Exemplary embodiments pertain to the art of space suits and, in particular, to modular armor for a hard upper torso of an atmospheric suit.
An atmospheric suit (e.g., space suit) includes several components that, together, provide a habitable environment (e.g., for an astronaut in deep space). The hard upper torso (HUT) forms a rigid enclosure about the upper body of the wearer and provides pressure containment for this part of the body. The HUT acts as a hub with structural attachment points for the arms, lower torso assembly (LTA), chest-mounted display and control modules, and primary life support subsystem (PLSS). The helmet attaches to an upper neck ring of the HUT. The HUT plays a load-bearing role by providing structural support to carry the PLSS, which is mounted to the back of the HUT, and the displays and control module (DCM), which is attached to the front of the HUT. The PLSS provides breathable oxygen, regulates pressure within the space suit, removes carbon dioxide and humidity, controls temperature, and may include communication equipment.
In one embodiment, modular armor for a hard upper torso (HUT) of an atmospheric suit that maintains a specific atmosphere within the suit includes a first outer layer including a first surface and a second surface opposite the first surface, and a second outer layer including a first surface and a second surface opposite the first surface. The armor also includes a core sandwiched between the first surface of the first outer layer and the first surface of the second outer layer. The armor is fabricated such that the second surface of the first outer layer is conformally affixed to the HUT.
Additionally or alternatively, in this or other embodiments, the armor also includes a first adhesive layer between the first surface of the first outer layer and the core and a second adhesive layer between the first surface of the second outer layer and the core. The first adhesive layer adheres the first outer layer to the core, and the second adhesive layer adheres the second outer layer to the core.
Additionally or alternatively, in this or other embodiments, the first outer layer and the second outer layer are composite laminate layers.
Additionally or alternatively, in this or other embodiments, the core includes titanium, aluminum, paper core, or rubber.
Additionally or alternatively, in this or other embodiments, the first outer layer, the second outer layer, and the core are fabricated via additive manufacturing as a single component.
Additionally or alternatively, in this or other embodiments, the single component is fabricated using a thermoplastic or metal.
Additionally or alternatively, in this or other embodiments, the second surface of the first outer layer is affixed to the HUT with hook and loop fasteners, snaps, fasteners, or pins.
Additionally or alternatively, in this or other embodiments, the core is formed as a repeating pattern of cells, each cell being a space with a shape defined by cell walls, and the cell walls of each of the cells being parallel with the first outer layer and the second outer layer or being perpendicular to the first outer layer and the second outer layer.
Additionally or alternatively, in this or other embodiments, one or more of the cells is filled with foam.
In another embodiment, a hard upper torso (HUT) of an atmospheric suit that maintains a specific atmosphere within the suit includes an upper neck ring configured as an attachment to a helmet, and modular armor. The modular armor includes a first outer layer including a first surface and a second surface opposite the first surface, and a second outer layer including a first surface and a second surface opposite the first surface. A core is sandwiched between the first surface of the first outer layer and the first surface of the second outer layer. The armor is fabricated such that the second surface of the first outer layer is conformally affixed to the HUT.
Additionally or alternatively, in this or other embodiments, the modular armor further comprises a first adhesive layer between the first surface of the first outer layer and the core and a second adhesive layer between the first surface of the second outer layer and the core. The first adhesive layer adheres the first outer layer to the core and the second adhesive layer adheres the second outer layer to the core.
Additionally or alternatively, in this or other embodiments, the first outer layer and the second outer layer are composite laminate layers and the core includes titanium, aluminum, paper core, or rubber.
Additionally or alternatively, in this or other embodiments, the first outer layer, the second outer layer, and the core are fabricated as a single component using additive manufacturing.
Additionally or alternatively, in this or other embodiments, the single component is fabricated using a thermoplastic or metal.
Additionally or alternatively, in this or other embodiments, the second surface of the first outer layer is affixed to the HUT with hook and loop fasteners, snaps, fasteners, or pins.
Additionally or alternatively, in this or other embodiments, the core is formed as a repeating pattern of cells, each cell being a space with a shape being defined by cell walls, and the cell walls of each of the cells being parallel with the first outer layer and the second outer layer or being perpendicular to the first outer layer and the second outer layer.
