1. Field of the Invention
This invention relates to a cover for use with an inflatable modular structure. The inflatable modular structure can be used as a spaced based platform or a habitat for use on a planet or other extraterrestrial body.
2. Description of the Prior Art
Inflatable modular structures are well known in the art as typified, for example, by U.S. Pat. No. 6,439,508 to Taylor, U.S. Pat. No. 6,231,010 to Schneider, et al, and U.S. Pat. No. 6,547,189 to Raboin, et al.
A major advantage to inflatable structures is that while the internal volume of a typical rigid hulled craft does not vary once deployed into space, the opposite is true for the inflatable structure. Once deployed into orbit, or to an extraterrestrial mass, the inside of the inflatable structure is filled with gas or air. The flexible hull, or shell, expands in response to the gas and, as a result, the internal volume of the inflatable structure increases. Thus, the internal volume of an inflated structure having a flexible hull becomes substantially larger than the volume of a solid hulled structure where both structures have a similar launch payload volume.
This fact translates into a significant cost savings. A single inflatable structure can provide an internal volume equivalent to a number of solid hulled structures. With present costs at approximately $10,000.00 to deploy a single pound of payload into space, a single launch of an inflatable module would provide a volume comparable to a number of launches containing rigid hulled structures. Couple this with the fact that many launch payloads can be several tons in weight, it is immediately apparent that a reduced number of launches saves a considerable amount of money.
While inflatable structures offer a number of advantages to less flexible structures, there are, however, technological challenges to deploying an inflatable module. For example, the flexible hull must be collapsible so that the module can fit into payload compartment of a launch vehicle and secured in place as to prevent unwanted effects arising from the acceleration of a launch on an unsecured mass. This is referred to as the pre-deployment configuration and storage of the hull at this stage should be done in a way such that the launch should not damage the hull.
A typical flexible hull has a number of layers. The internal surface is usually composed of an air bladder. The air bladder acts as a barrier to keep gas internal to the module from escaping into space. A typical air bladder is not very thick and to function optimally it cannot have any leaks. When compacted for launch, it is important that the bladder does not come into contact with surfaces that could damage the hull.
An inflatable structure usually has a central core. The core is most often solid and runs the longitudinal length of the module. The core acts as a backbone to the structure and assists in, among other things, providing the shape to the structure and a framework for securing equipment.
To reduce the weight of the module, the core does not take the form of a solid hull. Rather, the core can be comprised of distal ends joined by a number of connecting elements such as longerons. In this form, the core is not designed to cooperate with a collapsed flexible hull. The core could have sharp edges or other protrusions that could damage the bladder of the hull.
At the launch stage, the bladder must be secured about the core in such a way as to minimize the opportunity for perforations, punctures, and tears in the bladder. One way to reduce the chance of damaging the bladder is to place a relatively smooth surface on the outside of the core so that the flexible hull could be folded around the surface without making contact with the core. The relatively smooth surface would be connected to the core and substantially surround the core to provide protection and support for the bladder. This surface could be part of a cover that is adapted to work with the core.
Another issue concerning the flexible hull is the use of windows. It is not unusual for a structure to have at least one window if not more integral to the flexible hull. As a flexible hull is usually comprised of a number of layers including, but not limited to, an orbital debris shield, a restraint layer, and a bladder, there must be an opening through each layer for viewing through the window. Furthermore, the window would be secured to at least one layer of the hull. When collapsing the hull for the launch configuration, care must be taken to insure that the window is properly indexed in relation to the rest of the hull (thereby minimizing the tension between the window and hull while collapsing the hull) and that the window does not break due to the forces exerted on the smooth surface of the cover.
This could be accomplished in a number of ways. The smooth surface of the cover can be partially flexible to bend to a degree rather than being rigid. Also, a buffer material such as rubber can be placed between the window and the smooth surface. As to properly indexing the window in relation to the rest of the hull, the smooth surface may have an access port, opening, or a hingable structure such as a door. The opening can be used to insure that the window is in the correct location and then the opening closed to provide a further degree of support.
One potential drawback to this approach arises due to the fact that the cover would restrict access from the core to the internal volume of the structure when the hull becomes inflated. Thus, whatever form the cover takes, it must be removable from the core to allow access to the full internal volume created by the hull when the module is deployed.
Another challenge lies in the characteristic of the internal surface of the flexible hull. While a rigid hull can function to secure equipment to the inside of a solid hull, the inside of the flexible hull is not so functional. Typically, the bladder forms the inside surface of an inflatable structure. The bladder does not have the structural qualities of a solid hull.
While the micro-gravity condition in space does not require the bladder to support the full weight of an item that may be attached to the surface of the bladder, nevertheless whatever comes into contact with the bladder might experience forces from other sources that could damage the bladder. One answer to this problem would be to secure a large panel to the inside surface of the bladder that conforms to the surface of the bladder and can support equipment without the equipment coming into contact with the bladder. The panel would serve to protect the bladder from contact with potentially damaging items and provide a foundation for securing items, such as equipment, in place.
Yet another challenge exists in the storage of materials and equipment at launch. While an inflatable module usually has a solid core, this does not mean that the core alone can function to store all the items needed in the structure. Furthermore, it may be necessary to distribute the weight at launch such that the core would not be an optimum place to contain storage items.
What is needed is a cover to provide a smooth surface for folding the bladder and flexible hull in the pre-deployed configuration. The cover would be substantially hollow for storing items prior to launch and during a mission. Further, the cover would be removable from the core after launch and during deployment. Finally, the surface of the cover would be contoured to conform to the inside surface of the bladder and securable to the bladder to protect the bladder and to act as a foundation for securing equipment, materials, or other items as needed.
