Device to resolve angled ottoman configuration
A deployable ottoman extension fills the gap between the ottoman and fully reclined oblique aircraft seat. The deployable ottoman extension can pivot out from the ottoman about a pivot point and/or slide out along a rail. Alternatively, the ottoman extension may be hinged to the ottoman to deploy by flipping down. The deployable ottoman extension may include deployable support features that extend to the aircraft floor when deployed.
1. An aircraft seat system comprising:
an ottoman defining a cavity configured to receive a deployable ottoman extension;
a fully reclining seat, separate from the ottoman; and
a deployable ottoman extension, separate from the fully reclining seat, configured to deploy from the cavity,
wherein the deployable ottoman extension is configured to pivotably deploy and at least partially occupy a gap defined by a surface of the fully reclining seat when the fully reclining seat is reclined and the ottoman.
2. The aircraft seat system of claim 1 , further comprising:
an extension rail disposed on an internal surface of the ottoman; and
an extension guide disposed on a surface of the deployable ottoman extension,
wherein the extension guide is configured to engage and slide along the extension rail during deployment and define a maximum deployment of the deployable ottoman extension.
3. The aircraft seat system of claim 1 , further comprising a stowable support element pivotably mounted on a surface of the deployable ottoman extension.
4. The aircraft seat system of claim 1 , wherein:
the deployable ottoman extension comprises an attachment element configured to releasably affix the deployable ottoman extension to the fully reclining seat when deployed.
5. An aircraft ottoman comprising:
a deployable ottoman extension configured to pivotably deploy and at least partially occupy a gap defined by a surface of a fully reclining seat when the fully reclining seat is reclined and the aircraft ottoman,
wherein:
the aircraft ottoman defines a cavity configured to receive the deployable ottoman extension; and
the aircraft ottoman and deployable ottoman extension are separate from the fully reclining seat.
6. The aircraft ottoman of claim 5 , further comprising:
an extension rail disposed on an internal surface of the ottoman; and
an extension guide disposed on a surface of the deployable ottoman extension,
wherein the extension guide is configured to engage and slide along the extension rail during deployment and define a maximum deployment of the deployable ottoman extension.
7. The aircraft ottoman of claim 5 , further comprising a stowable support element pivotably mounted on a surface of the deployable ottoman extension.
8. The aircraft ottoman of claim 5 , wherein:
the deployable ottoman extension comprises an attachment element configured to releasably affix the deployable ottoman extension to the fully reclining seat when deployed.