Patent Number: 052992420
Section: description

DETAILED DESCRIPTION OF THE INVENTION In response to the above needs for space nuclear power, the Small Excore Heat Pipe Thermionic Reactor (SEHPTR) concept was developed. The SEHPTR concept provides an innovative solution to these concerns of potential users of space nuclear power systems. FIG. 1 illustrates the baseline SEHPTR concept, in which a reactor 10 having the control features of the present invention is shown. Heat is generated within a solid annular core 12 at very high temperatures. The core 12 includes tapered hexagonal shaped fuel elements of UO.sub.2 clad in tungsten. The fuel elements are packaged into four fuel bundles which comprise the core. The annular fuel bundles can be removed, allowing for the entire (non-nuclear) power system to be tested with an electrically heated core simulator. Both the inside and outside surfaces of the core radiate the heat to thermionic energy conversion devices 14 which are located around the core 12. The core heat is collected by high temperature annular emitter heat pipes (not shown) that isothermalize the emitter (inside heat pipe) surface both circumferentially and axially. The collector (cold side) is maintained at a constant temperature by molybdenum based sodium heat pipes 18 that run the length of the core and then bend around shield 19 and become an integral part of the radiator 20. In this particular embodiment of the concept, sixty two thermionic heat pipe units are employed to provide redundancy. There are no pumps or circulating core coolant loops associated with this design. The reactor core is designed to operate in the fast neutron energy spectrum, and criticality control is achieved by neutron leakage. Neutrons are reflected back into the core 12 from the periphery by windowed reflectors 22 and 24. This innovation is the subject of the present application and will be explained more fully below. A central poison rod 16 and associated drive mechanism 27 provides a secondary shutdown device at launch and a backup shutdown mechanism after operation begins on orbit. A cross section of the windowed reflector control scheme is depicted in FIG. 2. FIG. 2a shows the reflector control in an operating condition, and FIG. 2b shows the control in a shutdown condition. Movable annular reflector rings 22 and 24 are concentrically assembled and surround the core 12. Reflector 22 is the outer ring while reflector 24 is the inner ring, closest to the core 12. Each reflector ring includes a plurality of reflective portions 26 in an alternating relationship with a plurality of windowed portions 28 spaced around its circumference. The windowed portions 28 of the reflector rings may be simply voids or openings, or may be filled with a non-reflecting material. The core 12 is reflected around the periphery by the reflective portions 26 of the rings 22 and 24. It is preferred that the reflective portions 26 of the rings be BeO. The dual annular reflective rings 22 and 24 control the reactor by rotational movement relative to each other about the core 12. More specifically, reactor control is achieved by allowing neutrons to leak or be reflected by this dual rotating "windowed" reflector. The reactor 10 is shutdown when the inside and outside windowed portions 28 in the reflector rings 22 and 24 are aligned, as shown in FIG. 2b. The openings in each reflector ring are of a size to ensure that when the openings in each reflector are coincident, there is insufficient reflection of neutrons back to the reactor to allow the reactor to attain criticality. The reactor 10 becomes operational as the windowed portions 28 become non-aligned or closed, thus reflecting neutrons back into the core region, as seen in FIG. 2a. The redundant reflector control scheme of the present invention requires that independent drives turn either the inner or outer reflector ring segments in either direction (clockwise or counterclockwise). Referring to FIG. 3, a sectional view of the reactor control and its drive mechanisms is shown. Inner reflector drive shaft 30 is operably connected to inner pinion 32, which turns inner reflector ring gear 34. The ring gear 34 is structurally connected to the annular windowed inner reflector 24. A similar configuration is used for the outer reflector 22. Outer reflector drive shaft 36 is operably connected to outer pinion 38, which turns outer reflector ring gear 40. The ring gear 40 is structurally connected to the annular windowed outer reflector 22. Inner drive shaft 30 and outer drive shaft 36 are each driven by an individual drive motor (not shown). An annular space 42 between the reflectors 22 and 24, and an annular space 44 between the inner reflector 24 and the core 12 minimizes frictional resistance to rotational movement. A torsional spring or other stored energy device may be provided to interconnect the reflector rings 22 and 24. This torsional spring could be used to automatically return each or either reflector to a system unreflected state (i.e. reflector windows 28 aligned one to the other) upon a loss of power to the control drive motors. Fail safe shut down operation of the reactor would thus be achieved with the torsional spring. With the described arrangement, either the inside 24 or outside 22 reflector and its associated drive 30 or 36, respectively, is capable of independently controlling the reactor and providing redundancy. The simplicity of the drive system, the minimum number of moving parts, and the minimal driving distances and torques resulting from the limited rotation needed to form a complete uninterrupted reflector around the core ensures both minimum weight and maximum reliability for the system. To initiate reactor criticality, each reflector is operated independently and rotated in either direction to an extent that the openings in each are no longer aligned. This reduces the leakage of neutrons from the reactor and the reflector functions to reflect the neutrons back to the reactor core where they are used to initiate and sustain the fission process. Only one of the two reflectors need be moved to achieve reflection of the core. The ability to initiate or sustain a critical configuration by movement of either of the reactor reflectors means that two independent means of controlling the reactor reflector are provided, thus greatly enhancing the reliability of the reactor control system. The foregoing description of a preferred embodiment of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching. The embodiment was chosen and described to best explain the principles of the invention and its practical application and thereby enable others skilled in the art to best utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto.