This disclosure relates to a suit for use in extra vehicular activities (EVA) such as lunar or Martian landscape exploration.
EVA pressure suits have been proposed in which the subject enters from the rear of a hard upper torso (HUT). The HUT provides the visor and includes shoulder apertures and an entry opening, typically in the rear of the HUT to permit entry into the suit by the subject from an interior of a vehicle. Any primary and secondary life support systems are typically located behind the rear entry opening and pressure suit. Pressure suits should provide ease of entry by the subject as well as good mobility.
A suit includes a hard upper torso having an entry opening and shoulder apertures. The hard upper torso extends along a subject axis configured to coincide with an axis of a subject having donned the suit. The entry opening lies in a plane at an angle 7°+/−5° relative to the subject axis. The hard upper torso also includes non-circular shoulder apertures in one embodiment. In one example, the hard upper torso includes a waist bearing lying is at an angle of 63°+/−5° relative to the entry opening plane.
The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
The protrusions 26A, 26B may be volumes inside the HUT 14 or protective covers for volumes outside the pressure volume. The protrusion volumes can be shaped to utilize the maximum HUT width while avoiding impingement on arm movement. Placement of primary life support system elements in the HUT protrusions 26A, 26B reduces the PLSS mass and volume behind the subject 12 during EVA. This redistribution moves the PLSS mass closer to the subject's center of gravity for improved mass control during subject movement while providing a more front-to-back compact suit system envelope. The protrusions 26A, 26B may also provide a mounting area 29 to which lights or other devices may be attached external to the HUT 14.
The visor 16 may include spaced apart layers or shells. Shoulder apertures 22 are provided in the shell 23 at a fixed spacing relative to one another. The suit 10 has a HUT 14 providing arms arranged at the shoulder apertures 22.
The HUT 14 is shown in more detail in
The waist bearing 18A is at an angle 36 relative to the plane 32 of 63°+/−5°. The rearmost portion HUT bottom flange 48 is in close proximity to the habitat mating surface of the rear HUT flange 30. The waist bearing 18 is configured such that the front of the waist bearing 18 is positioned at sternum-height on the subject 12 once donned (
The HUT rear flange 30 extends vertically above the outside of the visor 16. The top of the entry opening 28 has a wall 31 that extends from the flange 30, in a direction that is approximately perpendicular to the subject axis 34, such that the top of the entry opening 28 is about level with the inside of the visor 16. The positioning of the entry opening 28 relative to the visor 16 in this manner enables the subject easy entry into the suit 10 while avoiding the need to reposition the HUT 14 upward or downward significantly subsequent to donning the suit in order to locate the subject's head within the visor 16.
The HUT 14 shell 23 may be of hybrid (two or more different fiber systems) composite construction. The shoulder apertures 22 may be non-circular, and in the example, elliptical. The shoulder apertures 22 may be other shapes. The shoulder apertures 22 lie in planes that are canted forward and inward (at the top) relative to one another, as best shown in
Referring to
View A-A illustrated in
The elliptical shape and orientation of the shoulder apertures 22 in the shell 23 better facilitate insertion of the subject's arms into the HUT 14 during donning of the suit 10.
Although an example embodiment has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.
This application claims priority to U.S. Provisional Application No. 61/474,443, which was filed on Apr. 12, 2011.
Number | Date | Country | |
---|---|---|---|
61474443 | Apr 2011 | US |