1. Field of the Invention
The present invention pertains to internal mechanical stress improvement for mitigating stress corrosion cracking in weld areas of piping, in particular, nozzles, safe ends (nozzle extension pieces) and pipes used in nuclear power plants.
2. Brief Discussion of the Related Art
Stress corrosion cracking and failure of nickel alloy pressure boundaries have been observed in nuclear reactor plant component applications since the 1980s. Most of the failures have been observed in wrought nickel alloy materials with less than 20% chromium, like NiCrFe Alloy 600, used in components exposed to reactor coolant environments, at high temperatures (typically greater than 600° F.), and at high stresses (typically greater than 80% of yield strength). Cracking has also been observed in weld areas using nickel alloy weld material, such as Alloy 82 and Alloy 182, which are widely used in the nuclear industry for joining dissimilar metals, such as stainless steel to low-alloy steel reactor plant nozzle-to-piping welds.
As a result of weld cracking, the nuclear industry must perform more frequent in-service weld inspections. Nuclear plants that have not mitigated such weld areas must perform ultrasonic inspections in reactor vessel nozzles every five years, and this incurs a very high cost per inspection. An ultrasonic inspection often requires an extra core barrel removal operation and a three-day outage extension. In addition to inspection requirement, plants with unmitigated welds are exposed to the risk associated with stress corrosion cracking developing in the weld areas.
To mitigate potential for cracking and to obtain relief from frequency of inspections, there is a need in the nuclear industry for economical mitigation of Alloy 82/182 welds in reactor vessel piping. As used herein, “piping” means all fluid conduits in nuclear power plants including, but not limited to, pipes, nozzles and safe ends.
The initiation of cracking can be mitigated and the growth of preexisting small cracks can be arrested by creating a deep compressive stress field on the internal or wetted surface of the Alloy 82/182 weld area. This can be done by imposing a carefully engineered large deformation layer (i.e., beyond yield strength or greater than 0.2% strain) on the piping at the weld area.
Some methods have been developed and applied that can mitigate the cracking susceptibility of the internal weld surface by techniques applied to the outside (i.e., dry) surface of the piping. However, access to the outer surfaces is not always practicable in nuclear power plant piping. Examples of this include, but are not limited to, designs for which the locations of the welds occur within radiation shields typically formed of reinforced concrete of substantial thickness (typically five feet), or occur in areas to which external access is restricted by equipment or by high radiation levels, or are entirely inside the reactor vessel (such as instrumentation penetrations).
In plants that do not have access to the outside (i.e., dry) surface of the piping weld areas, economical mitigation of such weld areas is particularly challenging. In the past, attempts to internally (i.e., from the wetted side) mitigate cracking in Alloy 82/182 weld areas have included performing internal weld on-lay and internal surface peening. The weld on-lay process is prohibitively expensive and risks significant delays if a problem occurs in accepting the final weld condition. Internal surface peening methods, such as water jet peening, laser peening and laser shock peening, have the disadvantage of creating only a very shallow compressive stress field (less than 1 mm or 0.04 inches deep) on the peened surface, cannot be confirmed by post-process measurements and cannot stop pre-existing small cracks which are deeper than the shallow peened metal layer. Neither of these methods is currently relied on for mitigation in the U.S. and neither method has an identified path to relief of weld inspection frequency requirements.
The present invention relates to internal methods and apparatus for mitigating stress corrosion crack growth in internal weld areas in piping in a nuclear power plant by the direct application of large radial forces to the internal (i.e., wetted) surface of the weld areas of the piping, thereby creating a deep residual compressive stress state on the target weld area. This internal mechanical stress improvement method permits mitigation of welds solely by forces applied directly to the normally wetted surfaces (e.g., by access via the inside of a reactor vessel) of piping, as compared with the prior art external (i.e., dry surface) mechanical methods.
In accordance with the present invention, flaw or crack growth in a piping weld area is arrested by creating a deep compressive stress field on the inside (i.e., wetted) surface of the weld area, such as Alloy 82/182 weld areas in nuclear power plant nozzles and piping. Methods according to the present invention create compressive stress fields on the wetted surface of the weld areas to be mitigated by imposing a large deformation using radial force applied to the wetted surface of the piping by an operating end of a tool located at the area of the weld.
A primary aspect of the present invention is to mitigate cracking in weld areas in piping of nuclear power plants by applying radial forces to the internal surface of the weld area to create deep residual compressive stress at the weld area. Various tools and apparatus can be utilized to create the large radial forces including wedge, roller and pneumatic arrangements through mechanical, hydraulic and/or pneumatic devices.
Some of the advantages of the present invention over the prior art are that stress mitigation can be achieved by applying radial forces internally of piping at a weld area thereby overcoming the issues associated with weld areas that are not externally accessible.
Other aspects and advantages of the present invention will become apparent from the following description of the preferred embodiments taken in conjunction with the accompanying drawings wherein like parts in each of the several figures are identified by the same reference characters.
There are many reasons why an internally applied stress mitigation device is preferred to an externally applied device, such as inaccessibility, physical interferences or impractical environment. One example is a nuclear power plant having an externally obstructed reactor vessel nozzle configuration as shown in
Weld areas are illustrated in
In accordance with the present invention, as shown in
In accordance with the present invention, large radial loads are directly applied to the weld area on the internal (wetted) surface of the piping (e.g. nozzle or safe end) by a radially movable member 26 to create, after removal of the member, a deep residual compressive stress state on the wetted surface of the weld area to mitigate stress corrosion cracking of the weld. A deep layer is one that extends about 25% or more through the wall thickness as opposed to a method that only affects the surface (e.g., less than 1 millimeter) stress condition.
The shape and axial location of the member 26 that is used to plastically deform the wetted weld area is important for developing the optimum residual stress field at the wetted weld surface. For a pipe-to-nozzle butt weld, while the form of the member shown in
Various tools can be utilized to provide application of sufficient radial force around the circumference of the piping at the weld area to cause the inside fibers of the piping (e.g. nozzle, safe end) to yield plastically. After the force is released, a compressive axial and circumferential residual stress field is created on the internal (i.e., wetted) surface of the weld area as shown in
Some examples of tools/devices that can be utilized with the method of the present invention are shown in
Another example of a tool for use in radial expansion of weld areas in accordance with the present invention is shown in
As will be appreciated, the tools shown in
The J-groove weld 10′ shown in
Inasmuch as the present invention is subject to many variations, modifications and changes in detail, it is intended that ail subject matter discussed above or shown in the accompanying drawings be interpreted as illustrative only and not be taken in a limiting sense.
The subject patent application is a continuation-in-part of U.S. patent application Ser. No. 13/942,608, filed Jul. 15, 2013, the entire disclosure of which is incorporated herein by reference.
Number | Date | Country | |
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Parent | 13942608 | Jul 2013 | US |
Child | 14622431 | US |