Mounting system for seat frame structure

US2023173957A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2023173957-A1
Application numberUS-202117540958-A
CountryUS
Kind codeA1
Filing dateDec 2, 2021
Priority dateDec 2, 2021
Publication dateJun 8, 2023
Grant date

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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.

Described are aircraft seat frame assemblies comprising a tube and a seat frame component mounting system. The seat frame component mounting system comprises a first tube mounting member and a second tube mounting member separable from the first tube mounting member. The tube is positionable between the first tube mounting member and the second tube mounting member. The seat frame component mounting system further comprises a fastener extending at least partially through the second tube mounting member, the tube, and the first tube mounting member to couple the second tube mounting member to the first tube mounting member. A clamping force is substantially evenly applied from the second tube mounting member and the first tube mounting member against an outer circumferential surface of the tube via the fastener.

First claim

Opening claim text (preview).

That which is claimed is: 1 . A passenger seat comprising: a tube; and a seat frame component mounting system comprising: a first tube mounting member; a second tube mounting member separable from the first tube mounting member, wherein the tube is positionable between the first tube mounting member and the second tube mounting member; and a fastener extending at least partially through the second tube mounting member, the tube, and the first tube mounting member to couple the second tube mounting member to the first tube mounting member; and wherein a clamping force is substantially evenly applied from the second tube mounting member and the first tube mounting member against an outer circumferential surface of the tube via the fastener. 2 . The passenger seat of claim 1 , wherein the first tube mounting member is integrally formed with a seat frame component. 3 . The passenger seat of claim 1 , wherein an entirety of an inner surface of at least one of the first tube mounting member or the second tube mounting member is in contact with at least a portion of the outer circumferential surface of the tube. 4 . The passenger seat of claim 1 , wherein at least one of the first tube mounting member or the second tube mounting member comprises at least one guide member. 5 . The passenger seat of claim 4 , wherein the other of the at least one of the first tube mounting member or the second tube mounting member comprises at least one opening. 6 . The passenger seat of claim 5 , wherein the second tube mounting member is positionable relative to the first tube mounting member so that the at least one guide member substantially aligns with the at least one opening. 7 . The passenger seat of claim 6 , wherein at least one second fastener is coupleable to the first tube mounting member and extends at least partially through the at least one opening, the at least one guide member, and the first tube mounting member. 8 . The passenger seat of claim 6 , wherein there is at least one gap between the first tube mounting member and the second tube mounting member in an area of the first tube mounting member and the second tube mounting member comprising the at least one opening and the at least one guide member. 9 . A method for assembling a passenger seat comprising a tube and a seat frame component mounting system, the method comprising: positioning the tube between a first tube mounting member and a second tube mounting member, wherein the second tube mounting member is separable from the first tube mounting member; inserting a fastener at least partially through the second tube mounting member, the tube, and the first tube mounting member to couple the second tube mounting member to the first tube mounting member; and tightening the fastener to apply a clamping force from the second tube mounting member and the first tube mounting member substantially evenly against an outer circumferential surface of the tube. 10 . The method of claim 9 , wherein an entirety of an inner surface of at least one of the first tube mounting member or the second tube mounting member is in contact with at least a portion of the outer circumferential surface of the tube. 11 . The method of claim 9 , wherein at least one of the first tube mounting member or the second tube mounting member comprises at least one guide member and at least one opening. 12 . The method of claim 11 , further comprising aligning the first tube mounting member and the second tube mounting member by aligning the at least one guide member of the at least one of the first tube mounting member or the second tube mounting member with the at least one opening of at least one of the first tube mounting member or the second tube mounting member. 13 . The method of claim 12 , further comprising coupling at least one second fastener to the first tube mounting member, wherein the at least one second fastener extends at least partially through the at least one opening, the at least one guide member, and the first tube mounting member. 14 . The method of claim 12 , wherein there is at least one gap between the first tube mounting member and the second tube mounting member in an area of the first tube mounting member and the second tube mounting member comprising the at least one opening and the at least one guide member. 15 . A seat frame component mounting system comprising: a first tube mounting member; a second tube mounting member separable from the first tube mounting member and moveable relative to the first tube mounting member along a linear axis; and a fastener extending at least partially through the second tube mounting member and the first tube mounting member to couple the second tube mounting member to the first tube mounting member. 16 . The seat frame component mounting system of claim 15 , wherein the first tube mounting member is integrally formed with a seat frame component. 17 . The seat frame component mounting system of claim 15 , wherein the linear axis extends substantially along a central axis extending through the fastener. 18 . The seat frame component mounting system of claim 15 , wherein at least one of the first tube mounting member or the second tube mounting member comprises at least one guide member and at least one opening. 19 . The seat frame component mounting system of claim 18 , wherein the second tube mounting member is positionable relative to the first tube mounting member so that the at least one guide member substantially aligns with the at least one opening. 20 . The seat frame component mounting system of claim 19 , wherein there is at least one gap between the first tube mounting member and the second tube mounting member in an area of the first tube mounting member and the second tube mounting member comprising the at least one opening and the at least one guide member.

Assignees

Inventors

Classifications

  • with locking mechanisms · CPC title

  • B60N2/242Primary

    Bus seats · CPC title

  • of the whole seat · CPC title

  • Shackle is integral with or independently attached to proximate side of plate or other side · CPC title

  • Lower frame constructions · CPC title

Patent family

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Frequently asked questions

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What does patent US2023173957A1 cover?
Described are aircraft seat frame assemblies comprising a tube and a seat frame component mounting system. The seat frame component mounting system comprises a first tube mounting member and a second tube mounting member separable from the first tube mounting member. The tube is positionable between the first tube mounting member and the second tube mounting member. The seat frame component mou…
Who is the assignee on this patent?
Safran Seats Usa Llc
What technology area does this patent fall under?
Primary CPC classification B60N2/01516. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Jun 08 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 6 related publications on this page (citations in our corpus or others sharing the same primary CPC).