Inlet nozzle assembly
A nozzle assembly is described for directing coolant into the duct tube of a fuel assembly attached thereto comprising: an elongated shell having inlet openings adjacent one end thereof for admitting coolant thereinto; an orifice plate assembly in the shell downstream of the inlet openings, neutron shielding means in the shell downstream of the orifice plate assembly; diffusing means in the shell downstream of the neutron shielding means for dispersing the coolant uniformly through the duct tube; the orifice plate assembly comprising separable stacked orifice plates having differently configurated and sized openings, respectively, for directing the coolant therethrough in a predetermined flow pattern. One of the orifice plates includes means for imparting a spiral flow to the coolant, and the shielding means includes a shield block having a central passage for conveying the coolant in a spiral path therethrough. The central passage has at one end thereof a converging inlet adjacent the one orifice plate. The shield block is formed with an annular well surrounding the central passage, and a partition defining in part the central passage and separating the well from the passage.
- Assignee:
- Dept. of Energy, Washington, DC
- Patent Number(s):
- US 4654194
- Application Number:
- TRN: 87-018241
- OSTI ID:
- 6612742
- Resource Relation:
- Patent File Date: Filed date 9 Sep 1985
- Country of Publication:
- United States
- Language:
- English
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Inlet nozzle assembly
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Related Subjects
FUEL ASSEMBLIES
COOLANTS
NOZZLES
ANNULAR SPACE
DUCTS
FLUID FLOW
INTAKE STRUCTURES
NEUTRONS
ORIFICES
SHIELDING
TUBES
BARYONS
CONFIGURATION
ELEMENTARY PARTICLES
FERMIONS
HADRONS
MECHANICAL STRUCTURES
NUCLEONS
OPENINGS
SPACE
220300* - Nuclear Reactor Technology- Fuel Elements