Three-dimensional multi-shell insulation
First Claim
1. A three-dimensional multi-shell insulation for insulating at least one portion of a spacecraft, the insulation comprising:
- a plurality of nested shell layers of progressively increasing size that are configured to at least partially surround the at least one portion of the spacecraft, each of the plurality of shell layers having layer edge portions on opposite sides of said each of the plurality of the shell layers, and said each of the plurality of shell layers having a layer major portion extending between the layer edge portions; and
at least one edge clamp operatively coupled to the plurality of shell layers at the respective layer edge portions on at least one side of the shell layers;
wherein each layer major portion has at least one layer major surface configured to be spaced apart from an opposing layer major surface of an adjacent shell layer for minimizing thermal conduction between the shell layers; and
wherein the respective layer major surfaces of each of the plurality of nested shell layers are configured to be spaced apart when the insulation is in use in a low-gravity and/or low-pressure environment;
wherein the at least one edge clamp is configured to maintain spacing between the respective layer major surfaces of the shell layers when the insulation is in use in a low-gravity and/or low-pressure environment; and
wherein each of the layer major portions of the plurality of shell layers has at least one abutment, the respective abutments of the adjacent shell layers being configured to provide a stop when engaging each other, thereby restricting the amount of relative lateral displacement between the adjacent shell layers.
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Accused Products
Abstract
A three-dimensional multi-shell insulation configured to conform to the shape of a spacecraft component to be insulated. The insulation may have a plurality of nested shell layers that are displaceable relative to each other for providing natural separation between the shell layers when the insulation is used in low-pressure and/or low-gravity space-related applications. To establish the spacing between shell layers, an edge clamp may be operatively coupled to an edge portion on at least one side of each shell layer. The shell layers may have sufficient flexibility and/or may be sufficiently displaceable relative to each other to allow the insulation to be installed or removed from the spacecraft component. One or more restraints may be provided in the space between the shell layers for restricting the relative lateral and/or transverse movement between shell layers for preventing contact. Additive manufacturing may be employed to fabricate the insulation and integrate features.
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Citations
16 Claims
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1. A three-dimensional multi-shell insulation for insulating at least one portion of a spacecraft, the insulation comprising:
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a plurality of nested shell layers of progressively increasing size that are configured to at least partially surround the at least one portion of the spacecraft, each of the plurality of shell layers having layer edge portions on opposite sides of said each of the plurality of the shell layers, and said each of the plurality of shell layers having a layer major portion extending between the layer edge portions; and at least one edge clamp operatively coupled to the plurality of shell layers at the respective layer edge portions on at least one side of the shell layers; wherein each layer major portion has at least one layer major surface configured to be spaced apart from an opposing layer major surface of an adjacent shell layer for minimizing thermal conduction between the shell layers; and
wherein the respective layer major surfaces of each of the plurality of nested shell layers are configured to be spaced apart when the insulation is in use in a low-gravity and/or low-pressure environment;wherein the at least one edge clamp is configured to maintain spacing between the respective layer major surfaces of the shell layers when the insulation is in use in a low-gravity and/or low-pressure environment; and wherein each of the layer major portions of the plurality of shell layers has at least one abutment, the respective abutments of the adjacent shell layers being configured to provide a stop when engaging each other, thereby restricting the amount of relative lateral displacement between the adjacent shell layers. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
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Specification