XYLENE POWER LTD.

FNR ACTUATOR

By Charles Rhodes, P.Eng., Ph.D.

INTRODUCTION:
A FNR Actuator is a linear actuator that raises or lowers a movable fuel bundle over a range of 1.1 m for insertion or withdrawal of that movable fuel bundle from the matrix of fixed fuel bundles. This insertion must be precise, smooth and hysterisis free. The insertion occurs against the force of gravity. The withdrawal is assisted by the force of gravity. The mass of a FNR movable fuel bundle is about 2.4 tonnes. A hysterisis free vertical position resolution of about 0.01 mm is desired.

OPEN AREA FRACTION:
Consider the fraction of open area for sodium rising through a fuel bundle between the fuel tubes. At most this fraction is:
[(5 inch / 8)^2 - Pi (1 inch / 4)^2] / (5 inch / 8)^2
= [0.390625 - 0.196350] / 0.390625
= 0.49734

This fraction is slightly reduced by the spiral wire winding and is further reduced over time by cumulative fuel tube swelling.

To obtain the required bending resistance we choose a movable fuel bundle support pipe which is 8 inch schedule 160 steel pipe that has an OD of 8.625 inch and an ID of 6.813 inch.

8.625 inch = 69 X (1 / 8) inch

6.813 inch = 54.5 X (1 / 8) inch ~ 55 X (1 / 8) inch

Now consider the fraction of open area for sodium rising past an 8.625 inch OD movable fuel bundle support pipe but confined within the movable fuel bundle shroud:
[(17 X 5 inch / 8)^2 - Pi (8.625 inch / 2)^2] / (17 X 5 inch / 8)^2
= [112.890625 - 58.42626] / 112.890625
= 0.482452

Note that these two open area fractions fractions are so close that we can adopt a movable fuel bundle with a 8.625 inch OD without concern for it significantly obstructing the natural sodium flow, provided that sodium can flow laterally over the top of the fuel bundle support pipe.

The movable fuel bundle grating area potentially obstructed by the movable fuel bundle support pipe is:
Pi (8.625 inch / 2)^2

The entry area for sodium flowing over the top of the movable fuel bundle support pipe is:
Pi (8.625 inch) D
where D is the axial distance between the top of the support pipe and the bottom of the grating. In order to maintain the same cross sectional area for sodium flow:
[Pi (8.625 inch) D] / [Pi (8.625 inch / 2)^2] = 0.5
or
4 D / 8.625 inch = 0.5
or
D = 8.625 inch / 8
~ 9 / 8 inch

These parameters indicate that the threaded shaft should be 6.0 inches OD which on the diagram is approximated by 49 / 8 inch

The actuator shown contains a (49 / 8) inch diameter 1.5 m high vertical threaded steel shaft located directly under the center of the movable fuel bundle. The bottom of this shaft is supported by a thrust bearing. This shaft has a:
6.625 onch OD = 53 / 8 inch OD axial drive gear mounted close its bottom end. This axial drive gear is realized by machining teeth onto the outside of a piece of 6 inch schedule 80 pipe (6.625 inch OD, 5.761 inch ID). The bottom end of the threaded shaft is machined down to 5.761 inches (146.329 mm) to accommodate the axial drive gear and is further reduced to 140 mm diameter to fit the bottom thrust bearing. This axial drive gear is driven by a hydraulic motor acting through a 1.5 inch diameter horizontal axis worm gear.

Bidirectional rotation of the worm gear causes a 3 inch high hex lifting nut on the 6 inch diameter threaded shaft to move up and down over a height range of about 1.1 m. The 8.625 inch OD, 6.813 inch ID round movable fuel bundle support pipe slides loosely over the threaded shaft. The bottom end of the movable fuel bundle support pipe fits over the lifting nut with a slot that prevents the lifting nut from rotating as the threaded shaft rotates. The vertical forces on the lifting nut are born by a set of small diameter radial screws. These screws are chosen so tha they will fail in shear if the vertical force becomes too large, as in an impact to the FNR that might affect its fuel geometry. When these screws fail the movable fuel bundle will fall to its fully retracted position.

Rotation of the worm gear causes the movable fuel bundle to slowly move up or down.

The 8.625 inch movable fuel bundle support pipe OD slides through a matching slightly larger diameter hole in a guide plate and ball bearing mounted on the top surface of the open steel lattice. This hole provides the movable fuel bundle lateral stability when the movable fuel bundle is totally withdrawn (at its lowest position) and the adjacent fixed fuel bundles are not present. The top of this hole is slightly conical to assist in blind insertion of the movable fuel bundle support pipe into this hole. The 6 inch diameter threaded shaft projects through and slightly above this hole to also assist in blind insertion of the movable fuel bundle support pipe.

The hex lifting nut keeps the movable fuel bundle at its the last set elevation.

The worm gear fits between the axial drive gear and one side of the movable fuel bundle space allocation.

