Seat release system

US2020062144A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2020062144-A1
Application numberUS-201716348366-A
CountryUS
Kind codeA1
Filing dateOct 25, 2017
Priority dateNov 8, 2016
Publication dateFeb 27, 2020
Grant date

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  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

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

The following invention relates to occupant recovery from an armoured land vehicle, and to a system for occupant recovery. There is provided a quick release seat system suitable for a vehicle, comprising a base element operably attached to a floor pan, said floor pan being rigidly affixed to the vehicle, a back element for supporting an occupant, wherein said base element and back element are rigidly affixed by at least one quick release mechanical clamp, such as to allow removal of said back element from the base element during an evacuation of the vehicle

First claim

Opening claim text (preview).

1 . A quick release seat system suitable for a vehicle, the system comprising: a base element operably attached to a floor pan, said floor pan being rigidly affixable to the vehicle; and a back element for supporting an occupant; wherein said base element and back element are rigidly clamped by at least one quick release mechanical clamp, such as to allow removal of said back element from the base element during an evacuation of the vehicle. 2 . The seat system according to claim 1 , wherein said base element comprises a first structural member, and said back element comprises a second structural member, wherein said at least one quick release mechanical clamp releasably clamps said first structural member and said second structural member. 3 . The seat system according to claim 1 , wherein said at least one quick release mechanical clamp includes at least two quick release mechanical clamps, wherein the base element comprises at least two first structural members and the back element comprises at least two second structural members, wherein said at least two first structural members are each rigidly affixed to the base element, and said at least two second structural members are rigidly affixed to said back element, and wherein said at least two quick release mechanical clamps releasably clamp said at least two first structural members and said at least two second structural members. 4 . The system according to claim 3 , wherein the at least two quick release mechanical clamps are rigidly connected by an elongate support. 5 . The seat system according to claim 1 , wherein the back element comprises a first structural member and a second structural member, wherein said first structural member is mounted to the back element, wherein said second structural member is mounted to said seat element, and wherein said at least one quick release mechanical clamp releasably affixes said first structural member and said second structural member. 6 . The system according to claim 1 , wherein said base element comprises a first structural member, and said back element comprises a second structural member, wherein the at least one quick release mechanical clamp comprises at least two clamping surfaces suitable for providing a releasable clamping engagement with said first and second structural members, the system comprising: a hinge member interconnecting said clamping surfaces; a clamp bar engaged with (1) at least one first clamping surface and (2) a release lever, wherein said release lever is releasably secured to at least one second clamping surface; and a tensioner configured to apply tension to allow the clamp bar to releasably secure the at least two clamping surfaces on the first and second structural members. 7 . The system according to claim 6 , wherein the release lever is pivotally attached to the clamp bar, wherein said release lever comprises a cam arrangement, such that rotation of the release lever about the clamp bar moves from a first tensioned position, which provides the releasable clamping engagement, to a second reduced tension position, which allows quick release of the releasable clamping engagement from said at least two clamping surfaces. 8 . The system according to claim 1 , wherein said base element comprises a first structural member, and said back element comprises a second structural member, wherein the at least one quick release mechanical clamp and said first and/or second structural members comprise one or more co-operative voids and lugs. 9 . The system according to claim 6 , wherein said release lever is temporarily secured to at least one second clamping surface by a retaining pin. 10 . A method of converting a rigid seat system in an armoured land vehicle to the quick release seat system of claim 1 , wherein said rigid seat systems comprises a base element and a back element, the base element operably attached to a floor pan, said floor pan being rigidly affixable to the vehicle, said back element for supporting an occupant, the method comprising: cutting the rigid seat system at at least one location, to provide a severed seat system; removing the back element of the severed seat system from the base element of the severed seat system; and re-attaching the back element of the severed seat system to the base element of the severed seat system with the at least one quick release mechanical clamp. 11 . The method according to claim 10 , wherein said base element comprises a first structural member, and said back element comprises a second structural member, wherein the at least one quick release mechanical clamp comprises: at least two clamping surfaces suitable for providing a releasable clamping engagement with said first and second structural members; a hinge member interconnecting said clamping surfaces; a clamp bar engaged with (1) at least one first clamping surface and (2) a release lever, wherein said release lever is releasably secured to at least one second clamping surface; and a tensioner configured to apply tension to allow the clamp bar to releasably secure the at least two clamping surfaces on the first and second structural members. 12 . A method of removing an occupant to be extracted from an armoured land vehicle comprising the quick release seat system as defined in claim 1 , the method comprising: operating the quick release seat system; and removing the occupant from an access point of the armoured land vehicle. 13 . A quick release mechanical clamp, comprising: at least two clamping surfaces suitable for providing a releasable clamping engagement with first and second structural members of a vehicle seat, the seat including base and back elements for supporting an occupant, wherein said base element comprises the first structural member, and said back element comprises the second structural member; a hinge member interconnecting a first clamping surface and a second clamping surface; a clamp bar engaged with (1) said first clamping surface and (2) a release lever, wherein said release lever is releasably secured to a second clamping surface; and a tensioner configured to apply tension to allow the clamp bar to releasably secure the first clamping surface and second clamping surface on the first and second structural members. 14 . The clamp according to claim 13 , wherein the release lever is pivotally attached to the clamp bar, wherein said release lever comprises a cam arrangement, such that rotation of the release lever about the clamp bar moves from a first tensioned position,. which provides a releasable clamping engagement,. to a second reduced tension position, which allows quick release of the clamp releasable clamping engagement from said at least two clamping surfaces. 15 . A quick release seat system suitable for a vehicle, the system comprising: a base element comprising a first structural member; and a back element for supporting an occupant and comprising a second structural member; a quick release mechanical clamp that releasably clamps the first structural member and the second structural member, wherein the quick release mechanical clamp comprises at least two clamping surfaces suitable for providing a releasable clamping engagement with said first and second structural members, such as to allow removal of said back element from the base element during an evacuation of the vehicle. 16 . The system according to claim 15 , the quick release mechanical clamp comprising: a hinge member interconnecting said clamping surfaces; a clamp bar engaged with (1) at least one first clamping surface and (2) a rele

Assignees

Inventors

Classifications

  • the back rest being mounted or joined with an easy attachment system to the seat · CPC title

  • using quick release attachments · CPC title

  • B60N2/682Primary

    Joining means · CPC title

  • Shock resilient mounted seats for armoured or fighting vehicles · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

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

What does patent US2020062144A1 cover?
The following invention relates to occupant recovery from an armoured land vehicle, and to a system for occupant recovery. There is provided a quick release seat system suitable for a vehicle, comprising a base element operably attached to a floor pan, said floor pan being rigidly affixed to the vehicle, a back element for supporting an occupant, wherein said base element and back element are r…
Who is the assignee on this patent?
Bae Systems Plc
What technology area does this patent fall under?
Primary CPC classification B60N2/01508. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Feb 27 2020 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).