Using foam for structural components of a seat assembly
11530044 · 2022-12-20
Assignee
Inventors
- Jason K. Smith (Denton, TX, US)
- Raul G. Reyes (Denton, TX, US)
- Andrew B. Severance (Fort Worth, TX, US)
Cpc classification
B64D11/0643
PERFORMING OPERATIONS; TRANSPORTING
B64D11/0649
PERFORMING OPERATIONS; TRANSPORTING
B64D11/0619
PERFORMING OPERATIONS; TRANSPORTING
Y02T50/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64D11/0647
PERFORMING OPERATIONS; TRANSPORTING
B60N2/995
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64D11/06
PERFORMING OPERATIONS; TRANSPORTING
B60N2/70
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Seat assemblies (200) including structural components (212, 222, 232) made of foam are described. A seat sub-assembly (210, 220, 230) can include a frame (214, 224, 234) and a foam support (212, 222, 232). The foam support (212, 222, 232) can be coupled to the frame (214, 224, 234) for receiving a load on the seat sub-assembly (210, 220, 230), dissipating at least half of the load, and dispersing the load through the frame (214, 224, 234).
Claims
1. A seat assembly comprising: a seat pan comprising: a bottom frame; and a bottom support coupled to the bottom frame for bearing at least half of a first load on the seat assembly and dispersing a portion of the first load across the bottom support to the bottom frame; a seat back coupled to the seat pan, the seat back comprising: a back frame; and a back support coupled to the back frame for bearing at least half of a second load on the seat assembly and for dispersing a portion of the second load across the back support to the back frame; and a leg rest coupled to the seat pan, the leg rest comprising: a leg frame; and a leg support coupled to the leg frame for bearing at least half of a third load on the seat assembly and for dispersing a portion of the third load across the leg support to the leg frame, and wherein the bottom support, the back support, and the leg support each include a load-bearing foam for receiving a corresponding load, dissipating at least half of the load, and dispersing a portion of the load through the corresponding frame, wherein the back frame defines a back-receiving area, wherein the foam of the back support is positioned within the back-receiving area, wherein the foam of the back support is larger than the back-receiving area, and wherein the back frame is positioned in a groove in the foam of the back support, wherein the leg frame defines a leg-rest area, wherein the foam of the leg support is positioned within the leg-rest area, wherein the foam of the leg support is larger than the leg-rest area, and wherein the leg frame is positioned in a groove in the foam of the leg support, and wherein the bottom frame comprises four frame segments defines a sitting area, wherein the foam of the bottom support is positioned within the sitting area, wherein the foam of the bottom support is larger than the sitting area, and wherein each of the four frame segments of the bottom frame are encompassed by the foam of the bottom support.
2. The seat assembly of claim 1, wherein the seat assembly is a passenger seat on a passenger aircraft, wherein the first load, the second load, and the third load include a weight of a passenger sitting in the passenger seat.
3. The seat assembly of claim 1, wherein the load-bearing foam comprises: a foam structural layer for dissipating the first load, the second load, or the third load; a foam comfort layer coupled to the foam structural layer for providing a cushion; and a covering for encompassing the foam structural layer and the foam comfort layer to protect the foam structural layer and the foam comfort layer.
4. The seat assembly of claim 3, wherein the foam structural layer includes a reinforcing grid having a series of ridges and gaps such that the foam structural layer provides greater support to an area of the seat assembly closer to the ridges than the gaps.
5. The seat assembly of claim 3, wherein the foam structural layer can include at least one of neopor, polyolefin, ethylene-vinyl acetate (“EVA”), polyethylene, polyform, polyurethane, or ethafoam.
6. The seat assembly of claim 1, wherein the load-bearing foam is a structural foam that is molded, machined, formed, or constructed to act as a load-bearing part of the seat assembly.
7. The seat assembly of claim 1, wherein foam is usable as a replacement for metal load-bearing components that support cushions.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(14) The subject matter of embodiments of the present invention is described here with specificity to meet statutory requirements, but this description is not necessarily intended to limit the scope of the claims. The claimed subject matter may be embodied in other ways, may include different elements or steps, and may be used in conjunction with other existing or future technologies. This description should not be interpreted as implying any particular order or arrangement among or between various steps or elements except when the order of individual steps or arrangement of elements is explicitly described.
(15) In some embodiments, foam can be used for structural components of a seat assembly in an aircraft, but is by no means limited to aircraft seat assemblies. A seat assembly can include any passenger seat and the foam can be used for structural components in any seat assembly or any other seat of any type or otherwise as desired. For example, embodiments may be used on trains, busses, in movie theaters, student seating, desk chairs, couches or any instance where reducing a weight of a seat assembly or combining a structural layer and comfort layer be useful.
(16) According to certain embodiments of the present disclosure, as shown in
(17) The foam bottom 212, foam back 222, and foam body 232 can be made of any suitable structural foam including, but not limited to, neopor, polyolefin, ethylene-vinyl acetate (“EVA”), polyethylene, polyform, polyurethane, and ethafoam.
(18) The foam bottom 212, the foam back 222, and the foam body 232 can replace both metallic load-bearing supports and their associated cushions to reduce a total weight of seat assembly 200. The bottom frame 214, the back frame 224, and the leg frame 234 can be made of any suitable material including, but not limited to, metals (e.g., aluminum and titanium), plastics (e.g., polypropylene), or a composite material.
(19) As illustrated in
(20) The foam bottom 212, the foam back 222, or the foam body 232 can include a reinforcing structure 240 for providing more focused support. In some examples, the reinforcing structure 240 can include a series of ridges and gaps that can provide greater support for areas that are closer to the ridges than the gaps. Providing greater support for specific areas can include reducing the amount the specific areas yields under a load as compared to other areas. The gaps can reduce the weight of the seat assembly 200, while the ridges can provide the requisite support. In some examples, the foam back 222 can include the reinforcing structure 240, which provides additional support for an area associated with the lumbar region of a passenger seated in the seat assembly 200. In additional or alternative examples, the reinforcing structure 240 can be based on a typical weight distribution model for a user.
(21) As depicted in
(22) As depicted in
(23) Although only the foam bottom 212 is depicted as having a comfort layer 218a and a structural layer 218b, the foam back 222 and foam body 232 can have multiple layers as well. Both the comfort layer 218a and structural layer 218b can be generated using injection molding, machining, forming, or constructing. In some examples, both the comfort layer 218a and the structural layer 218b can be combined into a single foam component.
(24) Constructing the seat bottom 210, the seat back 220, or the leg rest 230 can include assembling a frame 214, 224, 234. Constructing can further include generating a foam support 212, 222, 232 capable of supporting a load exerted on the foam support 212, 222, 232. Constructing can also include coupling the foam support 212, 222, 232 to the frame 214, 224, 234 to allow the foam support 212, 222, 232 to dissipate a portion of the load and disperse another portion of the load through the frame 214, 224, 234. In some examples, at least 50-60% of the load can be dissipated by the foam support 212, 222, 232. In some aspects, the foam bottom 212, foam back 222, and foam body 232 can replace existing metal or composite load-bearing components (e.g., bottom support 112, back support 122, or leg support 132) as well as separate cushions that can be positioned on top of the load-bearing components. For example, the foam back 222 can replace a back support 122 (e.g., a composite diaphragm) and an associated back cushion (not illustrated) in an existing seat, such as the seat assembly 100 shown in
(25) In the following, further examples are described to facilitate the understanding of the invention:
(26) Example #1: A seat sub-assembly comprising: a frame; and a foam support coupleable to the frame for receiving a load on the seat sub-assembly, dissipating at least half of the load, and dispersing a portion of the load through the frame.
(27) Example #2: The seat-sub assembly of any of the preceding or subsequent examples, wherein the seat sub-assembly is a seat back for a seat assembly on a passenger aircraft, wherein the frame includes a first segment and a second segment for extending from a seat bottom of the seat assembly, and a third segment for coupling the first segment and the second segment for defining a back-receiving area, wherein the foam support is positionable within the back-receiving area for supporting a back of a passenger sitting in the seat assembly, and wherein the load includes a weight of the passenger sitting in the seat assembly.
(28) Example #3: The seat-sub assembly of any of the preceding or subsequent examples, wherein the seat sub-assembly is a seat bottom for a seat assembly on a passenger aircraft, wherein the frame includes four segments positioned to define a sitting area, wherein the foam support is positionable within the sitting area for supporting a passenger sitting in the seat assembly, and wherein the load includes a weight of the passenger sitting in the seat assembly.
(29) Example #4: The seat-sub assembly of any of the preceding or subsequent examples, wherein the seat sub-assembly is a leg rest for a seat assembly on a passenger aircraft, wherein the frame includes four segments positioned to define a leg-rest area, wherein the foam support is positionable within the leg-rest area for supporting legs of a passenger sitting in the seat assembly, and wherein the load includes a weight of the passenger sitting in the seat assembly.
