Wave energy transmission apparatus for high-temperature environments
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorsJohn D. Buckley, William C. Edwards, Warren C. Kelliher, Ingrid A. Carlberg
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Abstract
A wave energy transmission apparatus has a conduit made from a refractory oxide. A transparent, refractory ceramic window is coupled to the conduit. Wave energy passing through the window enters the conduit.
Claims15
A wave energy transmission apparatus for transmitting optical wave energy from a high-temperature environment to a thermally-protected environment, comprising:
- a conic, open-ended tube made from at least one refractory oxide, said tube adapted to be installed in a thermally-protective structure such that said tube extends therethrough, said tube having a tapered end positioned proximate to a sidewall of the structure that will be exposed to a high-temperature environment;
- and
- a transparent window made from an amorphous ceramic selected from the group consisting of yttria and zirconia, said window being bonded into said tube at and flush with said tapered end thereof.
A wave energy transmission apparatus, comprising:
- a thermal protection structure having a first side exposed to a high-temperature environment and a second side that is thermally protected from the high-temperature environment;
- a substantially conically-shaped conduit defined by solid walls made from refractory oxide, said conduit having a first open end and a second open end with a diameter of said first open end being less than a diameter of said second open end, said solid walls further defining an exterior region engaged within said thermal protection structure, said conduit extending from said first side of said structure to said second side of said structure;
- and
- a transparent window fitted into said conduit at and flush with said first open end thereof wherein wave energy entering said first open end passes through said window, said window being made from an amorphous ceramic selected from the group consisting of yttria and zirconia.
A wave energy transmission apparatus for transmitting optical wave energy from a high-temperature environment experienced by a space vehicle during atmospheric re-entry to a thermally-protected environment within the space vehicle, comprising:
- a thermally-protective structure that includes an ablative heat shield adapted to be exposed to the high-temperature environment experienced during atmospheric re-entry;
- an open-ended, concially-shaped tube made from at least one refractory oxide and installed in said thermally-protective structure such that said tube extends therethrough, said tube having an end positioned proximate to said ablative heat shield;
- and
- a transparent window made from an amorphous ceramic selected from the group consisting of yttria and zirconia, said window being bonded into said tube at and flush with said end proximate to said ablative heat shield.
Dependencies are inferred from the claim text.