          also meet the specifications for linear elastic analysis considered to produce significant stresses, the rules          given in this guide.


d. The ratio of the minimum specified yield strength of the material to the minimum specified ultimate strength is less than 0.80.6. Buckling of the containment vessel should not occur under normal and accident conditions.
for cumulative damage given in Article NB-3222.4 of Section III of the ASME Boiler and Pressure Ves                6. Under accident conditions, the value of the sel Code should be applied.                                    stress intensity resulting from the primary membrane stresses should be less'than the lesser value of 2 .4Sm d. Appropriate stress concentration factors for          and 0.7S, (ultimate strength); and the stress intensity structural discontinuities should be used. A value of 4        resulting from the sum of the primary membrane should be used in regions where this factor is un              stresses and the primary bending stresses should be known.                                                        less than the lesser value of 3 .6Sm and Su.


7. Under accident conditions, the value of the stress intensity resulting from the primary membrane stresses should be less than the lesser value of 2.4Sm and 0.7Su (ultimate strength):
7.6-3
and the stress intensity resulting from the sum of the primary membrane stresses and the primary bending stresses should be less than the lesser value of 3.6Sm and Su..8. The extreme total stress intensity range between the initial zero stress state, fabrication, normal opera-tion. and accident conditions should be less than twice the adjusted value (adjusted to account for modulus of elasticity at the highest temperature)
of Sa at 10 cycles given by the appropriate design fatigue curves.A value of 4 should be used as the maximum stress concentration factor in regions where this fac-tor is unknown.9. In some cask designs. shielding materials apply loads through differential thermal expansion or supp-ly additional strength to the containment vessel. In such cases, shielding materials that have low yield strengths (e.g., lead) may be structurally analyzed us-ing an elastic-plastic technique while the inner shell is analyzed by a linear elastic analysis.


When uranium is used for shielding and is needed to add strength to the containment vessel, the fracture behavior of the uranium shielding should he considered.
7. The extreme total stress intensity range between    cycles given by the appropriate design fatigue curves.


7.6-3 Ii .D0
the initial state, the fabrication state (see definition 9 in the Discussion), the normal operating conditions,          Appropriate stress concentration factors for struc and the accident conditions should be less than twice      tural discontinuities should be used. A value of 4 the adjusted value (adjusted to account for modulus of elasticity at the highest temperature) of Sa at 10
                                                            should be used in regions where this factor is unknown.


==J. IMPLEMENTATION==
I
1I,-pUrp'os o N his section. is to provide infornma-16n , .:ppII&#xfd;l Ints:- lien ezs rardingj the N RC stahrt~. plan wror Lil.i n .this regulatory guide.I w.-.cpt in thl %L t.s case i n h~ich thL dfplpic nt 'or icnu proposes .mndmet.ptatl ahk letrilativt method.t'or conilpI\ ing;wtth ,pecified portions ol*.tht Conmris%I.J)NITED
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STATES* NUCLEAR REGULATO11Y
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COMMISSION
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INAS H IN rTON; D. C. 20555* OFFICIAL BUSINESS PE~NALTY IFOR PRIVATE USE. S300 sions regulahtions., the design criteria described herein%, ill be used bh the starr mter October I .1977. in as-.se.sing the. adequacy or designs. ur coiltainnient:.,ces-" LI 0l" packages for shipping irradiated fuel with respect to the structural rcquiremcnis in and 7.1-36 .of I..CI"R. Part7 71. When alternative criteria.roposed...ti.applicant or licensee should denitinrtr tl'heir use satisfies the: requirements of -&sect;,7 T3 5mAnd 71 36 o 1 10 CF R Part .71.POSTAOE AND FEEs PAID I*NUCLAR RC.ULA.ORV
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Latest revision as of 11:38, 28 March 2020

(Revision 1), Design Criteria for Structural Analysis of Shipping Cask Containment Vessels
ML003739418
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Issue date: 03/31/1978
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Download: ML003739418 (4)


Revision 1 March 1978 U.S. NUCLEAR REGULATORY COMMISSION

REGULATORY GUIDE

OFFICE OF STANDARDS DEVELOPMENT

REGULATORY GUIDE 7.6 DESIGN CRITERIA FOR THE STRUCTURAL ANALYSIS OF

SHIPPING CASK CONTAINMENT VESSELS

A. INTRODUCTION

those given in this guide on a case-by-case basis.

