The present disclosure relates broadly to energy attenuating systems and devices, and more particularly for example, systems and devices for attenuating under-vehicle blast and aircraft slam-down impact forces. Such devices may include those integrated into seating systems for military aircraft, including but not limited to, fixed and rotary wing aircraft, and all ground vehicles, including tracked and wheeled vehicles of current or future designs, which function as crew and cargo transport and combat fighting vehicles. The technology field may further relate to energy attenuating systems in civilian transportation of all types, such as automobiles, trucks, buses, rail transport systems and commercial and civilian aircraft, ground vehicles for firefighters and other rescuer transport vehicles. Such energy attenuating systems or devices may help reduce impact loading resulting from crash, slam down, under-vehicle blast, and other events, on vehicle occupants, thereby improving survivability of, and mitigating injury to the vehicle occupants.
In the accompanying drawings:
The present invention is described more fully hereinafter with reference to the accompanying drawings and/or photographs, in which one or more exemplary embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be operative, enabling, and complete. Accordingly, the particular arrangements disclosed are meant to be illustrative only and not limiting as to the scope of the invention. Moreover, many embodiments, such as adaptations, variations, modifications, and equivalent arrangements, will be implicitly disclosed by the embodiments described herein and fall within the scope of the present invention.
Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation. Unless otherwise expressly defined herein, such terms are intended to be given their broad ordinary and customary meaning not inconsistent with that applicable in the relevant industry and without restriction to any specific embodiment hereinafter described. As used herein, the article “a” is intended to include one or more items. Where only one item is intended, the term “one”, “single”, or similar language is used. When used herein to join a list of items, the term “or” denotes at least one of the items, but does not exclude a plurality of items of the list.
For exemplary methods or processes of the invention, the sequence and/or arrangement of steps described herein are illustrative and not restrictive. Accordingly, it should be understood that, although steps of various processes or methods may be shown and described as being in a sequence or temporal arrangement, the steps of any such processes or methods are not limited to being carried out in any particular sequence or arrangement, absent an indication otherwise. Indeed, the steps in such processes or methods generally may be carried out in various different sequences and arrangements while still falling within the scope of the present invention.
Additionally, any references to advantages, benefits, unexpected results, or operability of the present invention are not intended as an affirmation that the invention has been previously reduced to practice or that any testing has been performed. Likewise, unless stated otherwise, use of verbs in the past tense (present perfect or preterit) is not intended to indicate or imply that the invention has been previously reduced to practice or that any testing has been performed.
Further, the term “vehicle” as used herein means any land, air, sea, or space vehicle, including for example cars, trucks, military land vehicles of all kinds, aircraft, helicopters, and any other mobile means for transporting personnel or cargo from one place to another.
Referring to
One exemplary embodiment of an energy attenuating mount system in accordance with the present disclosure is shown in
As shown in the side views of
The side mounted vehicle seat further incorporates a roller 28 on, or extending from the side of the seat base 10 facing the mount plate 15, and positioned substantially below the sliding attachments 20, 40. The roller 28 supports the seat base 10 in a horizontal orientation, and is configured to roll in a vertical direction against a vertical surface such as mount plate 15. The roller 28 may be comprised of one roller, or multiple spaced apart rolling elements. In the embodiment shown in
The roller 28 along with blocks 20, 40 may be permanently attached to, or integral with the side of seat base 10 as illustrated for example in
Alternatively, the blocks 20, 40, and roller 28 may be attached to, or form integral parts of a separate seat attachment bracket 29 such as shown in
Under normal conditions the seat base 10 is prevented from sliding downward relative to mounting plate 15 by an energy attenuating (EA) link 16 attached to the sliding mechanism 12 (or 32). The EA link is attached at one end to the slide block 20 (or mount block 40), and at the other end to the bottom of bracket 24 (or 44). The EA link may be any crushable element designed to absorb the energy imparted by the vehicle structure to the seat in a sudden impact event such as an under-vehicle mine blast. For example, the exemplary EA link 16 may be an elongated solid metal bar comprising straight sections and bends as depicted, or alternatively any bent, curved, or sinusoidal design. EA link 16 may also include at least two fastener points at each end to prevent rotation. Each seat mount system 1 may comprise one or more EA links 16 connected to respective sliding mechanisms 12, 32. An exemplary EA link is described in U.S. Pat. No. 7,938,485, assigned to the assignee of the present invention, the entire contents of which are hereby incorporated by reference.
