The disclosed embodiment is directed to parts of footwear including uppers, boot legs; stiffeners and other single parts of footwear, as well as heels and top pieces and sole and heel units. It is more particularly directed to an inner boot-binding system for people working in pressurized habitats such as a space station, submarine or Nuclear-Biological-Chemical (NBC) vehicle; workers who wear pressurized suits for lunar or planetary exploration or deep-sea diving; or those working in hazmat environments. Suits used in these environments contain a “life support backpack” which circulates fresh air within the pressurized suit.
Astronauts exposed to a microgravity environment, such as that in the pressurized International Space Station, secure themselves in place by sliding their feet under toe bars located throughout the habitat. Activity performed inside a pressurized environment or vehicle, for example, working on equipment or tending experiments, is called Internal Vehicle Activity (IVA). Activity performed outside a pressurized environment or vehicle is called External Vehicle Activity (EVA).
A “pressurized suit” is a protective garment that isolates a wearer from the outside environment such as the vacuum of space; highly pressurized salt water; or environments of hazardous gasses.
A pressurized suit boot-binding system secures a wearer to an inner boot during IVA, and to an outer or “surface” boot during EVA. During EVA, crew-members wear pressurized suits and pressurized outer boots. The boots have in the past used a Velcro strap on the exterior of the outer boot to secure them during lunar EVA. This type of clip was used during the Apollo lunar missions.
Some elements of pressurized suits impede movement and make activity difficult. During IVA, use of stabilizing toe bars have reportedly caused foot fatigue and injury. During EVA, walking, kneeling and completing tasks, as well as managing the considerable mass of the pressurized suit, is reportedly arduous and difficult and can cause foot fatigue and injury. Stability is further challenged because a life-support backpack shifts the wearer's center of gravity backward, resulting in counter-balancing movements. The stiffness and bulk of the suit make it difficult to counter the offset center of gravity. Further impediments to movement are caused by the suit's internal pressure, which is higher than ambient pressure.
Occupations requiring strenuous tasks while isolated from the environment include those of astronauts (referred to here as the crew or crew members), deep-sea divers, and workers wearing hazmat suits. Occupations requiring traverse across rugged, hot or cold surfaces requires a garment system that ties body garments to footwear and that can secure the foot to a thermal-isolating surface boot. A pressurized boot-binding system must allow easy doffing and donning of both pressurized suit and surface boot without snagging or tearing the pressure barrier in the pressurized suit.
Although special suits have been developed to isolate wearers from harsh environments, conventional pressurized suit boots are not adequately developed for traverse across rugged terrain in extreme temperature conditions. A safe temperature range for any continuous-contact surface ranges from 50° F. to 111° F. But surfaces on the earth's moon range from −185° F. to 210° F. Current systems involve thick, soft insulation material that resist heat transfer. The thick, soft material allows feet to slide about inside the boots, sometimes resulting in injury. A boot-binding system should firmly secure wearers' feet during IVA, and to a surface boot during EVA, while allowing the flexibility needed to work in thermally challenging conditions while wearing a pressurized suit.
A surface boot-binding system is configured to provide stability, flexibility and thermal isolation to individuals in occupations requiring isolation from harsh environments.
Adapted for use with a pressurized suit, the system assists in thermally isolating the wearer's feet from surface temperatures, and enables easy and predictable donning and doffing. Because the surface boot-binding system employs manually operable spring elements, it can be customized to accommodate various foot sizes and flexibility preferences.
A binding system mounts an inner boot to an IVA-binding plate, as well as to a surface boot during EVA. During IVA, the embodiment's binding system enables securing the wearer to receiver bindings variously located on habitat surfaces, separate from a wearer.
The system enables comfortable traverse along rugged terrain to one wearing a pressurized suit and carrying a life-support backpack during EVA. Flexible sole plates and embedded springs assist in thermally isolating the wearer from outer surface temperatures while providing comfort adjustment.
An inner boot is affixed to an inner sole plate which includes a toe-pin receptacle and a heel catch. An outer boot has a ring structure at its opening for connecting it to the leg of a pressurized suit. The outer boot is affixed to an outer-sole plate that includes a toe-pin mechanism and a heel-latch mechanism for attaching the outer boot to a leg of a pressurized suit.
A release cord is pulled to release the outer-sole plate heel-latch. A toe-pin mechanism may be oriented below the wearer's metatarsophalangeal joints to allow toes to flex.
The toe-pin mechanism may be affixed to a base structure and outer-sole plate. A toe pin and receptacle are seated against a pin spring-plate with an adjustment screw.
In some embodiments a heel mechanism joins an inner-sole plate heel catch to a latch in an outer-sole plate. The latch is held in a normally closed position with a spring or compressible material. Pulling a release cord actuates a linkage to move a shaft that releases the heel catch, releasing the inner sole from the outer-sole plate.
