1. Field of the Invention
The present invention relates to a clamp, and, more particularly, the present invention relates to a repair device for use, for example, with boiling water reactor jetpumps.
2. Description of the Related Art
While the present invention may be used in a variety of industries, the environment of a boiling water reactor (BWR) nuclear power plant will be discussed herein for illustrative purposes. In a BWR, a steam-water mixture is produced when reactor coolant (water) moves upward through the core, absorbing heat produced by the fuel. The steam-water mixture leaves the top of the core and enters a moisture separator, where water droplets are removed before the steam is allowed to enter the steam line. The steam line directs the steam to the main turbine, causing it to turn the turbine and the attached electrical generator. The steam is then exhausted to a condenser where it is condensed into water. The resulting water is pumped out of the condenser back to the reactor vessel, Recirculation pumps and jet pumps allow the operator to vary coolant flow through the core and change reactor power.
Within the BWR vessel, core shrouds surround the core to provide a barrier to separate the downward coolant flow through the annulus/downcomer (the space between the core shroud and the reactor vessel wall) from the upward flow through the core and fuel bundles. In a typical boiling water reactor, jet pumps are located in the downcomer and provide forced flow of coolant through the reactor vessel in order to yield higher reactor power output than would be possible with natural circulation. Twenty jet pumps are located in two semicircular groups in the annular downcomer region of the reactor. Two jet pumps and a common inlet header or riser pipe comprise a jet pump assembly as shown in
Inlet risers 5 are utilized for each jet pump assembly 1 to permit the reactor recirculation inlet nozzles to be located below the active fuel region. This prevents significant fast neutron exposure which could adversely affect the mechanical properties of the nozzle penetration welds. Additionally, riser brace arms 11 provide lateral support for the upper end of the jet pump assembly 1 and also allow for the vertical differential expansion between the riser 2 and the reactor vessel during plant heat-up and cool-down.
The inlet mixer elbow 7 and converging nozzle 8 sections redirect the coolant flow stream 180° and increase the velocity of the flow stream as the coolant passes through the nozzle 8. This increase in fluid flow velocity results in lower static pressure of the driving flow. This decreased static pressure in the upper end of the inlet mixer 5 draws higher pressure water from the downcomer plenum and the two flows (driving and drive are then combined together in the mixing section 9 of the inlet mixer 5. The inlet mixer 5 interfaces with the diffuser assembly 6 at the slip joint 12 of the jet pump. The slip joint 12 provides means to remove the inlet mixer assembly 5 from a jet pump assembly 1 and also accommodates the differential thermal expansion that occurs in the jet pump assembly 1 during plant heat-up and cool-down. This differential thermal expansion is the result of the riser pipe 2 being anchored in the low alloy carbon steel of the reactor vessel and the differing lengths of stainless steel jet pump components. The inlet mixer assemblies 5 are supported laterally by a restrainer bracket 13 that is welded to the riser pipe 2. The gravity wedge 10 of the inlet mixer and two opposing set screws that are mounted to the restrainer bracket 13 are designed to restrain the inlet mixer 5.
The inlet mixers 5 are subject to flow induced vibration resulting from the mixing action of the drive and driven flow components in the mixing section 9 of the inlet mixer 5. In addition, unstable pressure fluctuations result from the passage of coolant through the slip joint 12 to the lower pressure downcomer annulus. Consequently, abnormal wear of jet pump assembly 1 components has been experienced at several BWR plants. Components affected have been the inlet mixer 5 and diffuser collar 6 at the slip joint location 12, and the gravity wedge 10 and interfacing surface of the restrainer bracket 13. Isolated cracking has also been experienced at the set screw tack welds, riser brace 11 to riser pipe 2 weld, and short radius elbow 3 to thermal sleeve weld.
Thus, there is a need to provide a simple mechanical device which will minimize or limit coolant leakage at the slip joint location and also provide supplemental structural support to the jet pump assembly.
The jet pump stabilizer disclosed and claimed herein restricts coolant leakage at the jet pump slip joint. A clamp body is provided in two parts to interconnect around the jet pump riser pipe. In this manner, it can be placed in position without removal of any jet pump assembly components. Two U-clamps are connected to the clamp body, each U-clamp fitted around a separate one of the jet pump inlet mixer pipes. A wedge subassembly is positioned intermediate the riser pipe and each mixer pipe. The wedge assemblies impart a force to the mixer pipe in a direction that is substantially opposite the force imparted to the mixer pipe by the U-clamp. Thus, the mixer is restrained against movement, including flow-induced vibration. The connections between the U-clamp and the clamp body can incorporate mating spherical seats to accommodate any misalignment between the two mixer pipes and the riser pipe.
