Nuclear fuel assembly with multi-pitch wire wrap
A nuclear fuel assembly is constructed with fuel assembly components that are wire wrapped and positioned in hexagonal rings within a fuel assembly duct. The fuel assembly components positioned in an outermost ring of the fuel assembly are wire wrapped with a pitch that is shorter than fuel assembly components positioned at an interior ring of the fuel assembly. The shorter pitch at the outer ring of the fuel assembly increases pressure drop of a coolant fluid at the edge and corner subchannels and thereby reduces the temperature gradient across the fuel assembly, which provides a higher output temperature of the nuclear reactor without substantially increasing peak temperature of the fuel cladding.
1 . A method for increasing a pressure drop of a coolant fluid within a nuclear fuel assembly in an edge subchannel, comprising:
providing a fuel assembly having a duct and configured to hold a plurality of fuel assembly components arranged in concentric rings within the duct;
positioning a first fuel assembly component within an inner ring of the fuel assembly, the first fuel assembly component being wire wrapped at a first pitch, wherein a first plurality of the fuel assembly components within the inner ring of the fuel assembly create interior subchannels between two or more of the plurality of fuel assembly components within the inner ring;
positioning a second fuel assembly component within an outermost ring of the fuel assembly, the second fuel assembly component being wire wrapped at a second pitch smaller than the first pitch, wherein positioning the second fuel assembly component includes a clocking angle that avoids contact between wire wrappings of the second fuel assembly component and wire wrappings of all immediately adjacent fuel assembly components in both the outermost ring and any adjacent inner ring, and wherein a second plurality of fuel assembly components within the outermost ring create edge subchannels between the second plurality of fuel assembly components and the duct; and
flowing a coolant fluid through the fuel assembly, wherein the wire wrap at the second pitch increases the pressure drop of the coolant fluid flowing through the edge subchannels.
2 . The method of claim 1 , wherein positioning a second fuel assembly component within an outermost ring of the fuel assembly comprises positioning a plurality of second fuel assembly components within the outermost ring of the fuel assembly, wherein each of the plurality of second fuel assembly components is wire wrapped at the second pitch.
3 . The method of claim 1 , further comprising positioning a third fuel assembly component within a penultimate ring of the fuel assembly, the third fuel assembly component being wire wrapped at the second pitch.
4 . The method of claim 1 , wherein the second pitch comprises twice the number of wraps as the first pitch.
5 . The method of claim 1 , wherein the second pitch comprises four times the number of wraps as the first pitch.
6 . The method of claim 1 , wherein the first fuel assembly component has a first clocking angle, and wherein positioning the second fuel assembly component further comprises positioning the second fuel assembly component to have a second clocking angle different from the first clocking angle.
7 . The method of claim 1 , further comprising positioning the first fuel assembly component at a first clocking angle.
8 . The method of claim 7 , further comprising positioning the second fuel assembly component at a second clocking angle different from the first clocking angle.
9 . The method of claim 1 , wherein the first fuel assembly component comprises one or more of fissionable fuel, fertile fuel, a neutron absorber, or a neutron reflector.
10 . The method of claim 1 , further comprising positioning a third fuel assembly component within a penultimate ring of the fuel assembly, the third fuel assembly component being wire wrapped at a third pitch smaller than the first pitch and larger than the second pitch.
11 . The method of claim 10 , further comprising positioning a fourth fuel assembly component within the fuel assembly, the fourth fuel assembly component having a wire wrap at a fourth pitch, the fourth pitch different from the first pitch, the second pitch, and the third pitch.
12 . The method of claim 1 , wherein the first pitch is an integer multiplier of the second pitch.
13 . The method of claim 1 , wherein the second pitch is half of the first pitch.
14 . The method of claim 1 , wherein the first fuel assembly component and the second fuel assembly component are located within a fuel duct and wherein the second fuel assembly component is placed nearer a wall of the fuel duct than the first fuel assembly component.
15 . The method of claim 1 , wherein one or more of the first fuel assembly component and the second fuel assembly component comprises fissionable fuel.
16 . The method of claim 1 , wherein one or more of the first fuel assembly component and the second fuel assembly component comprises fertile fuel.
17 . The method of claim 1 , wherein one or more of the first fuel assembly component and the second fuel assembly component comprises a neutron absorber.
18 . The method of claim 1 , wherein the first fuel assembly component is wire wrapped in a first rotational direction about a longitudinal axis of the first fuel assembly component, and wherein the second fuel assembly component is wire wrapped in the first rotational direction about a longitudinal axis of the second fuel assembly component.
19 . The method of claim 1 , wherein the first fuel assembly component is wire wrapped at the first pitch with a single continuous wire in a helical pattern.