The worm gear is driven by a bidirectional hydraulic motor. The hydraulic motor assembly shares the same shaft as the worm gear. Each actuator is field replaceable whereas replacement of the open steel lattice requires major work. Note that for field replacement the threaded shaft and its axial drive gear (6.625 inch OD) can be lowered through the upper guide plate hole and ball bearing (8.625 inch ID).

The open steel lattice components are too large to fit through an airlock.

The two hydraulic pressure tubes feeding each hydraulic motor are snaked along the bottom of the open steel lattice.

The required hydraulic pressure is provided by gravity feed from two overhead liquid sodium tanks. One tank feeds one set of shutdown movable fuel bundles. the other tank feeds the other set of movable fuel bundles. The feed valves to the hydraulic motor connections that cause fuel bundle withdrawal are normally open. The remaining feed valves are normally closed. Hence loss of station control power causes drain down of the contents of the overhead Na tanks through the hydraulic motors that cause movable fuel bundle withdrawal.

A movable fuel bundle has a mass of about 2.4 tonnes. Hence the actuator must be sufficiently robust to dependably support, position and stabilize this mass. When the movable fuel bundle is fully withdrawn the threaded rod and the movable fuel bundle support pipe must hold the movable fuel bundle vertical. The threaded shaft and the movable fuel bundle support pipe must both be of sufficient diameter that they will not fail due to worst case shear force. Hence the need for a 8.625 inch OD thick wall movable fuel bundle support pipe with a 6.0 inch diameter threaded shaft.

The OD of the axial drive gear is:
6.625 inch = 53 / 8 inch

The axial drive gear is heat shrunk on to an unthreaded end portion of the threaded shaft.

The matching worm gear minimum threaded length is about:
3 X (5 / 8) inch = 15/8 inch

The hydraulic motor parts must fit under (1 / 4) of the adjacent fixed fuel bundle space allocation so as to permit multiple hydraulic motors to overlap the same fixed fuel bundle space allocation.

An advantage of this actuator design is that there is almost no vertical movement hysterisis. When there is no hydraulic fluid flow to the hydraulic motor the movable fuel bundle remains at its last set vertical position. This mechanical configuration provides excellent FNR fuel geometry stability.

Each hydraulic motor has two dedicated hydraulic lines, one for causing movable fuel bundle insertion into the matrix of fixed fuel bundles and one for causing movable fuel bundle withdrawal from the matrix of fixed fuel bundles.

The actual vertical position of each movable fuel bundle is monitored via an overhead scan of the elevation of the corresponding indicator tube top.

The actuators fit into to the open steel lattice that supports the FNR fuel bundles.

Assume that the worm gear is realized using commercial threaded rod 1.5 inch diameter. That rod has 6 threads / inch.
 

DIMENSIONS:
The axial drive gear tooth spacing is the same as the worm gear tooth spacing at 6 threads / inch.

Hence number of axial drive gear teeth:
= Pi (53/8) inch X 6 teeth / inch
= 124.878 teeth ~ 124 teeth

Assume that the threaded shaft is 47 / 8 inch outside diameter and has 8 / 3 threads per inch. Then:
124 rotations of the worm gear will cause the movable fuel bundle to rise or fall by (3 / 8) inch. Hence one worm gear rotation causes a change in movable fuel bundle insertion of:
3 inch / 8 (124) = .003024 inch
= .003024 inch X .0254 m / inch
= 7.68 X 10^-5 m
= 76.8 um

Hence to precisely set the FNR temperature setpoint we need to control the worm gear rotation to a fraction of one revolution. That rotation control is achieved via pulse width control of the hydraulic fluid jets that feed the hydraulic motor.

Let Fj be the fluid jet tangential force in the hydraulic motor.

One 360 degree rotation of the worm gear delivers a lifting energy of:
2.4 tonne X 2200 lb / tonne X (3 / 8 inch) / 124 = 15.968 lb-inch.

Assume that the hydraulic tubing is round within an inside diameter of 0.500 inch. Then the hydraulic jet area is:
Pi (0.500 inch / 2)^2 = 0.196 inch^2

Then the minimum hydraulic jet pressure is:
0.968 lb /0.196 inch^2 = 4.94 lb / inch^2

In reality, due to stiction and imperfect energy transfer in the hydraulic motor we probably need 3X this pressure. In order to provide for rapid emergency movable fuel bundle withdrawal this pressure should be provided by two gravity feed tanks mounted near the ceiling of the primary pool space. The downflow liquid sodium pipes need to each be of the order of 8 inch ID to provide a sufficient surge flow of liquid sodium when all the actuators are simultaneously demanding service.

The hydraulic tubing must be routed behind and between the intermediate heat exchange bundles such that in an earthquake the fuel assembly can move horizontally with respect to the primary sodium pool walls at least 0.5 m in any direction without the hydraulic lines sustaining any physical damage. It is probably prudent to route this hydraulic tubing through conduits for physical protection where it crosses over the pool deck.

The hydraulic fluid withdrawal control valves should be normally open and the insertion contrl valves should be normally closed so as to default to the withdrawn position on loss of station power. These valves exist in a 460 degrees C environment. The argon control pressure is turned on by normally closed solenoid valves which open when energized and which are located outside the primary sodium pool space. The argon control pressure lines can be teflon to provide a thermal break.