A clamp ring is provided for each jet pump mixer. Each clamp ring is provided in two parts to interconnect around the jet pump mixer pipe. In this manner, the clamp rings can be placed in position without removal of any jet pump assembly components. An outboard portion (that is, a portion away from the riser pipe) of each clamp ring is placed between the U-clamp and the mixer pipe, and may be mechanically connected thereto. An inboard portion (that is, a portion towards or adjacent to the riser pipe) of each clamp ring is placed between the wedge and the mixer pipe, and may be mechanically connected thereto. In this manner, the clamp ring is held in the desired position about the jet pump inlet mixer. A seal, preferably a malleable seal, may be provided on the inner perimeter of the clamp ring such that it is in contact with the mixer above the slip joint. This clamp ring seal limits leakage past the jet pump slip joint in an upward direction.
A sealing ring is attached to each clamp ring. Each sealing ring is provided in two parts to interconnect around the jet pump mixer pipe. In this manner, the sealing rings can be placed in position without removal of any jet pump assembly components. Each sealing ring is connected to its corresponding clamp ring by one or more spring-biased connection pins, allowing movement of the sealing ring relative the clamp ring. A seal, preferably a malleable seal, may be provided on a lowermost portion of the sealing ring. The springs bias the sealing ring downward, causing the seal to contact the jet pump diffuser collar below the slip joint. This sealing ring seal limits leakage past the jet pump slip joint in a downward direction. Slots may be provided in the sealing ring to accommodate the jet pump diffuser guide vanes. The relative movement between the sealing ring and the clamp ring accommodate any thermal expansion or contraction at the slip joint.
The present invention is described with reference to the accompanying drawings, which illustrate exemplary embodiments and in which like reference characters reference like elements. It is intended that the embodiments and figures disclosed herein are to be considered illustrative rather than restrictive.
The inboard 31 and outboard 32 semi-circular clamp segments are configured with an opposing tongue-and-groove design to ensure proper alignment of these two clamp segments. Additionally, slots are provided in the seal ring 36 to allow for clearance with the diffuser 6 guide vanes. These engineered slots are sized to minimize slip joint coolant leakage by providing a tight fit with the diffuser guide vanes.
Malleable metal seals 39 may be integrated into the clamp 33 and seal 36 rings to provide a more positive seal against coolant leakage. A preferred spatial orientation of these metal seals is depicted in the cross-sectional view of
The inlet mixer restraint assembly 50 preferably includes a right clamp subassembly 51 and a left clamp subassembly 52.
One of the clamp body portions 51, 52 may be provided with one or more “tongue” features 57 that interface with a corresponding pair of mating “groove” features 58 that may be provided on the other clamp body 52, 51. This tongue-and-groove arrangement can help ensure proper subassembly alignment and ease of remote installation. For example, the right clamp body 51 can incorporates a pair of tongue features 57 that interface with a pair of mating groove features 58 of the left clamp body 52 as shown in the illustrated embodiments of
The as-built distance between the riser pipe 2 and the inlet mixer 5 preferably is stabilized by a system of wedges 60. A preferred system of wedges 60 is illustrated in
In order to eliminate shear stress in the U-clamp bolts 71, pockets can be provided in the right 51 and left 52 clamp bodies. As shown in the cross-sectional view of
Optionally, in lieu of relying solely on friction to maintain the slip joint clamp 30 in position on the jet pump inlet mixer 5, stop bolts 75 and accompanying stop bolt keepers 76 can be employed. As illustrated in
This disclosed jet pump stabilizer design restricts coolant leakage at the jet pump slip joint 12, accommodates thermal expansion at the slip joint 12, provides additional lateral support to the inlet mixers 5, accommodates misalignment between the riser pipe 2 and adjacent inlet mixers 5, and can be installed without removal of any jet pump assembly components, such as the inlet mixer 5.
While the preferred embodiments of the present invention have been described above, it should be understood that they have been presented by way of example only, and not of to limitation. It will be apparent to persons skilled in the relevant art that various changes in form and detail can be made therein without departing from the spirit and scope of the invention. Thus the present invention should not be limited by the above-described exemplary embodiments, but should be defined only in accordance with the following claims and their equivalents. Furthermore, while certain advantages of the invention have been described herein, it is to be understood that not necessarily all such advantages may be achieved in accordance with any particular embodiment of the invention. Thus, for example, those skilled in the art will recognize that the invention may be embodied or carried out in a manner that achieves or optimizes one advantage or group of advantages as taught herein without necessarily achieving other advantages as may be taught or suggested herein.
This patent application claims the benefit of U.S. Provisional Patent Application No. 61/703,734 filed on Sep. 20, 2012, which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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61703734 | Sep 2012 | US |