Additionally or alternatively, in this or other embodiments, one or more of the cells is filled with foam.
In yet another embodiment, a method of assembling a hard upper torso (HUT) of an atmospheric suit that maintains a specific atmosphere within the suit to include modular armor includes forming a first outer layer including a first surface and a second surface opposite the first surface and forming a second outer layer including a first surface and a second surface opposite the first surface. The method also includes forming a core sandwiched between the first surface of the first outer layer and the first surface of the second outer layer. The second surface of the first outer layer is conformally affixed to the HUT.
Additionally or alternatively, in this or other embodiments, the method also includes adhering the first outer layer to the core with a first adhesive layer and adhering the second outer layer to the core with a second adhesive layer.
Additionally or alternatively, in this or other embodiments, the forming the first outer layer, the forming the second outer layer, and the forming the core is as a single component based on additive manufacturing.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
As previously noted, a HUT is a part of an atmospheric suit, such as a space suit. The HUT maintains pressure within the suit and must also withstand impact, because a breach of the HUT can result in loss of pressure in the suit and may present a danger to the wearer. The HUT may include a rear entry door (RED) that facilitates donning and doffing he HUT from the back. The HUT must be thin enough and light enough (low mass) not to impede the mobility of the wearer of the suit. Thus, the HUT may be fabricated from fiberglass or another rigid material that is not bulky. However, this may make the HUT insufficient to withstand a fall or impact (e.g., of a micrometeoroid in deep space).
Embodiments detailed herein relate to modular armor for a HUT of an atmospheric suit. The modular armor may be attached to the HUT only where impact-absorption is deemed to be needed such that the effect on the overall mobility and weight of the HUT is minimized. While a space suit is discussed, in particular, for explanatory purposes, the HUT may also be part of another type of atmospheric suit (i.e., a suit that maintains a specific atmosphere within it). For example, in addition to being used in deep space (e.g., in an extravehicular mobility unit or space suit), the atmospheric suit including the HUT may be used in underwater (e.g., in an atmospheric diving suit), earth-based (e.g., in a hazmat suit or contamination suit), high-altitude (e.g., in a flight suit), and sub-surface applications.
According to an exemplary embodiment, the armor 110 is assembled from separate parts. In this case, an adhesive layer 320 on the second sides 317a, 317b (generally 317) of each of the outer layers 310a, 310b (generally 310) adheres the outer layers 310 to a core 115 that is sandwiched therebetween. The outer layers 310 may each be a composite laminate. The material of the outer layers 310 may be a fiberglass or carbon fiber that is pre-impregnated with a resin and cured. An initial curing may be performed for each of the outer layers 310 prior to stacking and curing other components of the armor 110. Alternately, all the components of the armor 110 may be cured together. The core 115 may be titanium, aluminum, paper core, or rubber, for example. Paper core refers to a pulped product that results from short fibers rolled with a resin into a sheet and then joined with other such sheets into a structure (e.g., honeycomb). According to alternate embodiments, the core 115 may be another metal or alloy.
According to an alternate embodiment, the armor 110 is additively manufactured. In this case, the first and second outer layers 310 and the core 115 are fabricated as a single component. A thermoplastic or metal may be used in the three-dimensional printing process that forms the armor 110 as a single component. The adhesive layer 320 is not needed according to this embodiment.
The shape of the armor 110 is not limited by any exemplary embodiment. As shown in
The armor 110 is not flexible. Further, a given module of the armor 110 must be conformally affixed to a given area of the HUT 120. Thus, based on the area of the HUT 120 to which the given module of armor 110 is to be affixed, not only the shape but also the profile shape of the armor 110 is designed and fabricated to match the profile shape of the area of the HUT 120. This is illustrated, for example, by the four modules of armor 110 in
That is, in any of the embodiments, based on where on the HUT 120 a particular module of armor 110 is to be affixed, the thickness of the armor 110 may be varied. Fabricating the armor 110 via additive manufacturing, in particular, facilitates adaptively generating armor 110 based on the location on the HUT 120 and the application. For example, if the additive manufacturing is facilitated in a deep space vehicle, armor 110 may be designed and added based on an upcoming extravehicular mission. Additionally, in any of the embodiments, cell walls 620 may be corrugated.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.