Sections 71.35 and 71.36 of 10 CFR Part 71,

"Packaging of Radioactive Material for Transport Section III of the ASME Boiler and Pressure Code t and Transportation of Radioactive Material Under contains requirements for the design of nuclear power Certain Conditions," require that packages used to plant components. Portions of the Code that use a transport radioactive materials meet the normal and "design-by-analysis" approach for Class 1 compo I ypothetical accident conditions of Appendices A and nents have been adapted in this guide to form accept B, respectively, to Part 71. This guide describes de able design criteria for shipping cask containment sign criteria acceptable to the NRC staff for use in the vessels. The design criteria for normal transport con structural analysis of the containment vessels of Type ditions, as defined in 10 CFR Part 71, are similar to B packages used to transport irradiated nuclear fuel. the criteria for Level A Service Limits (formerly Alternative design criteria may be used if judged ac called "normal conditions") of Section III, and the ceptable by the NRC staff in meeting the structural design criteria for accident conditions are similar to requirements of §§71.35 and 71.36 of 10 CFR Part those for Level D Service Limits (formerly called

71. "faulted conditions"). However,Section III was de veloped for reactor components, not fuel casks, and many of the Code's requirements may not be appli

B. DISCUSSION

cable to fuel cask design.

At present, there are no design standards that can be directly used to evaluate the structural integrity of The criteria in this guide reflect the designs of re the containment vessels of shipping casks for ir cently licensed shipping casks. The containment ves radiated fuels. This guide presents containment ves sels having these designs were made of austenitic sel design criteria that can be used in conjunction stainless steel, which is ductile even at low temper with an analysis which considers the containment atures. Thus, this guide does not consider brittle frac vessel and other principal shells of the cask (e.g., ture. Likewise, creep is not discussed because the outer shell, neutron shield jacket shell) to be linearly temperatures of containment vessels for irradiated elastic. A basic assumption for the use of this guide fuel are characteristically below the creep range, is that the principle of superposition can be applied to even after the hypothetical thermal accident require determine the effect of combined loads on the con ment of 10 CFR Part 71. The nature of the design tainment vessel. However, use of this guide does-not cyclic thermal loads and pressure loads is such that preclude appropriate nonlinear treatment of other thermal ratchetting is not considered a realistic fail cask components (e.g., impact limiters and lead ure mode for cylindrical containment vessels. Con shielding). tainment vessel designs that are significantly differ Design criteria for nonlinear structural analyses are ent from current designs (in shape, material, etc.)

not presented in this guide because of the present lack may necessitate the consideration of the above failure of data sufficient to formulate substantial nonlinear modes.

criteria. The NRC staff will review criteria other than Copies may be obtained from the American Society of

  • Lines indicate substantive changes from previous issue. Mechanical Engineers, United Engineering Center, 345 East

47th Street, New York, N.Y. 10017.

USNRC REGULATORY GUIDES Comments should be sent to the Secretary of the Commission, US. Nuclear Re u latory Commission. Washington, DC. 20555, Attention Docketing and Servie

9 Regulatory Guides are issued to describe and make available to the public methods Branchy acceptable to the NRC staff of implementing specific parts of the Commission's regulations, to delineate techniques used by the staff in evaluating specific problems The guides are issued in the following ten broad divisions or postulated accidents, or to provide guidance to applicants, Regulatory Guides are not subsirtutes for regulations, and compliance with them is not required 1. Power Reactors 6 Products Methods and solutions different from those set out in the guides will be accept able if they provide a basis for the fidigs requisite to the issuance or continuance 2. Research and Test Reactors 7. Transportation of a or by the Commiision.

fermnt r 3, Fuels and Materials Facilities 8. Occupational Health ncense 4. Environmental and Siting 9 Antitrust Review

5. Materials and Plant Protection 10, General Comments and suggestions for improvements in these guides are encouraged at all Requests for single copies of issued guides which may be reproduced) yr for place times, and guides will be revised, as appropriate, to accommodate comments and ment on an automatic distribution list for single copies of future guides in specilic to reflect new information or experience. This guide was revised as a result of divisions should be made in writing to the U.S. Nuclear Regulatory Commission substantive comments received from the public and additional staff review. Washington, 0.C 20555, Attention Director. Division of Document Control

Regulatory positions 2 and 6 ensure that failure than load-controlled, and these stresses decrease as due to gross unrestrained yielding across a solid sec yielding occurs.

