Aircraft seat mounting device
US-2016340045-A1 · Nov 24, 2016 · US
US10988259B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10988259-B2 |
| Application number | US-201716348892-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 13, 2017 |
| Priority date | Nov 10, 2016 |
| Publication date | Apr 27, 2021 |
| Grant date | Apr 27, 2021 |
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There is provided a seat base frame ( 10 ) comprising one or more base frame tubes ( 16 ) having noncircular cross-sections. In a specific example, the tubes ( 16 ) have elliptical cross-sections. Further embodiments provide base frame tubes ( 16 ) made of magnesium or magnesium alloys.
Opening claim text (preview).
What is claimed is: 1. A base frame for a seat, comprising: a rear base frame tube comprising an elliptical external shape; and a front base frame tube comprising an elliptical external shape; wherein each of the rear and front base frame tubes comprises a long axis and a short axis that collectively define the elliptical external shape of each of the rear base frame tube and the front base frame tube; wherein an axis intersecting a centroid of each of the rear base frame tube and the front base frame tube is horizontal; wherein the rear base frame tube is positioned such that the long axis of the rear base frame tube slopes forwardly and upwardly at substantially a 35-55 degree angle relative to the horizontal; wherein the front base frame tube is positioned such that the long axis of the front base frame tube slopes forwardly and downwardly at substantially a 10-30 degree angle relative to the horizontal. 2. The base frame of claim 1 , further comprising one or more seat spreaders and one or more seat legs cooperable with the rear and front base frame tubes. 3. The base frame of claim 2 , wherein the one or more seat spreaders comprise a rear opening and a forward opening, the rear opening sized and configured to receive the rear base frame tube and the forward opening sized and configured to receive the front base frame tube. 4. The base frame of claim 1 , wherein at least one of the rear base frame tube, the front base frame tube, or both comprise a first wall portion and a second wall portion, wherein wall thicknesses differ between the first wall portion and the second wall portion. 5. The base frame of claim 1 , wherein at least one of the rear base frame tube, the front base frame tube, or both comprise magnesium or a magnesium alloy. 6. The base frame of claim 1 , wherein the seat comprises an aircraft seat. 7. An aircraft seat, comprising a base frame; one or more seat spreaders; one or more seat legs; and one or more base frame tubes each comprising an elliptical external shape, wherein the one or more base frame tubes comprise a rear ellipse tube and a front ellipse tube, wherein each of the rear and front ellipse tubes comprises a long axis and a short axis that collectively define the elliptical external shape of each of the rear ellipse tube and the front ellipse tube; wherein an axis intersecting a centroid of each of the rear ellipse tube and the front ellipse tube is horizontal; wherein the rear ellipse tube is positioned in the base frame such that the long axis of the rear ellipse tube slopes forwardly and upwardly at substantially a 35-55 degree angle relative to the horizontal; wherein the front ellipse tube is positioned in the base frame such that the long axis of the front ellipse tube slopes forwardly and downwardly at substantially a 10-30 degree angle relative to the horizontal. 8. The aircraft seat claim 7 , wherein at least one of the rear ellipse tube, the front ellipse tube, or both comprise a first wall portion and a second wall portion, wherein wall thicknesses differ between the first wall portion and the second wall portion. 9. The aircraft seat claim 7 , wherein at least one of the rear ellipse tube, the front ellipse tube, or both comprise magnesium or a magnesium alloy.
Weight reduction · CPC title
with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash · CPC title
Width modification of seat assemblies, e.g. for class modification · CPC title
Seats characterised by special features for reducing weight · CPC title
Lower frame constructions · CPC title
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