In the event of a sudden impact (e.g., under-vehicle mine blast or slam-down), mount system 1 allows the seat carrying the occupant to independently stroke downward relative to the vehicle, and in an attenuated manner against the supporting force of the EA links 16. The guide rods 22, 42 control the bending direction of the EA links 16, and prevent twisting during vertical displacement.
The exemplary EA links 16 are designed to substantially absorb the impact energy, and may be custom tunable by modifying their material thickness, and/or shape. In one exemplary implementation, the present seat mount system may attenuate an impact of a 6.5 meters-per-second pulse, such as may result from an under-vehicle mine or IED explosion. The exemplary mount system 1 may also be capable of withstanding the following road shock loads transmitted through the vehicle chassis structure: 10 G's vertical, 8 G's longitudinal, and 5 G's transverse. In other exemplary embodiments, the seating assembly 10 may incorporate other or additional known energy attenuation links or devices. Although the EA links 16 may protect the occupant for multiple impact events, it is generally considered disposable and is easily replaced to restore a maximum level of protection to the mounting system 1.
Another exemplary side-mounted, energy attenuating seat system in accordance with the present invention is shown in
An upper portion of the seat base 10 is attached to a block 20 of the front sliding mechanism 12 and a block 40 of the rear sliding mechanism 32. A backing plate 67 may be incorporated to enhance stability of the assembly. Seat base 10 further incorporates a roller 28 on the side facing plate 15, located substantially below the point of attachment of the seat base 10 to the blocks 20, 40. A lower portion of mounting plate 15 may serve as a bearing surface for roller 28 to react the moment load imparted by seat inertia forces.
For the purposes of describing and defining the present invention it is noted that the use of relative terms, such as “substantially”, “generally”, “approximately”, and the like, are utilized herein to represent an inherent degree of uncertainty that may be attributed to any quantitative comparison, value, measurement, or other representation. These terms are also utilized herein to represent the degree by which a quantitative representation may vary from a stated reference without resulting in a change in the basic function of the subject matter at issue.
Exemplary embodiments of the present invention are described above. No element, act, or instruction used in this description should be construed as important, necessary, critical, or essential to the invention unless explicitly described as such. Although only a few of the exemplary embodiments have been described in detail herein, those skilled in the art will readily appreciate that many modifications are possible in these exemplary embodiments without materially departing from the novel teachings and advantages of this invention. For example, although the seat mount system of the present invention has been generally described and depicted in terms of a side-mounted arrangement, the same mount system is equally applicable and useful with any seat orientation. In particular, the seat mount system may be effectively positioned to support a vehicle seat from the back instead of from the side, or from any angular position in between. Accordingly, all such modifications are intended to be included within the scope of this invention as defined in the appended claims.
This document claims the benefit of the filing date of U.S. Provisional Patent Application 61/394,675, entitled “Cantilever Mounted Energy Attenuating Vehicle Seat” to Wilhelm, which was filed on Oct. 19, 2010, the contents of which are hereby entirely incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
3619006 | Barecki | Nov 1971 | A |
3968863 | Reilly | Jul 1976 | A |
3985388 | Hogan | Oct 1976 | A |
4349167 | Reilly | Sep 1982 | A |
4440441 | Marrujo et al. | Apr 1984 | A |
4474347 | Mazelsky | Oct 1984 | A |
4523730 | Martin | Jun 1985 | A |
4525010 | Trickey et al. | Jun 1985 | A |
5125598 | Fox | Jun 1992 | A |
5273240 | Sharon | Dec 1993 | A |
5676336 | Nefy et al. | Oct 1997 | A |
5788185 | Hooper | Aug 1998 | A |
5842669 | Ruff | Dec 1998 | A |
6257663 | Swierczewski | Jul 2001 | B1 |
6561580 | Bergey | May 2003 | B1 |
6585190 | Mort | Jul 2003 | B2 |
6692069 | Beroth et al. | Feb 2004 | B2 |
7445181 | Knoll et al. | Nov 2008 | B2 |
7513558 | Hansen | Apr 2009 | B2 |
7658425 | Paxton et al. | Feb 2010 | B2 |
7744155 | List et al. | Jun 2010 | B2 |
7758095 | Elhanany | Jul 2010 | B2 |
7938485 | Perciballi et al. | May 2011 | B1 |
8087723 | Honnorat et al. | Jan 2012 | B2 |
20090066126 | Stevens | Mar 2009 | A1 |
20090267391 | Honnorat et al. | Oct 2009 | A1 |
20110079681 | Honnorat | Apr 2011 | A1 |
Number | Date | Country | |
---|---|---|---|
61394675 | Oct 2010 | US |