Lock mechanism for rotary component control
US-2020324676-A1 · Oct 15, 2020 · US
US11919425B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11919425-B2 |
| Application number | US-202117563840-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 28, 2021 |
| Priority date | Dec 28, 2020 |
| Publication date | Mar 5, 2024 |
| Grant date | Mar 5, 2024 |
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A rotary recline mechanism for allowing reclining movement of a first part relative to a second part, the mechanism comprising: a first gear mechanism comprising first and second gear rings having first and second sets of teeth that engage to lock the first and second parts relative to each other and disengage on operation of an actuator to allow relative movement of the first and second parts by application of a force on one of the parts in a first direction, and a second override gear mechanism to allow relative movement of the first and second parts by application of a force in a second direction while the first and second sets of teeth are engaged.
Opening claim text (preview).
The invention claimed is: 1. A rotary recline mechanism for allowing reclining movement of a first part relative to a second part, the mechanism comprising: a first gear mechanism comprising a first gear ring and a second gear ring having a first set of teeth and a second set of teeth, respectively, that engage to lock the first part and the second part relative to each other and disengage on operation of an actuator to allow relative movement of the first part and the second part by application of a force on one of the parts in a first direction, and a second override gear mechanism to allow relative movement of the first part and the second part by application of a force in a second direction while the first set of teeth and second set of teeth are engaged, wherein the second override gear mechanism is a ratchet gear mechanism comprising: a second ratchet gear mechanism located within the second gear ring to provide an override function for the rotary recline mechanism whereby the first part relative to the second part can be returned to a start position without disengaging the first set of teeth and the second set of teeth by means of the actuator. 2. The rotary recline mechanism of claim 1 , further comprising a first flange configured to attach the mechanism to the first part, and a second flange configured to attach the mechanism to the second part, the first gear ring attached to the first flange and the second gear ring attached to the second flange. 3. The rotary recline mechanism of claim 2 , further comprising a main shaft around which the first gear ring and the second gear ring are mounted, wherein the main shaft is permanently secured to the second flange. 4. The rotary recline mechanism of claim 1 , further comprising a torsional spring tensioned to bias the first gear ring to a position in which the first part is upright relative to the second part. 5. The rotary recline mechanism of claim 1 , wherein the actuator comprises a cable to be pulled by a user. 6. The rotary recline mechanism of claim 1 , further comprising a main shaft around which the first gear ring and the second gear ring are mounted. 7. The rotary recline mechanism of claim 6 , further comprising a linear guide bearing arranged to slide along the main shaft. 8. The rotary recline mechanism of claim 1 , further comprising a ratchet gear cover housing secured to a hub, and a plurality of pawls pivotally mounted to the hub, wherein the second gear ring is provided with a plurality of inwardly extending teeth and the plurality of pawls are provided with outer teeth arranged to mesh with the plurality of inwardly extending teeth. 9. The rotary recline mechanism of claim 8 , wherein the pawls are mounted to the hub by means of pins. 10. The rotary recline mechanism of claim 1 , wherein at least one of the first set of teeth or the second set of teeth have a slope on one side that is steeper than the slope on a other side to enable the override function. 11. The rotary recline mechanism of claim 1 , further comprising a shear pin to limit an angular range of movement between the first part and the second part in normal operation, wherein the shear pin is configured to shear in response to a predetermined force, such that the angular range of movement between the first part and the second part is increased. 12. The rotary recline mechanism of claim 11 , further comprising hard stops that limit the angular range of movement to an increased range when the shear pin has sheared. 13. The rotary recline mechanism of claim 1 , wherein the first part is a seat back, and the second part is one of a seat pan or a seat cushion of a reclining seat. 14. An aircraft seat comprising: a seat back adjustable relative to a second part, the second part being one of a seat pan or a seat cushion; and a rotary mechanism configured to allow reclining movement of the seat back relative to the second part, the rotatory mechanism comprising: a first gear mechanism comprising a first gear ring and a second gear ring having a first set of teeth and a second set of teeth, respectively, that engage to lock the seat back and the second part relative to each other and disengage on operation of an actuator to allow relative movement of the seat back and the second part by application of a force on one of the seat back or the second part in a first direction; and a second override gear mechanism to allow relative movement of the seat back and the second part by application of a force in a second direction while the first set of teeth and the second set of teeth are engaged, wherein the second override gear mechanism is a ratchet gear mechanism comprising: a second ratchet gear mechanism located within the second gear ring to provide an override function for the rotary recline mechanism whereby the seat back relative to the second part can be returned to a start position without disengaging the first set of teeth and the second set of teeth by means of the actuator, wherein the actuator is provided on or in a seat arm of the aircraft seat.
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