This invention is directed to a cover for a modular structure. The inflatable modular structure has a core with at least two longerons and an inflatable shell and the inflatable shell has an internal surface that generally encloses both the longerons and a plurality of covers. The core has a plurality of attachment elements cooperating with the covers such that each cover is releasably attached to the core in the pre-deployed configuration. In that configuration the inflatable shell is folded over, and secured to, the covers such that the covers provide a measure of protection for the shell so that the shell does not come into contact with the core. In the deployed configuration the inflatable shell is pumped up with air and the covers are released from the core and removably attached to a plurality of affixing members disposed on the inside surface of the inflatable shell such that the covers serve as a foundation for securing items in place.
The cover has a first segment having a longitudinal axis, an interior surface, and having an arcuate exterior surface along the length of the longitudinal axis. The arcuate exterior surface of the first segment is adapted to provide support and protection for the folded inflatable shell during the pre-deployed configuration. The arcuate surface also has at least one affixing member for cooperating with an affixing member on the interior surface of the inflatable shell such that the arcuate exterior surface is removable attached to the interior surface of the inflatable shell during the deployed configuration.
There is also a second segment of the cover that has a substantially flat surface. The second segment is adapted to substantially secure items in place when the arcuate exterior surface is fastened to the interior surface of the inflatable shell in the deployed configuration.
Along with the first and second segments, the cover has a plurality of ribs disposed between, and joined to, the inner surface of the first segment and the substantially flat surface of the second segment. There are a number of attachment elements disposed on the ribs adapted to cooperate with the attachment elements on the core such that the cover is releasably attached to the core in the pre-deployed configuration.
a is an isometric view of the top of a cover;
b is an isometric view of a cover showing attachment elements;
c is an exploded view of corresponding attachment elements;
d is a partial isometric view of a cover on two longerons;
e is a partial isometric view of a cover attached to braces;
a is an isometric view of the core with covers;
a is a side view of a cover attached to the internal surface of an inflatable shell;
b is a side view of a cover attached to the internal surface of an inflatable shell;
c is an isometric view of a cover with items secured in place;
The present invention may best be understood by reference to the following description taken in conjunction with the accompanying drawings.
Turning to
The pin 120 can be released by an operator. This contemplates a pin that can be removed by mechanically by a crewmember or the use of an electromechanical device. The figure identifies attachment element 116 at one possible location on the longeron 118. However, attachment elements 114 and 116 can be oriented to cooperate on other locations on the longeron and the rib. The attachment elements 114 and 166 and the pin 120 are used in conjunction to allow the cover 110 to be releasably attached to the core in the pre-deployed configuration.
As shown in
Addressing
Turning to
Now addressing
In the preferred embodiment, the affixing members 136 and 138 are made of Velcro. However, other types of affixing members such as, but not limited to, magnetic strips could be used. In any case, the cover 100 is removably attached in this way to the internal surface 134.
Once the cover 100 is removably secured in place on the internal surface of the shell 134, the cover can be used to secure other items in place. This is exemplified in
Turning now to
Another purpose of the access openings is shown in
There has thus been described a novel cover for use with an inflatable modular structure. It is important to note that many configurations can be constructed from the ideas presented. The foregoing disclosure and description of the invention is illustrative and explanatory thereof and thus, nothing in the specification should be imported to limit the scope of the claims. Also, the scope of the invention is not intended to be limited to those embodiments described and includes equivalents thereto. It would be recognized by one skilled in the art the following claims would encompass a number of embodiments of the invention disclosed and claimed herein.
Number | Name | Date | Kind |
---|---|---|---|
1603182 | Aborn | Oct 1926 | A |
1958296 | Crow | May 1934 | A |
2131528 | Soyer | Sep 1938 | A |
2693195 | Frieder et al. | Nov 1954 | A |
3300910 | Isaac | Jan 1967 | A |
3364632 | Isaac | Jan 1968 | A |
3432609 | Brion, Jr. et al. | Mar 1969 | A |
3534750 | Kolozsvary | Oct 1970 | A |
3548904 | MacKell | Dec 1970 | A |
3984142 | Van Valkenburgh | Oct 1976 | A |
4224770 | Petty | Sep 1980 | A |
4375876 | Stewart | Mar 1983 | A |
4485991 | Fuller | Dec 1984 | A |
4531330 | Phillips | Jul 1985 | A |
4557144 | Lucchini | Dec 1985 | A |
4719935 | Gustafson | Jan 1988 | A |
4736762 | Wayman | Apr 1988 | A |
4939874 | Compton | Jul 1990 | A |
5313666 | Bax et al. | May 1994 | A |
5600927 | Kennon | Feb 1997 | A |
5682622 | Tagg | Nov 1997 | A |
5946871 | Kassardjian et al. | Sep 1999 | A |
6021614 | Krieger | Feb 2000 | A |
6115971 | Loebertmann et al. | Sep 2000 | A |
6231010 | Schneider et al. | May 2001 | B1 |
6250022 | Paz et al. | Jun 2001 | B1 |
6308474 | Wilson | Oct 2001 | B1 |
6367496 | Rempel et al. | Apr 2002 | B1 |
6439508 | Taylor | Aug 2002 | B1 |
6547189 | Raboin et al. | Apr 2003 | B1 |
6672744 | DeLine et al. | Jan 2004 | B2 |
6708451 | Gomes | Mar 2004 | B1 |
6860069 | Morris | Mar 2005 | B2 |
6892497 | Moon et al. | May 2005 | B2 |
D571021 | Gebka | Jun 2008 | S |
Number | Date | Country |
---|---|---|
6-136962 | May 1994 | JP |
WO 8402065 | Jun 1984 | WO |
Number | Date | Country | |
---|---|---|---|
20050091937 A1 | May 2005 | US |