Tracking base assembly for aircraft seat

Patent metadata

Field	Value
Publication number	US-11338922-B2
Application number	US-201715702324-A
Country	US
Kind code	B2
Filing date	Sep 12, 2017
Priority date	Sep 12, 2017
Publication date	May 24, 2022
Grant date	May 24, 2022

Abstract

A tracking base assembly for an aircraft seat includes base rails mounted to floor tracks in an aircraft cabin by floor track fittings in fixed positions, the base rails connected by a tracking member for providing longitudinal tracking while minimizing added height. The base rails include tracking slots extending longitudinally, and the tracking member includes tracking elements translatable forward and backward along the tracking slots, allowing an aircraft seat mounted to the tracking member to translate forward from a retracted configuration into an extended or berthing configuration (and backward to the retracted configuration). The tracking member includes a locking mechanism for locking the tracking member and seat in intermediate positions within the tracking slots. The tracking slots may be oriented slightly downward from the horizontal to allow for gravity-assisted tracking or to counteract the nose-up flight angles associated with cruising altitude, providing for easier seat tracking.

First claim

I claim:

1. A tracking base assembly for an aircraft seat, comprising:
two base rails configured for mounting to a floor of an aircraft, each base rail having an upper surface and including a tracking slot extending longitudinally from a first tracking position to a second tracking position;
the two base rails connected and held in spaced apart relations by a tracking member comprising:
a top surface configured to have an aircraft seat mounted thereto, the top surface extending between the two base rails no higher than the upper surface of the two base rails,
one or more paired tracking elements configured to translate along the tracking slots between the first tracking position and the second tracking position, each pair of tracking elements joined by a common axle within the tracking member;
and
a locking assembly configured to secure the tracking member between the first tracking position and the second between the first and the second tracking positions.

2. The tracking base assembly of claim 1 , wherein the locking assembly includes at least one electronic actuator configured to activate and deactivate the locking assembly.

3. The tracking base assembly of claim 1 , wherein the one or more paired tracking elements include at least one of paired sliding components, paired bearing components, or paired rolling components.

4. The tracking base assembly of claim 1 , wherein:
each base rail has an outside surface and an inside surface, the two or more inside surfaces facing each other and including the tracking slots.

5. The tracking base assembly of claim 4 , wherein the tracking slots extend from the inside surfaces to the outside surfaces.

6. The tracking base assembly of claim 1 , further comprising:
at least one tracking limiter disposed within the tracking slots, the at least one tracking limiter configured to restrict the translation of the tracking member beyond at least one intermediate tracking point corresponding to the tracking limiter.

7. The tracking base assembly of claim 1 , further comprising:
one or more lateral crossing spars configured to laterally connect and hold in spaced apart relations the two or more base rails.

8. An aircraft seat having a tracking base assembly, comprising:
a seat frame;
a seatback and a seatpan attached to the seat frame;
a tracking base assembly configured for mounting to the seat frame, the tracking base assembly configured for mounting to a floor of an aircraft and comprising:
two base rails configured for mounting to the floor, each base rail having an upper surface including a tracking slot extending longitudinally from a first tracking position to a second tracking position;
the two base rails connected and held in spaced apart relations by a tracking member to which the seat frame is configured for mounting, the seatback and seat frame configured to collectively translate between an upright configuration and a berthed configuration relative to the base rails via the tracking member, the tracking member comprising:
a top surface configured to have the aircraft seat mounted thereto, the top surface extending between the two base rails no higher than the upper surface of the two base rails, one or more paired tracking elements configured to translate along the tracking slots between the first tracking position and the second tracking position, each pair of tracking elements joined by a common axle;
and
a locking assembly configured to secure the tracking member between the first and the second tracking positions.

9. The aircraft seat of claim 8 , wherein the locking assembly includes at least one electronic actuator configured to activate and deactivate the locking assembly.

10. The aircraft seat of claim 8 , wherein the one or more paired tracking elements include at least one of paired sliding components, paired rolling components, or paired bearing components.

11. The aircraft seat of claim 8 , wherein:
each base rail has an outside surface and an inside surface, the two or more inside surfaces facing each other and including the tracking slots.

12. The aircraft seat of claim 11 , wherein the tracking slots extend from the inside surfaces to the outside surfaces.

13. The aircraft seat of claim 8 , further comprising:
at least one tracking limiter disposed within the tracking slots, the at least one tracking limiter configured to restrict the translation of the tracking member beyond at least one intermediate tracking point corresponding to the tracking limiter.

14. The aircraft seat of claim 13 , wherein the at least one tracking limiter is movable between the first tracking point and the second tracking point.

15. The aircraft seat of claim 8 , further comprising:
a swivel coupled to the tracking member, the seat frame mountable to the tracking member via the swivel and capable of rotating relative to a z-axis of the swivel.

16. The aircraft seat of claim 8 , further comprising:
an extended tracking module coupled to the tracking member, the seat frame mountable to the extended tracking module, the extended tracking module configured to:
longitudinally articulate the seat frame parallel to a longitudinal axis; and
laterally articulate the seat frame perpendicular to the longitudinal axis.

17. The aircraft seat of claim 8 , further comprising:
one or more lateral crossing spars configured to laterally connect and hold in spaced apart relations the two or more base rails.

Assignees

• Rockwell Collins Inc

Inventors

• Oleson Michael L

Classifications

• B64D11/064

  Adjustable inclination or position of seats · CPC title

• B60N2/062

  transversally slidable · CPC title

• B60N2/14

  rotatable, e.g. to permit easy access (B60N2/10 {, B60N2/2869} take precedence) · CPC title

• B60N2/0717

  Rounded, e.g. circular · CPC title

• B64D11/0696 Primary

  Means for fastening seats to floors, e.g. to floor rails · CPC title