An inner-sole plate has toe-pin receptacles at its forward or toe end and a catch support on its back or heel end. The inner-sole plate structure is affixed to an inner-sole plate to provide rigidity. Similarly, an outer-sole plate structure is affixed to the outer-sole plate to provide rigidity. This outer-sole plate structure has toe-pin mechanisms at its forward (toe) end, and a heel mechanism at its back (heel) end. The outer sole plate includes a heel-latch mechanism housing and cover formed of flexible elastomeric material designed to protect the heel latch from dust and debris.
The outer sole-plate is adapted to alternatively affix to a surface so that a wearer may clip in to it, i.e., secure the inner boot to an externally positioned outer-sole plate.
The outer boot has a structural ring for attaching it to the leg of a pressurized suit.
A heel mechanism is connected to an outer-sole plate that is engaged with an outer boot. Boot and suit are connected by use of a connection ring.
An inner-sole plate is affixed to an inner boot. The inner-sole plate has a catch that mates with a latch in the heel mechanism, and at least one pin-and-hole alignment to the outer-sole plate. A compressible elastic material surrounds alignment pin(s).
The latch is released by moving a linkage which releases the catch from the latch. A secondary cover prevents unintended actuation of the linkage.
In another example embodiment the clip-in mechanism is positioned under the metatarsal joint to allow the foot to flex, easing walking and kneeling. This clip-in mechanism may be adjusted by manipulating a knob that controls spring tension.
Elastomeric padding between mechanisms provides vertical spring tension to secure the inner boot catch to the binding system latch and reduces wear on some of the system's moving parts and fatigue to the user. The padding is designed to also insulate the foot against exterior temperatures.
In some embodiments, the outer-sole plate has base structure at the toe and heel areas that translate force by wearer to the surface boot.
Springs in the integrated inner- and outer-sole plate system enable plates to move independently to offset unwanted movement resulting from manufacturing tolerance in the lateral and forward-and-aft directions between the sole plates. In order for the pins to fit into the bushings, the pin must have an outer-diameter clearance between 0.001″ to 0.050.″ This accounts for varying fit tolerances due to material and size changes occurring under ambient temperature changes: as pins expand or contract, pin/bushing compression springs and heel-plate compression springs move to accommodate changes in size, reducing clearance between parts.
Toe spring tension is manually adjustable and may be customized prior to EVA. A heavy person might tighten spring tension and a person of lighter weight might loosen it. Adjustments might also be made to offset varying gravitational constants.
One skilled in the art understands that pins may be machined to shapes other than cylindrical. A faceted shape minimizes twisting in its hole.
One skilled in the art understands that inner or outer sole plates may be made of non-conductive materials to protect a foot from environments of harsh temperatures, and specifically to prevent heat transfer between the pin of the outer boot and the receptacle of the inner boot. One skilled in the art understands that the inner and outer sole plates may be made of metallic or non-metallic materials to enhance foot flexibility.
In some embodiments involved motion and actuation forces are within accepted human anthropometric values.
In
In
In
In
Referring to
In some embodiments, the outer sole plate 218 may be fastened to a surface of a structure to allow a user to attach an inner boot and inner sole plate combination 210/212, and thus a foot or feet, to the outer sole plate 218 by inserting a toe under the toe bar 208 and fastening a catch 226 to a heel-latch mechanism 222. In this manner a user may remain in a substantially fixed position relative to the structure that the outer sole plate 218 is fastened to. This is particularly important when working in an unstable environment such as deep sea, micro gravity or zero gravity environments. In other embodiments, an outer sole plate 218 is part of an outer boot as illustrated in
Referring to
In all embodiments the strength required to compress and release included spring elements are within the strength values outlined in NASA/SP-2010-3407 titled HUMAN INTEGRATION DESIGN HANDBOOK for male and female crew ranging from 5th to 95th percentile, and may be easily modified if the percentile range increases.
An inner-sole plate 212 is engaged with an inner boot 210 and an outer-sole plate 218. A heel mechanism 222 is connected to an outer-sole plate 218 which is in turn connected to the upper of an outer boot 216 which includes a connection ring 222 which connects the outer boot to the let of a pressurized suit. The inner-sole plate 212 is affixed to an inner boot 210. One skilled in the art understands that an inner-sole plate may be manufactured as part of an inner boot 210 or may be affixed to an existing boot. The inner-sole plate includes a catch 226 for engaging with a latch 228 in the heel mechanism 222. The inner-sole plate further includes at least one alignment hole 252 proximal to the heel of the inner boot 210, for alignment with at least one alignment pin 250 in the outer-sole plate 218. A compressible elastic material 244 surrounds alignment pin(s) 250. Dashed lines 209 depict the alignment between alignment hole(s) 252 and alignment pin(s) 250. One skilled in the art understands that pins may be machined in various shapes including cylindrical, ovate or multi-sided to prevent twisting. In some embodiments a catch 226 is designed with a sufficiently low profile so as to minimize snagging on the interior surfaces of a pressurized suit.
The inner sole to outer sole combinations described above are applicable to any number of shoes or boots intended to secure a wearer to a platform or within a surface boot or shoe.
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Number | Date | Country | |
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62845353 | May 2019 | US |