IP Library Granted Patent US 8,070,105
Granted Patent B2
US 8,070,105 · App. 11/956,826 · Granted Dec 6, 2011

Inflatable nested toroid structure

Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
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Quick Facts
Patent No.
US 8,070,105
App. No.
11/956,826
Granted
Dec 6, 2011
Kind
B2
Abstract

An inflatable structure comprises at least two generally toroidal, inflatable modules. When in a deployed mode, the first, inner module has a major diameter less than that of a second, outer module and is positioned within the inner circumference of the outer module such that the first module is nested circumferentially alongside the second module. The inflatable structure, in a non-deployed, non-inflated mode, is of compact configuration and adapted to be transported to a site of deployment. When deployed, the inflatable structure is of substantially increased interior volume. In one embodiment, access between the interior of the first module and the second module is provided by at least one port or structural pass-through. In another embodiment, the inflatable structure includes at least one additional generally toroidal module external of and circumferentially surrounding the second module.

Claims (24)

1. An inflatable structure adapted for deployment in exoatmospheric space, comprising, upon deployment:

at least two substantially toroidal, inflatable modules, comprising first and second, substantially toroidal, inflatable modules each having a minor diameter;

the second module having a major diameter greater than that of the first module;

the first module and the second module being positioned to one another in a substantially co-planar relationship, the first module being nested circumferentially alongside the second module;

means for operatively connecting the first module and the second module structurally together;

a structural pass-through for providing access between the interiors of the first and second modules, the structural pass-through being configured to allow a human occupant to pass conveniently between the interior volume of the first module and the interior volume of the second module; and

means for shielding the inflatable structure from at least one environmental hazard.

2. The inflatable structure of claim 1 , further comprising a core assembly, the first module circumferentially surrounding the core assembly.

3. The inflatable structure of claim 1 , further comprising means for inflating the first module and the second module.

4. The inflatable structure of claim 1 , wherein the minor diameter of the first module is substantially equal to the minor diameter of the second module.

5. The inflatable structure of claim 1 , further comprising at least one additional inflatable toroidal module having, in its deployed mode, a major diameter greater than that of the second module, the second module being nested concentrically within and circumferentially alongside the at least one additional toroidal module.

6. The inflatable structure of claim 1 , wherein the means for shielding the inflatable structure from at least one environmental hazard comprises a layer of protective material extending over at least portions of the first and second modules.

7. An inflatable structure adapted for deployment in exoatmospheric space, comprising, upon deployment:

at least two substantially toroidal, inflatable modules, comprising first and second, substantially toroidal, inflatable modules each having a minor diameter;

the second module having a major diameter greater than that of the first module;

the first module and the second module being positioned to one another in a substantially co-planar relationship, the first module being nested circumferentially alongside the second module;

means for operatively connecting the first module and the second module structurally together; and

a structural pass-through for providing access between the interiors of the first and second modules, the structural pass-through being configured to allow a human occupant to pass conveniently between the interior volume of the first module and the interior volume of the second module.

8. The inflatable structure of claim 7 , further comprising a core assembly, the first module circumferentially surrounding the core assembly.

9. The inflatable structure of claim 7 , further comprising means for inflating the first module and the second module.

10. The inflatable structure of claim 7 , wherein the minor diameter of the first module is substantially equal to the minor diameter of the second module.

11. The inflatable structure of claim 7 , further comprising means for shielding the inflatable structure from at least one environmental hazard in exoatmospheric space.

12. The inflatable structure of claim 7 , further comprising at least one additional inflatable toroidal module having, in its deployed mode, a major diameter greater than that of the second module, the second module being nested concentrically within and circumferentially alongside the at least one additional toroidal module.

13. The inflatable structure of claim 11 , wherein the means for shielding the inflatable structure from at least one environmental hazard comprises a layer of protective material extending over at least portions of the first and second modules.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2008
From: JOHNSON, CHRISTOPHER J; RABOIN, JASEN L; SPEXARTH, GARY R
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Reel/Frame 020436/0153 →
Continuity (1)
Related Publication 20110180669A1 · Jul 28, 2011