(30) Example #5: The seat-sub assembly of any of the preceding or subsequent examples, wherein the foam support comprises: a foam structural layer for dissipating the load; a foam comfort layer coupled to the foam structural layer for providing a cushion; and a covering for encompassing the foam structural layer and the foam comfort layer to provide protection to the foam structural layer and the foam comfort layer.
(31) Example #6: The seat-sub assembly of any of the preceding or subsequent examples, wherein the frame is encompassed by the foam structural layer.
(32) Example #7: The seat-sub assembly of any of the preceding or subsequent examples, wherein the foam structural layer includes a reinforcing grid having a series of ridges and gaps such that the foam structural layer provides greater support to an area of the seat sub-assembly closer to the ridges than the gaps.
(33) Example #8: The seat-sub assembly of any of the preceding or subsequent examples, wherein the foam structural layer can include at least one of neopor, polyolefin, ethylene-vinyl acetate (“EVA”), polyethylene, polyform, polyurethane, or ethafoam.
(34) Example #9: The seat-sub assembly of any of the preceding or subsequent examples, wherein the foam support is a structural foam that is molded, machined, formed, or otherwise constructed to act as a load-bearing part of the seat sub-assembly.
(35) Example #10: The seat-sub assembly of any of the preceding or subsequent examples, wherein foam is usable as a replacement for metal load-bearing components that support cushions.
(36) Example #11: A seat assembly comprising: a seat pan comprising: a bottom frame; and a bottom support coupled to the bottom frame for bearing at least half of a first load on the seat assembly and dispersing a portion of the first load across the bottom support to the bottom frame; a seat back coupled to the seat pan, the seat back comprising: a back frame; and a back support coupled to the back frame for bearing at least half of a second load on the seat assembly and for dispersing a portion of the second load across the back support to the back frame; and a leg rest coupled to the seat pan, the seat pan comprising: a leg frame; and a leg support coupled to the leg frame for bearing at least half of a third load on the seat assembly and for dispersing a portion of the third load across the leg support to the leg frame, and wherein at least one of the bottom support, the back support, or the leg support includes a load-bearing foam.
(37) Example #12: The seat assembly of any of the preceding or subsequent examples, wherein the seat assembly is a passenger seat on a passenger aircraft, wherein the first load, the second load, and the third load include a weight of a passenger sitting in the passenger seat.
(38) Example #13: The seat assembly of any of the preceding or subsequent examples, wherein the load-bearing foam comprises: a foam structural layer for dissipating the first load, the second load, or the third load; a foam comfort layer coupled to the foam structural layer for providing a cushion; and a covering for encompassing the foam structural layer and the foam comfort layer to protect the foam structural layer and the foam comfort layer.
(39) Example #14: The seat assembly of any of the preceding or subsequent examples, wherein at least one of the bottom frame, the back frame, or the leg frame is encompassed by the foam structural layer.
(40) Example #15: The seat assembly of any of the preceding or subsequent examples, wherein the foam structural layer includes a reinforcing grid having a series of ridges and gaps such that the foam structural layer provides greater support to an area of the seat assembly closer to the ridges than the gaps.
(41) Example #16: The seat assembly of any of the preceding or subsequent examples, wherein the foam structural layer can include at least one of neopor, polyolefin, ethylene-vinyl acetate (“EVA”), polyethylene, polyform, polyurethane, or ethafoam.
(42) Example #17: The seat assembly of any of the preceding or subsequent examples, wherein the load-bearing foam is a structural foam that is molded, machined, formed, or constructed to act as a load-bearing part of the seat assembly.
(43) Example #18: The seat assembly of any of the preceding or subsequent examples, wherein foam is usable as a replacement for metal load-bearing components that support cushions.
(44) Example #19: A method comprising: assembling a frame for a component of a seat assembly; generating a foam support capable of supporting at least half of a load exertable on the component; and coupling the foam support to the frame to allow the foam support to disperse a portion of the load through the frame.
(45) Example #20: The method of any of the preceding or subsequent examples, wherein the seat assembly is a passenger seat on a passenger aircraft, wherein generating the foam support comprises at least one of molding, machining, forming, or constructing a structural foam that includes a foam structural layer to act as a load-bearing part of the passenger seat and a foam comfort layer for providing a cushion to a passenger seated in the seat assembly.
(46) Different arrangements of the components depicted in the drawings or described above, as well as components and steps not shown or described are possible. Similarly, some features and sub-combinations are useful and may be employed without reference to other features and sub-combinations. Embodiments of the invention have been described for illustrative and not restrictive purposes, and alternative embodiments will become apparent to readers of this patent. Accordingly, the present invention is not limited to the embodiments described above or depicted in the drawings, and various embodiments and modifications may be made without departing from the scope of the claims below.