Abstract: A nuclear fuel assembly having a bottom nozzle with protrusions that extend from the upstream (lower or fluid entry) and downstream (upper or fluid exit) side of a horizontally supported perforated flow plate. The protrusions have a funnel-like shape that gradually decreases the lateral flow area on the upstream side of the perforated flow plate and gradually increases the lateral flow area on the downstream side of the perforated plate. The protrusions on the downstream side are preferably recessed to accommodate the ends of the fuel rods.

Abstract: A nuclear fuel assembly having a bottom nozzle with protrusions that extend from the upstream (lower or fluid entry) and downstream (upper or fluid exit) side of a horizontally supported perforated flow plate. The protrusions have a funnel-like shape that gradually decreases the lateral flow area on the upstream side of the perforated flow plate and gradually increases the lateral flow area on the downstream side of the perforated plate. The protrusions on the downstream side are preferably recessed to accommodate the ends of the fuel rods.

Abstract: In one embodiment, an alignment device may be configured to align a first turbine engine casing and a second turbine engine casing. The alignment device may include a fixed portion configured to be fixedly attached to the first turbine engine casing. The alignment device may also include a bridge portion configured to interface with the second turbine engine casing, wherein the bridge portion defines a first range of motion for the fixed portion along a first axis and a second range of motion for the fixed portion along a second axis when the alignment device is engaged with the first turbine engine casing and the second turbine engine casing, and wherein the alignment device is configured to facilitate movement of the first turbine engine casing relative to the second turbine engine casing within the range of motion and the second range of motion.

Abstract: In one embodiment, an alignment device may be configured to align a first turbine engine casing and a second turbine engine casing. The alignment device may include a fixed portion configured to be fixedly attached to the first turbine engine casing. The alignment device may also include a bridge portion configured to interface with the second turbine engine casing, wherein the bridge portion defines a first range of motion for the fixed portion along a first axis and a second range of motion for the fixed portion along a second axis when the alignment device is engaged with the first turbine engine casing and the second turbine engine casing, and wherein the alignment device is configured to facilitate movement of the first turbine engine casing relative to the second turbine engine casing within the range of motion and the second range of motion.