tion does not occur. Secondary stresses (i.e., stresses that are self-limiting) are not considered to cause The bending stress at a gross structural discon gross unrestrained yielding but are considered in tinuity, such as where a cylindrical shell joins a flat fatigue and shakedown analyses. head, is generally self-limiting and is considered to be a secondary stress. However, when the edge mo Regulatory position 3 ensures that fatigue failure ment at the shell and head junction is needed to pre does not occur, and regulatory position 4 ensures that vent excessive bending stresses in the head, the stress the structure will shake down to elastic behavior after at the junction is considered a primary stress. The a few cycles. Both of these positions address only the bending stress at a joint between the walls of a rec stress range of normal operation. Recent studies 2 tangular cross-section shell is considered a primary have shown that fatigue strength decreases beyond stress.

10' cycles for certain material

s. Regulatory position

3.b addresses the possibility of fatigue strength re 4. Primary membrane stress means the average duction beyond 10' cycles. normal primary stresses across the thickness of a solid section. Primary bending stresses are the com Regulatory position 5 states that buckling of the ponents of the normal primary stresses that vary containment vessel should not occur. While it is rec linearly across the thickness of a solid section.

ognized that local or gross buckling of the contain ment vessel could occur without failure (i.e., leak 5. Alternating stress intensity, Sait, means one age), the stress and strain limits given in this guide half the maximum absolute value of S'2, Sý3, S;,, for are based on linear elastic analysis and are inappro all possible stress states i and j where 0-, 0"2 , and ("3 priate for determining the integrity of a postbuckled are principal stresses and vessel. If the analysis of a containment vessel indi cates the likelihood of structural instability, the de S'12 = (o1i - G"1,) - (0"'i 0-2 i)

sign criteria of this guide should not be used. Sý3 = (0r 2 i - 92i) - (o` 3 1 S'31 = (0-3i - 0-3 i) - (0'H

Regulatory position 7 places a limit on the extreme range of the total stresses due to the initial and fabri

0-7, etc., follow the principal stresses as their direc cation states (see definition 9 below) and the normal tions rotate if the directions of the principal stresses operating and accident states of the containment ves at a point change during the cycle.

sel. The 10-cycle value of Sa (taken from the ASME

design fatigue curves) is used. Because this value is 6. Stresses caused by stress concentrations means in the extreme low-cycle range, this regulatory posi stress increases due to local geometric discontinuities tion is actually a limit on strain rather than stress. (e.g., notches or local thermal "hot spots"). These stresses produce no noticeable distortions.

Design criteria for bolted closures are not pre sented in this guide. Insufficient information exists, 7. Type B quantity is defined in §71.4(q) of 10

particularly for response to impact loading, to estab CFR Part 71. Normal conditions of transport and lish such criteria. hypothetical accident conditions are defined in Ap pendices A and B, respectively, to 10 CFR Part 71.

The following terms are presented with the defini tions used in this guide: 8. Containment vessel means the receptacle on which principal reliance is placed to retain the

1. Stress intensity means twice the maximum shear radioactive material during transport.

stress and is equal to the largest algebraic difference between any two of the three principal stresses. 9. Fabrication means the assembly of the major components of the casks (i.e., the inner shell, shield

2. Primarv stress means a stress that is necessary ing, outer shell, heads, etc.) but not the construction to satisfy the laws of equilibrium of forces and mo of the individual components. Thus, the phrase fab ments due to applied loadings, pressure loadings, and ricationstresses includes the stresses caused by inter body (inertial) loadings. Primary stresses are not ference fits and the shrinkage of bonded lead shield self-limiting because local yielding and minor distor ing during solidification but does not include the re tions do not reduce the average stress across a solid sidual stresses due to plate formation, welding, etc.

section.

The prefabrication 2tate is designated as the initial

3. Secondary stress means a stress that is self state and is treated as having zero stress.

limiting. Thermal stresses are considered to be sec

10. Shakedown means the absence of a continuing ondary stresses since they are strain-controlled rather cycle of plastic deformation. A structure shakes down if, after a few cycles of load application, the deforma

2 C. E'. Jaske and W. J. O'Donnell, 'Fatigue Design Criteria for tion stabilizes and subsequent structural response is Pressure Vessel Alloys,' ASME Paper 77-PVP-12. elastic.