Assume that the hydraulic tubes are evenly spaced around the perimeter of the primary sodium pool. Then the average tube to tube center to center distance is:
[Pi (20 m) - 8 m] / [2 (464 movable bundles)] = 0.059 m
That is sufficient space for 0.375 inch ID tubing with compression fittings.

A practical pressurized hydraulic fluid source may be an immersed pump that pumps to an overhead gravity pressure tank used for actuator operation.
 

HYDRAULIC MOTOR POSITION:
The hydraulic motor should be supported and oriented so that its CW and CCW fluid input ports are on top and its fluid discharge port is on the bottom but still well above the primary sodium pool floor. The issue is that we want any dirt that finds its way into the hydraulic system to fall out via the hydraulic motor fluid discharge port, which should be on the bottom.
 

ACTUATOR PERFORMANCE STABILITY:
Each FNR Actuator relies on smooth meshing of the worm gear with the flat gear. Both the bottom of the threaded shaft and the worm gear shaft must be firmly supported so that this smooth gear meshing is sustained far into the future. It might be prudent to have an automatic test sequence that from time to time sequentially runs every movable fuel bundle up and down by a controlled amount to demonstrate that the actuators continue to work as designed and that the fuel bundles have not been subject to swelling or other problems that might cause a movable fuel bundle jam.
 

MECHANICAL RIGIDITY CONSIDERATIONS:
A major issue in fuel bundle design is horizontal mechanical stability and rigidity because the overall fuel bundle height of 8.0 m is much greater than its width (.3016 m or 0.3651 m). Hence, the mechanical design of the fuel bundles is important to ensure that during fabrication, transport, installation and operation the fuel bundles do not bend, warp or otherwise deform. Such bending or warping might potentially cause a jam in the vertical sliding of a movable fuel bundle within the surrounding matrix of fixed fuel bundles.

A fixed fuel bundle has corner girders which extend down below the fuel tubes to also serve as support legs and attach to the internal diagonal plates that provide lower central support and an upper central lifting point. On installation the corner girders of fixed fuel bundles connect to adjacent fixed fuel bundles via diagonal bolts at the top of each corner girder and by cast fittings at the bottom of each corner girder. These cast fittings are firmly attached to the open steel support lattice. The cast fittings fit inside the fixed fuel bundle legs and are tapered at their tops to allow practical blind mating with the fuel bundle supports with +/- 6 mm position error.

The corner girders of every fixed fuel bundle extend downwards 1.5 m below the bottom of the fuel fuel tube support grating. At the top of the fuel bundle 0.5 m diagonal sheet extensions provide lifting points for fuel bundle installation and removal. Short corner girder upward extensions allow use of diagonal bolts for horizontally connecting together adjacent fixed fuel bundles.
 

The entire weight of the fixed fuel bundles is supported by the four fuel bundle legs and the reinforced diagonal plate extensions. These supports extend 1.5 m below the fuel tube bottoms to allow liquid sodium to easily flow into the bottom of the fuel bundles and to minimize long term fast neutron damage to the open steel lattice.

In operation each movable fuel bundle's weight is borne by the 3.0 inch high lifting nut on the threaded shaft which sets the amount of the movable fuel bundle's insertion into the matrix of fixed fuel bundles. This lifting nut engages 8 threads. The movable fuel bundle travel is limited at the bottom by its 1.1 m of projecting support pipe length after an allowance of 0.4 m for the grating, support pipe to grating space and support pipe adapter fins.
 

PASSIVE FUEL BUNDLES:
In order to achieve fuel bundle interchangability the passive fuel bundles are the same size and are mounted in the same manner as the active fuel bundles. However, the passive fuel bundles are supported by fixed studs so that they are not movable and can not withdraw from the fixed fuel bundle matrix.
 

HORIZONTAL FUEL ASSEMBLY MOVEMENT CLEARANCE:
In an earthquake it is important for the fuel assembly to be able to slide horizontally about half way under the intermediate heat exchange bundle bottom manifold before there is a collision between the fuel assembly and the 12 inch diameter bottom manifold feed pipe. This clearance issue requires careful control the height of the open steel lattice, the height of the fuel bundles and the depth of the intermediate heat exchange bundles.
 

FNR ACTUATOR REPLACEMENT
Sooner or later a particular FNR Actuator will need replacement. All such actuators should fit into an equipment transfer airlock.

This airlock internal width must be about 1.5 m to accommodate intermediate heat exchanger radial piping and the intermediate heat exchange bundle manifold outside diameter.

The open steel lattice is fabricated in sections that are field welded together. The open steel lattice has a flat bottom for low friction sliding over the underlying layer of ball bearings. The open steel lattice bottom plates must smoothly fit together. On top of the bottom plates, directly under the fixed fuel bundles, must be neutron absorbing gravel. This gravel must not be permitted to foul the adjacent movable fuel bundle actuators.
 

This web page last updated August 11, 2022.