Floor grid for aircraft

US11203407B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11203407-B2
Application numberUS-202016732384-A
CountryUS
Kind codeB2
Filing dateJan 2, 2020
Priority dateJan 2, 2020
Publication dateDec 21, 2021
Grant dateDec 21, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A floor grid includes an outboard member, a first seat track and a second seat track, a first member extending from the outboard member to the first seat track, a second member extending from the first seat track to the second seat track, a first stanchion extending from the outboard member to the first seat track, a second stanchion extending from the outboard member to the second seat track, a third seat track and a fourth seat track, an intercostal extending from the second seat track to the fourth seat track, a third member extending from the outboard member to the third seat track, a fourth member extending from the third seat track to the fourth seat track, a third stanchion extending from the outboard member to the third seat track, and a fourth stanchion extending from the outboard member to the fourth seat track.

First claim

Opening claim text (preview).

What is claimed is: 1. A floor grid for an aircraft, the floor grid comprising: an outboard member; a first seat track and a second seat track, wherein the first seat track is outboard of the second seat track and substantially parallel to the second seat track; a first shear beam comprising: a first member extending from the outboard member to the first seat track; and a second member extending from the first seat track to the second seat track; a first stanchion extending from the outboard member to the first seat track; a second stanchion extending from the outboard member to the second seat track; a third seat track and a fourth seat track, wherein the third seat track is outboard of the fourth seat track and substantially parallel to the fourth seat track; an intercostal extending from the second seat track to the fourth seat track, wherein the outboard member is forward of the intercostal; a second shear beam comprising: a third member extending from the outboard member to the third seat track; and a fourth member extending from the third seat track to the fourth seat track; a third stanchion extending from the outboard member to the third seat track; and a fourth stanchion extending from the outboard member to the fourth seat track. 2. The floor grid of claim 1 , wherein the outboard member has a substantially circular shape and is positioned radially outward with respect to the first seat track, the third seat track, the first shear beam, the first stanchion, the second stanchion, the intercostal, the second shear beam, the third stanchion, and the fourth stanchion. 3. The floor grid of claim 1 , wherein the intercostal is substantially parallel with the outboard member. 4. The floor grid of claim 1 , wherein the outboard member is a first outboard member, the floor grid further comprising a second outboard member that is aft of the first outboard member, wherein the first shear beam intersects the second seat track at a joint, and wherein a first longitudinal distance between the first outboard member and the joint is 40 to 60 percent of a second longitudinal distance between the first outboard member and the second outboard member. 5. The floor grid of claim 1 , wherein the first stanchion meets the first seat track at a joint that is forward of the intercostal. 6. The floor grid of claim 1 , wherein the third stanchion meets the third seat track at a joint that is forward of the intercostal. 7. The floor grid of claim 1 , wherein the first seat track, the second seat track, the third seat track, the fourth seat track, the first shear beam, the second shear beam, and the intercostal are substantially coplanar and define a floor plane. 8. The floor grid of claim 7 , wherein the first seat track or the second seat track has an I-beam structure. 9. The floor grid of claim 1 , wherein the first shear beam intersects the first seat track at a first joint and intersects the second seat track at a second joint, wherein the first joint is forward of the second joint. 10. The floor grid of claim 9 , wherein the second shear beam intersects the third seat track at a third joint and intersects the fourth seat track at a fourth joint, wherein the third joint is forward of the fourth joint. 11. The floor grid of claim 1 , wherein the second stanchion intersects the intercostal and the first shear beam. 12. The floor grid of claim 11 , wherein the fourth stanchion intersects the intercostal and the second shear beam. 13. The floor grid of claim 1 , wherein the first stanchion and the second stanchion each extend between the outboard member and the first shear beam. 14. The floor grid of claim 13 , wherein the third stanchion and the fourth stanchion each extend between the outboard member and the second shear beam. 15. The floor grid of claim 1 , wherein the first stanchion and the second stanchion intersect at a joint on the outboard member. 16. The floor grid of claim 15 , wherein the joint is below the first shear beam. 17. The floor grid of claim 15 , wherein the third stanchion and the fourth stanchion intersect at a second joint on the outboard member. 18. The floor grid of claim 17 , wherein the second joint is below the second shear beam. 19. A floor grid for an aircraft, the floor grid comprising: an outboard member; a first seat track and a second seat track, wherein the first seat track is outboard of the second seat track and substantially parallel to the second seat track; a first shear beam comprising: a first member extending from the outboard member to the first seat track; and a second member extending from the first seat track to the second seat track, wherein the first shear beam intersects the first seat track at a first joint and intersects the second seat track at a second joint, wherein the first joint is forward of the second joint; a first stanchion extending from the outboard member to the first seat track; a second stanchion extending from the outboard member to the second seat track, wherein the first stanchion and the second stanchion intersect at the outboard member; a third seat track and a fourth seat track, wherein the third seat track is outboard of the fourth seat track and substantially parallel to the fourth seat track; an intercostal extending from the second seat track to the fourth seat track; a second shear beam comprising: a third member extending from the outboard member to the third seat track; and a fourth member extending from the third seat track to the fourth seat track; a third stanchion extending from the outboard member to the third seat track; and a fourth stanchion extending from the outboard member to the fourth seat track. 20. A floor grid for an aircraft, the floor grid comprising: an outboard member; a first seat track and a second seat track, wherein the first seat track is outboard of the second seat track; a first shear beam comprising: a first member extending from the outboard member to the first seat track; and a second member extending from the first seat track to the second seat track; a first stanchion extending from the outboard member to the first seat track; a second stanchion extending from the outboard member to the second seat track; a third seat track and a fourth seat track, wherein the third seat track is outboard of the fourth seat track; an intercostal extending from the second seat track to the fourth seat track, wherein the outboard member is forward of the intercostal, and wherein the first stanchion meets the first seat track at a first joint that is forward of the intercostal; a second shear beam comprising: a third member extending from the outboard member to the third seat track; and a fourth member extending from the third seat track to the fourth seat track; a third stanchion extending from the outboard member to the third seat track, wherein the third stanchion meets the third seat track at a second joint that is forward of the intercostal; and a fourth stanchion extending from the outboard member to the fourth seat track.

Assignees

Inventors

Classifications

  • Frames · CPC title

  • specially adapted for freight · CPC title

  • B64C1/18Primary

    Floors · CPC title

  • Means for fastening seats to floors, e.g. to floor rails · CPC title

  • Modular or preassembled units for creating cabin interior structures · CPC title

Patent family

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Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11203407B2 cover?
A floor grid includes an outboard member, a first seat track and a second seat track, a first member extending from the outboard member to the first seat track, a second member extending from the first seat track to the second seat track, a first stanchion extending from the outboard member to the first seat track, a second stanchion extending from the outboard member to the second seat track, …
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64C1/18. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 21 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).