Integrated spreader assembly
US-2024140607-A1 · May 2, 2024 · US
Aircraft seat mounting device
US2016340045A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016340045-A1 |
| Application number | US-201415104678-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 16, 2014 |
| Priority date | Dec 16, 2013 |
| Publication date | Nov 24, 2016 |
| Grant date | — |
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- Title
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- Abstract
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- Assignees and inventors
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- Key dates
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- First independent claim
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- CPC / IPC classifications
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- Citations and related patents
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Abstract
Official abstract text for this publication.
An aircraft seat mounting device with at least one carrier profile, with at least one aircraft seat element and with at least one intermediate element, which at least substantially encompasses the at least one carrier profile and is coupled to the at least one aircraft seat element. The intermediate element is arranged rotatably with respect to the carrier profile at least in case of crash/deformation.
First claim
Opening claim text (preview).
1 . An aircraft seat mounting device with at least one carrier profile, with at least one aircraft seat element and with at least one intermediate element, which at least substantially encompasses the at least one carrier profile and is coupled to the at least one aircraft seat element, wherein the intermediate element is arranged rotatably with respect to the carrier profile at least in case of crash/deformation. 2 . The aircraft seat mounting device according to claim 1 , comprising at least one further aircraft seat element, which is coupled to the intermediate element. 3 . The aircraft seat mounting device according claim 1 , wherein the aircraft seat element is embodied as a seat divider. 4 . The aircraft seat mounting device according to claim 1 , wherein the aircraft seat element is embodied as a seat leg. 5 . The aircraft seat mounting device according to claim 1 , wherein the intermediate element comprises at least one connection ram, via which the aircraft seat element is coupled to the intermediate element. 6 . The aircraft seat mounting device according to claim 5 , wherein the connection ram is coupled to the intermediate element via substance-to-substance bond. 7 . The aircraft seat mounting device according to claim 5 , wherein the connection ram has, in a connection region with the intermediate element, an extension in a circumferential direction which is less than 180 degrees. 8 . The aircraft seat mounting device according to claim 1 , wherein the at least one intermediate element is fixated with respect to the carrier profile at least in an axial direction. 9 . The aircraft seat mounting device according to claim 1 , wherein the intermediate element is arranged in a torque-proof fashion with respect to the carrier profile at least in one operating state. 10 . The aircraft seat mounting device according to claim 1 , wherein the intermediate element is fixedly connected to the carrier profile by means of an adhesive bond at least in one operating state. 11 . The aircraft seat mounting device according to claim 1 , wherein the carrier profile is at least substantially made of a light metal and/or of a fiber-composite material. 12 . The aircraft seat mounting device at least according to claim 1 , comprising at least one second intermediate element, wherein respectively only one aircraft seat element is coupled to one of the two intermediate elements. 13 . The aircraft seat mounting device at least according to claim 1 , comprising at least one further aircraft seat element, which is directly coupled to the carrier profile. 14 . An aircraft seat with an aircraft seat mounting device according to claim 1 . 15 . The aircraft seat mounting device according claim 2 , wherein the aircraft seat element is embodied as a seat divider. 16 . The aircraft seat mounting device according to claim 2 , wherein the aircraft seat element is embodied as a seat leg. 17 . The aircraft seat mounting device according to claim 2 , wherein the intermediate element comprises at least one connection ram, via which the aircraft seat element is coupled to the intermediate element. 18 . The aircraft seat mounting device according to claim 6 , wherein the connection ram has, in a connection region with the intermediate element, an extension in a circumferential direction which is less than 180 degrees. 19 . The aircraft seat mounting device according to claim 2 , wherein the at least one intermediate element is fixated with respect to the carrier profile at least in an axial direction. 20 . The aircraft seat mounting device according to claim 2 , wherein the intermediate element is arranged in a torque-proof fashion with respect to the carrier profile at least in one operating state.
Assignees
Inventors
Classifications
- B64D11/06Primary
Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title
with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title
Seats characterised by special features for reducing weight · CPC title
- B64D11/0696Primary
Means for fastening seats to floors, e.g. to floor rails · CPC title
Weight reduction · CPC title
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Frequently asked questions
Answers are generated from the same data shown on this page.
- What does patent US2016340045A1 cover?
- An aircraft seat mounting device with at least one carrier profile, with at least one aircraft seat element and with at least one intermediate element, which at least substantially encompasses the at least one carrier profile and is coupled to the at least one aircraft seat element. The intermediate element is arranged rotatably with respect to the carrier profile at least in case of cras…
- Who is the assignee on this patent?
- Recaro Aircraft Seating Gmbh & Co Kg
- What technology area does this patent fall under?
- Primary CPC classification B64D11/06. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Thu Nov 24 2016 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).