This application relates to a fecal collection device for use in zero gravity, wherein compacted bags are retained at a compacted position.
As can be appreciated, space vehicles operate in zero or near zero gravity. The interior of such vehicles is limited and space is at a premium. For manned space vehicles, human waste must be accommodated.
Thus, it is known to provide compacting devices for fecal material. Generally, toilets for use is space environments are known which move fecal material into storage bags. The storage bags are then stored in a collection unit. A compactor compacts the bags to better utilize available space.
The compactors are provided with air holes that must remain unblocked. There is sometimes a challenge in zero or near zero environments that the bags may expand back and may even block the air holes.
A fecal canister for use in a space application has a canister body extending from an inlet end toward a remote end. Hooks are aligned along an inner surface of the canister from the inlet end towards the remote end. In embodiments, a compaction lid, or a storage bag catch on the hooks to maintain a compacted position.
These and other features may be best understood from the following drawings and specification.
The interior 28 of the canister 22 is angled such that at end 29, remote from entry end 31, there is a smaller cross-sectional area than at the interior at an entry end 31.
A plurality of straps 32, formed of the hook side of a hook and loop fastener material, extend between the entry end 31 and towards closed or remote end 29. While illustrated as extending the entire distance, the material need only extend over a portion of the distance.
The compaction lid 26 is shown to have a plurality of tabs 30 at an outer periphery. As the cross-sectional area of the interior 28 becomes smaller, with movement from end 31 towards end 29, the tabs 30 bend as shown in this figure and toward the entry end 31.
While the compactor 24 is being utilized to compact the bags 27, the tabs 30 will move past the hooks. However, once the compaction has stopped the hooks will retain the tabs 30 and, thus, the compaction lids 26, such that the bags 27 do not expand back toward the end 31.
As shown, air holes 34 allow airflow into an outer chamber 35. In this manner, the holes 34 are not blocked by expanding collection bags 27. The airflow provides several functions. It assists separation of the feces from the astronaut. Once separated, the airflow keeps the feces at the bottom of the collection bag away from the user. Once the collection bag is closed, the airflow carries the collection bag into the canister. This is why it is desirable that the airflow holes remain open and not covered by the collection bag.
Thus, the hooks on the strips 32 will capture the tabs 30 on the innermost lid 126. As shown at 34, the hooks will have a good area on the tabs 30 to grab. Tabs 30 on lid 226 are less bent. Still, as shown at 38, there will be sufficient “bite” to hold the tabs 30 on the intermediate compactor lid 226. The strips 32 should be positioned such that the hooks are generally facing the remote end.
Further, in embodiments, even the tabs 30 on the outermost lid 326 should be held adequately to resist expansion.
Bags 42 may be formed of a material that includes a non-woven material, such as a polyester. The bags 42 may have other material to provide loops to catch on the hooks.
The bag can be formed with a polytetrafluoroethylene (PTFE) coated interior to provide better storage. The non-woven outer side of the bag will snag on the hooks of the strips 32.
One hook and loop type material that may be utilized is available under the trademark Velcro® owned by Velcro Industries. However, other materials having an adequate hooking capability may also be utilized.
In one embodiment, both the lid structure of
Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this disclosure. For that reason, the following claims should be studied to determine the true scope and content of this disclosure.
This invention was made with government support under Contract No. NNH16C087C, awarded by NASA. The Government has certain rights in this invention.