Pneumatic structure and associated production method
US-2023175273-A1 · Jun 8, 2023 · US
US12352055B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12352055-B2 |
| Application number | US-202117997766-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 7, 2021 |
| Priority date | May 7, 2020 |
| Publication date | Jul 8, 2025 |
| Grant date | Jul 8, 2025 |
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The present invention relates to a pneumatic structure ( 10 ) comprising an inextensible body ( 12 ) defining at least a network of internal cavities ( 14 ), each cavity having a closed contour in at least one section of the cavity Each cavity being suitable for being pressurized so as to change the inextensible body from a rest configuration to at least one pressurized configuration, Inextensible body having, in each pressurized configuration, a macroscopic metric different from its macroscopic metric in the rest configuration, Each cavity being formed of at least two substantially rectilinear channels, each channel being fluidly connected to at least one of the other channels, the two said channels forming a heading change angle, Each cavity comprising at least one non-zero heading change angle, in particular at least three non-zero heading change angles.
Opening claim text (preview).
The invention claimed is: 1. A pneumatic structure including an inextensible body defining at least one network of internal cavities, every cavity having a closed contour in at least one section of the cavity, every cavity being suitable for being pressurized so as to change the inextensible body from a rest configuration to at least one pressurized configuration, the inextensible body having, in every pressurized configuration, a macroscopic metric different from the macroscopic metric thereof in the rest configuration, the inextensible body having, in every pressurized configuration, a Gaussian curvature different from the Gaussian curvature in the rest configuration thereof, every cavity being formed from at least two substantially rectilinear channels, every channel being fluidically connected to at least one of the other channels), the two said channels forming a direction changing angle (χ, χ′) at the common end of the channels, every cavity comprising at least one non-zero direction changing angle (χ, χ′). 2. The pneumatic structure according to claim 1 , wherein the Gaussian curvature is zero in the rest configuration and is non-zero in the pressurized configuration. 3. The pneumatic structure according to claim 1 , wherein the value of the direction changing angle (χ, χ′) of every channel varies along a cavity. 4. The pneumatic structure according to claim 1 , wherein every channel has a width (ω−e), defined laterally in said channel and in the rest configuration, less than one third of the length (L) of said channel. 5. The pneumatic structure of claim 1 , wherein at least one cavity comprises a channel separating into at least two channels. 6. The pneumatic structure according to claim 1 , wherein at least one cavity is suitable for receiving an overpressure compared to the atmospheric pressure, the inextensible body being in the rest configuration in the absence of overpressure, the inextensible body being in the pressurized configuration when the internal pressure of every cavity is greater than a deployment pressure equal to the Young's modulus multiplied by the ratio to the cube between the thickness of the inextensible body and the minimum width (ω−e) of the channels. 7. The pneumatic structure according to claim 1 , wherein, in the rest configuration, the inextensible body has a flat shape, that is a flat disk or a rectangle, the pneumatic structure being foldable in said rest configuration. 8. The pneumatic structure of claim 1 , wherein, in the pressurized configuration, the inextensible body defines an outer shell having a three-dimensional shape, the pneumatic structure having a flexural modulus in the pressurized configuration greater than 100 times the flexural modulus of the pneumatic structure in the rest configuration. 9. The pneumatic structure according to claim 1 , wherein the pneumatic structure has a symmetry with respect to a central axis or with respect to a plane of symmetry in the rest configuration. 10. The pneumatic structure according to claim 1 , wherein the inextensible body has a periphery in the rest configuration, every cavity extending peripherally, along a direction substantially tangential to the periphery or along a direction substantially orthogonal to the periphery. 11. The pneumatic structure of claim 1 , wherein the inextensible body defines at least one opening, the ratio between the surface area of the opening and the surface area of the inextensible body being less than 70%. 12. The pneumatic structure according to claim 1 , wherein the inextensible body comprises at least two flat layers with similar contours and welded together. 13. The pneumatic structure according to claim 11 , wherein the inextensible body comprises at least three overlaid layers, the inextensible body defining at least a first network of cavities between two successive layers and at least a second network of cavities between two other successive layers, the first network and the second network being advantageously suitable for being pressurized independently of one another. 14. The pneumatic structure of claim 1 , forming wherein the pneumatic structure is part of: a biomedical equipment item, a furniture component, a leisure equipment item, a tent or a swimming pool, a tableware equipment item, a plate, or an industrial equipment item with adaptable shape, or a formwork for a concrete structure.
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