Functionally graded lattice cermet fuel structure with shape corresponding to a mathematically-based periodic solid, particularly for nuclear thermal propulsion applications

US12159727B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12159727-B2
Application numberUS-202318378691-A
CountryUS
Kind codeB2
Filing dateOct 11, 2023
Priority dateApr 1, 2019
Publication dateDec 3, 2024
Grant dateDec 3, 2024

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Nuclear propulsion fission reactor structure has an active core region including fuel element structures, a reflector with rotatable neutron absorber structures (such as drum absorbers), and a core former conformal mating the outer surface of the fuel element structures to the reflector. Fuel element structures are arranged abutting nearest neighbor fuel element structures in a tri-pitch design. Cladding bodies defining coolant channels are inserted into and joined to lower and upper core plates to from a continuous structure that is a first portion of the containment structure. The body of the fuel element has a structure with a shape corresponding to a mathematically-based periodic solid, such as a triply periodic minimal surface (TPMS) in a gyroid structure. The nuclear propulsion fission reactor structure can be incorporated into a nuclear thermal propulsion engine for propulsion applications, such as space propulsion.

First claim

Opening claim text (preview).

What is claimed is: 1. A nuclear fuel lattice structure, comprising: a body having a structure including a plurality of webbings having outer surfaces that define a network of interconnected channels located within an envelope surface of the body, wherein a baseline of the webbings is an implicit surface of a mathematically-based periodic solid, wherein the mathematically-based periodic solid is a triply periodic minimal surface (TPMS), wherein at least a portion of the channels extend from a first outer surface of the body to a second outer surface of the body, wherein the structure has a volumetric density of 35% to 85%, and wherein a composition of the structure includes a nuclear fissionable fuel having an enrichment of up to 20%. 2. The nuclear fuel lattice structure according to claim 1 , wherein the triply periodic minimal surface (TPMS) is a gyroid structure, and wherein the implicit surface is defined by a gyroid equation (sin×cos y+sin y cos z+sin z cos x)=0. 3. The nuclear fuel lattice structure according to claim 2 , wherein each webbing has a thickness relative to the baseline, and, within the body, the thickness of the webbing varies in accordance with a vector field. 4. The nuclear fuel lattice structure according to claim 3 , wherein the thickness of the webbings is symmetric relative to the baseline. 5. The nuclear fuel lattice structure according to claim 3 , wherein the thickness of the webbings is asymmetric relative to the baseline. 6. The nuclear fuel lattice structure according to claim 1 , wherein a uranium content of the nuclear fissionable fuel varies by spatial location in the body. 7. The nuclear fuel lattice structure according to claim 6 , wherein the variation in uranium content by spatial location in the body includes increasing a content of U235 due to an increased density of the lattice. 8. The nuclear fuel lattice structure according to claim 1 , wherein the mathematically-based periodic solid is biased to effect a flow rate of a medium flowing through the network of interconnected channels. 9. The nuclear fuel lattice structure according to claim 1 , wherein the body is disc-shaped and occupies a volume that includes a radial side surface corresponding to a thickness of the body between the first outer surface and the second outer surface. 10. The nuclear fuel lattice structure according to claim 1 , wherein the triply periodic minimal surface (TPMS) is a Schwarz minimal surface. 11. The nuclear fuel lattice structure according to claim 1 , wherein the nuclear fissionable fuel is high-assay low-enriched uranium (HALEU) with a U 235 assay equal to or greater than 5 percent to equal to or lower than 20 percent. 12. The nuclear fuel lattice structure according to claim 1 , wherein the nuclear fissionable fuel includes uranium oxide that is less than 20% enriched, uranium with 10 wt. % molybdenum (U-10Mo), uranium nitride (UN), or a cermet thereof. 13. A nuclear fuel segment, comprising: the nuclear fuel lattice structure according to claim 1 ; and a cladding layer deposited on the outer surfaces of the plurality of webbings that define the network of interconnected channels. 14. The nuclear fuel segment according to claim 13 , wherein the cladding layer has a composition including molybdenum, tungsten, rhenium, tantalum, hafnium and alloys thereof, including carbides. 15. A nuclear reactor structure, comprising: an active core region including a plurality of nuclear fuel segments according to claim 13 , wherein the plurality of nuclear fuel segments are arranged along an axial centerline defining a longitudinal axis of the nuclear reactor structure. 16. The nuclear reactor structure according to claim 15 , wherein the network of interconnected channels in the body of adjacent nuclear fuel segments are aligned to provide fluid communication from a first end surface of the active core to a second end surface of the active core. 17. A nuclear thermal propulsion engine, comprising: the nuclear reactor structure according to claim 15 , wherein the nuclear reactor structure is housed within an interior volume of a hull; shielding; a reservoir for cryogenically storing propulsion gas; turbomachinery; and a nozzle, wherein the shielding, the turbomachinery, and the reservoir are operatively mounted to a first end of the hull to provide a flow path from the reservoir to the nuclear reactor structure, and wherein the nozzle is operatively mounted to a second end of the hull to provide a flow path for superheated propulsion gas exiting the nuclear thermal propulsion engine.

Assignees

Inventors

Classifications

  • Mobile reactors · CPC title

  • Fuel · CPC title

  • Selection of substances for use as neutron-absorbing material · CPC title

  • Ceramic dispersion fuel, e.g. cermet · CPC title

  • Metallic fuel; Intermetallic dispersions · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US12159727B2 cover?
Nuclear propulsion fission reactor structure has an active core region including fuel element structures, a reflector with rotatable neutron absorber structures (such as drum absorbers), and a core former conformal mating the outer surface of the fuel element structures to the reflector. Fuel element structures are arranged abutting nearest neighbor fuel element structures in a tri-pitch design…
Who is the assignee on this patent?
Bwxt Advanced Tech Llc
What technology area does this patent fall under?
Primary CPC classification G21C21/02. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Dec 03 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).