L

7.6-2

C. REGULATORY POSITION

4. The stress intensity, Sn, associated with the range of primary plus secondary stresses under nor The following design criteria are acceptable to the mal conditions should be less than 3 Sm. The calcula NRC staff for assessing the adequacy of designs for tion of this stress intensity is similar to the calcula containment vessels of irradiated fuel shipping casks tion of 2 Salt; however, the effects of local stress con in meeting the structural requirements in §§7 1.35 and centrations that are considered in the fatigue calcula

71.36 of 10 CFR Part 71. References to the ASME tions are not included in this stress range.

Boiler and Pressure Vessel Code indicate the 1977 edition. The 3Sm limit given above may be exceeded if the following conditions are met (these conditions can I. The values for material properties, design stress generally be met only in cases where the thermal intensities (Sm), and design fatigue curves for Class 1 bending stresses are a substantial portion of the total components given in Subsection NA of Section III stress):

of the ASME Boiler and Pressure Vessel Code should a. The range of stresses under normal condi be used for the materials that meet the ASME specifi tions, excluding stresses due to stress concentrations cations. For other materials, the method discussed in and thermal bending stresses, yields a stress inten Article III -2000 of Subsection NA should be used to sity, Sn, that is less than 3Sm.

derive design stress intensity values. ASTM material properties should be used, if available, to derive de b. The value Sa used for entering the design sign stress intensity values. The values of material fatigue curve is multiplied by the factor Kg, where:

properties that should be used in the structural analy K. = 1.0, for Sn--3Sm sis are those values that correspond to the appropriate

=1.0+n(m -)(-m- ), for 3Sm<Sn<3mSn temperatures at loading.

- , for Sn > 3mSm

2. Under normal conditions, the value of the stress n intensity resulting from the primary membrane stress should be less than the design stress intensity, Si, Sn is as described in regulatory position 4.a.

and the stress intensity resulting from the sum of the The values of the material parameters m and n are primary membrane stresses and the primary bending given for the various classes of materials in the fol stresses should be less than 1.5Si. lowing table:

Tmax

3. The fatigue analysis for stresses under normal m n 'F °C

conditions should be performed as follows: Low-Alloy Steel 2.0 0.2 700 371 a. Sa1t is determined (as defined in the Discus Martensitic Stainless Steel 2.0 0.2 700 371 sion). The total stress state at each point in the nor Carbon Steel 3.0 0.2 700 371 mal operating cycle should be considered so that a Austenitic Stainless Steel 1.7 0.3 800 427 maximum range may be determined. Nickel -Chromium-Iron 1.7 0.3 800 427 b. The design fatigue curves in Appendix I of Section III of the ASME Boiler and Pressure Vessel Code should be used for cyclic loading less than or c. The temperatures do not exceed those listed equal to 106 cycles. Cornsideration should be given to in the above table for the various classes of materials.

further reduction in fatigue strength when loading ex d. The ratio of the minimum specified yield ceeds 10' cycles. strength of the material to the minimum specified ul timate strength is less than 0.8.

c. SaIt should be multiplied by the ratio of the modulus of elasticity given on the design fatigue 5. Buckling of the containment vessel should not curve to the modulus of elasticity used in the analysis occur under normal or accident conditions. Suitable to obtain a value of stress to be used with the design factors, should be used to account for eccentricities in fatigue curves. The corresponding number of cycles the design geometry and loading. An elastic-plastic taken from the appropriate design fatigue curve is the buckling analysis may be used to show that structural allowable life if only one type of operational cycle is instability will not occur; however, the vessel should considered. If two or more types of stress cycles are also meet the specifications for linear elastic analysis considered to produce significant stresses, the rules given in this guide.

for cumulative damage given in Article NB-3222.4 of Section III of the ASME Boiler and Pressure Ves 6. Under accident conditions, the value of the sel Code should be applied. stress intensity resulting from the primary membrane stresses should be less'than the lesser value of 2 .4Sm d. Appropriate stress concentration factors for and 0.7S, (ultimate strength); and the stress intensity structural discontinuities should be used. A value of 4 resulting from the sum of the primary membrane should be used in regions where this factor is un stresses and the primary bending stresses should be known. less than the lesser value of 3 .6Sm and Su.

7.6-3

7. The extreme total stress intensity range between cycles given by the appropriate design fatigue curves.

the initial state, the fabrication state (see definition 9 in the Discussion), the normal operating conditions, Appropriate stress concentration factors for struc and the accident conditions should be less than twice tural discontinuities should be used. A value of 4 the adjusted value (adjusted to account for modulus of elasticity at the highest temperature) of Sa at 10

should be used in regions where this factor is unknown.

I

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