Deployable portable electronic device holder for aircraft seat
A portable electronic device holder, separate from an aircraft tray table, has a spring biased lower retention portion with lower retention plates for securing a lower edge of a portable electronic device. The lower retention plate acts in concert with either one or more ridges molded into or affixed to a recess in a seat back panel, or with a spring biased, extendable upper retention portion with an upper retention plate to hold the portable electronic device in place.
1. A portable electronic device holder, disposed in an aircraft seat back housing, comprising:
a lower retention portion comprising at least two retention plates configured to abut an edge of a portable electronic device, a first lower retention plate defining a first viewing angle and a second lower retention plate defining a second viewing angle;
one or more lower extension arms disposed on a surface of the lower retention portion, the one or more extension arms configured to allow the lower retention portion to rotate away from an aircraft seat back; and
one or more upper retention elements,
wherein the at least two lower retention plates and one or more upper retention elements are configured to hold the portable electronic device in a static position relative to the aircraft seat back, and interlock when in a stowed orientation.
2. The portable electronic device holder of claim 1 , wherein the one or more upper retention elements comprise an upper retention plate disposed on an upper extension arm, the upper extension arm configured to move linearly along a path parallel to the aircraft seat back.
3. The portable electronic device holder of claim 2 , wherein the upper retention element is biased toward a stowed orientation by a spring.
4. The portable electronic device holder of claim 3 , further comprising a linkage disposed on the one or more lower extension arms, the linkage configured to apply an upward force to the upper extension arm to partially extend the upper retention element upward.
5. The portable electronic device holder of claim 2 , further comprising an inductive charging element disposed in the upper extension arm.
6. An aircraft passenger seat comprising:
a portable electronic device holder comprising:
a lower retention portion comprising at least two lower retention plates configured to abut an edge of a portable electronic device, a first lower retention plate defining a first viewing angle and a second lower retention plate defining a second viewing angle;
one or more lower extension arms disposed on a surface of the lower retention portion, the one or more extension arms configured to allow the lower retention portion to rotate away from the aircraft passenger seat back; and
one or more upper retention elements,
wherein the at least two lower retention plates and one or more upper retention elements are configured to hold the portable electronic device in a static position relative to the aircraft passenger seat back, and interlock when in a stowed orientation.
7. The aircraft passenger seat of claim 6 , wherein the upper retention elements are disposed on the aircraft seat back.
8. The aircraft passenger seat of claim 6 , wherein the one or more upper retention elements comprise an upper retention plate disposed on an upper extension arm, the upper extension arm configured to move linearly along a path parallel to the aircraft passenger seat back.
9. The aircraft passenger seat of claim 8 , wherein the upper retention element is biased toward a stowed orientation by a spring.
10. The aircraft passenger seat of claim 9 , further comprising a linkage disposed on the one or more lower extension arms, the linkage configured to apply an upward force to the upper extension arm to partially extend the upper retention element upward.
11. An aircraft comprising:
an aircraft passenger seat having a portable electronic device holder comprising:
a lower retention portion comprising at least two lower retention plates configured to abut an edge of a portable electronic device, a first lower retention plate defining a first viewing angle and a second lower retention plate defining a second viewing angle;
one or more lower extension arms disposed on a surface of the lower retention portion, the one or more extension arms configured to allow the lower retention portion to rotate away from an aircraft seat back; and
one or more upper retention elements,
wherein the at least two lower retention plates and one or more upper retention elements are configured to hold the portable electronic device in a static position relative to the aircraft seat back, and interlock when in a stowed orientation.
12. The aircraft of claim 11 , wherein the upper retention elements are disposed on the aircraft seat back.
13. The aircraft of claim 11 , wherein the one or more upper retention elements comprise an upper retention plate disposed on an upper extension arm, the upper extension arm configured to move linearly along a path parallel to the aircraft seat back.
14. The aircraft of claim 13 , wherein the upper retention element is biased toward a stowed orientation by a spring.
15. The aircraft of claim 14 , further comprising a linkage disposed on the one or more lower extension arms, the linkage configured to apply an upward force to the upper extension arm to partially extend the upper retention element upward.