Mounting systems for personal electronic devices and related methods

US9809311B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9809311-B2
Application numberUS-201514927919-A
CountryUS
Kind codeB2
Filing dateOct 30, 2015
Priority dateOct 30, 2015
Publication dateNov 7, 2017
Grant dateNov 7, 2017

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  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 mounting system may be installed in an aircraft, such as by installing a first plate and a second plate on either side of a sandwich panel wall in a personal space of an aircraft. The first plate and second plate may be coupled together, and a structural interface may receive a mounting accessory such that it is positioned adjacent the first plate. A personal electronic device may be mounted to the mounting accessory, thereby facilitating use of the personal electronic device on-board the aircraft. Such a mounting system may facilitate the use of personal electronic devices in lieu of costly in-flight entertainment systems. The first plate and second plate may be secured to a honeycomb core sandwich panel, such that fasteners may extend through inserts extending through the core, thereby distributing the weight of the personal electronic device and mounting accessory via the first plate and second plate.

First claim

Opening claim text (preview).

The invention claimed is: 1. A mounting system, comprising: a sandwich panel having a first surface, a second surface opposite the first surface, and a core extending between the first surface and the second surface; and a structural portion coupled to the sandwich panel, the structural portion comprising: a first plate having a first outer surface and a first inner surface opposite the first outer surface, the first plate being coupled to the first surface of the sandwich panel such that the first inner surface faces the first surface of the sandwich panel; and a second plate having a second outer surface and a second inner surface opposite the second outer surface, the second plate being coupled to the second surface of the sandwich panel such that the second inner surface faces the second surface of the sandwich panel, wherein the second plate is coupled with respect to the first plate such that a portion of the sandwich panel is positioned therebetween; and a structural interface configured to receive a mounting accessory for a personal electronic device such that the mounting accessory is positioned adjacent the first plate. 2. The mounting system according to claim 1 , wherein the structural portion further comprises: a plurality of floating nut plates; a plurality of fasteners substantially fixing the first plate with respect to the second plate, wherein at least a first respective fastener of the plurality of fasteners couples the first plate to the first surface, and wherein at least a second respective fastener of the plurality of fasteners engages a respective floating nut plate of the plurality of floating nut plates, thereby coupling the second plate to the second surface; and a plurality of through-inserts extending through the core of the sandwich panel, wherein each respective fastener of the plurality of fasteners extends through a respective through-insert of the plurality of through-inserts. 3. The mounting system according to claim 2 , wherein each floating nut plate of the plurality of floating nut plates is formed integrally with the second plate. 4. The mounting system according to claim 2 , wherein the each fastener of the plurality of fasteners is installed through the first plate, through a respective through-insert of the plurality of through-inserts, and into a respective floating nut plate of the plurality of floating nut plates. 5. The mounting system according to claim 1 , wherein the structural interface is configured to receive a plurality of different types of mounting accessories for a plurality of different types of personal electronic devices, wherein the structural interface is configured such that each of the plurality of different types of mounting accessories is selectively removable from the structural interface and selectively replaceable with a different respective mounting accessory of the plurality of different types of mounting accessories. 6. The mounting system according to claim 1 , further comprising the mounting accessory, wherein the mounting accessory is configured to maintain the personal electronic device in a position suitable for use by one or more of a passenger and a crew member. 7. The mounting system according to claim 1 , wherein the structural portion further comprises a charging interface, the charging interface being configured to charge the personal electronic device. 8. The mounting system according to claim 1 , wherein the sandwich panel comprises a honeycomb core sandwich panel, wherein the first surface of the sandwich panel is an interior wall of a personal space of an aircraft, and wherein the second surface of the sandwich panel is an exterior wall of the personal space of the aircraft. 9. The mounting system according to claim 1 , wherein the sandwich panel comprises a cut-out extending through at least a portion of the core, the cut-out being configured to receive a power component, the power component comprising one or more of a wire, a cable, a power supply, and a charger. 10. The mounting system according to claim 1 , wherein the sandwich panel forms a portion of one or more of a main cabin, a passenger service unit, a sidewall, a passenger seat, an aircraft closet, an aircraft galley, a rolling galley cart, a lavatory, a cockpit, and a crew rest. 11. The mounting system according to claim 1 , wherein the mounting system is configured to suspend the personal electronic device from the sandwich panel, thereby positioning the personal electronic device for use and securing it to the sandwich panel via the structural portion and the mounting accessory coupled thereto. 12. The mounting system according to claim 1 , wherein the structural interface comprises a plurality of structural interfaces, each structural interface being configured to receive a respective mounting accessory from a plurality of mounting accessories for a respective personal electronic device from a plurality of personal electronic devices, wherein the first plate comprises a plurality of first plates, each first plate being configured to receive a respective structural interface from the plurality of structural interfaces, wherein the second plate comprises a plurality of second plates, each second plate being configured to be coupled to a respective first plate of the plurality of first plates, such that the respective first plate and the respective second plate are positioned on either side of the sandwich panel, wherein the plurality of structural interfaces comprises a plurality of different types of structural interfaces, and wherein the plurality of first plates comprises a plurality of different types of first plates, the different types of first plates differing in at least one of size, shape, and type of structural interface. 13. The mounting system according to claim 12 , wherein each first plate of the plurality of first plates comprises at least one charging interface, the at least one charging interface being configured to charge the respective personal electronic device. 14. A kit for mounting a personal electronic device in an aircraft, the kit comprising: a first plate having a first outer surface and a first inner surface opposite the first outer surface, the first plate being configured to be coupled to a first surface of an interior monument within the aircraft such that the first inner surface faces the first surface of the interior monument, the first plate comprising a plurality of through-holes formed therethrough; a second plate having a second outer surface and a second inner surface opposite the second outer surface, the second plate being configured to be coupled to a second surface of the interior monument such that the second inner surface faces the second surface of the interior monument, wherein the second surface of the interior monument is opposite the first surface; a structural interface configured to receive a mounting accessory for a personal electronic device such that the mounting accessory is positioned adjacent the first plate; a plurality of through-inserts each being configured to receive a respective fastener therethrough; and a plurality of floating nut plates, each of the plurality of floating nut plates being configured to engage a respective fastener when the respective fastener is positioned such that it extends through a respective through-insert of the plurality of through-inserts; wherein the kit is configured to be installed in the aircraft such that the plurality of through-inserts are positioned such that they extend between the first surface of the interior monument and the second surface of the interior monument and such that a respective

Assignees

Inventors

Classifications

  • Allowing quick release of the apparatus · CPC title

  • Interior liners · CPC title

  • with ball-joint (ball-jointed hinges F16C11/06 {; adjustable mountings employing universal joints for lighting devices F21V21/26 - F21V21/30}) · CPC title

  • Arrangements for entertainment or communications, e.g. radio, television · CPC title

  • Other supports for positioning apparatus or articles (heads thereof F16M11/02 {; undercarriages thereof F16M11/20} ; adapted to be stuck in the ground A45F3/44 {; sockets or holders for poles or posts E04H12/22}); Means for steadying hand-held apparatus or articles {(supports for measuring instruments G01D11/30; supports for casings of remote control switching devices H01H9/025)} · CPC title

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What does patent US9809311B2 cover?
A mounting system may be installed in an aircraft, such as by installing a first plate and a second plate on either side of a sandwich panel wall in a personal space of an aircraft. The first plate and second plate may be coupled together, and a structural interface may receive a mounting accessory such that it is positioned adjacent the first plate. A personal electronic device may be mounted …
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64D11/0015. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Nov 07 2017 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).