Butterfly leafs for economy seat middle handle
A stowable armrest extension rotates or translates from the armrest and deploys into one or more horizontal extensions. Linking elements connect the movement of various components to direct, restrict, and automate deployment. A central column may isolate the butterfly leafs to prevent incidental contact between neighboring passengers. An actuator may apply a force to deploy the stowable armrest extension, either when a release is activated or when a top cap is moved.
1. An aircraft armrest comprising:
an armrest body defining an internal space and an opening in a top portion;
a top cap configured to moveably cover the opening in the top portion; and
a deployable armrest extension disposed in the internal space, comprising:
one or more hinged leafs; and
a deployment mechanism comprising:
a translation channel configured to direct the deployable armrest extension upward through the opening in the top portion;
one or more top cap directing channels configured to engage corresponding pins in the top cap and direct the top cap into the internal space; and
a linkage connecting the corresponding pins to the deployable armrest extension to actuate movement of the top cap when the deployable armrest extension is deployed.
2. The aircraft armrest of claim 1 , wherein the linkage comprises a cable and pulley.
3. The aircraft armrest of claim 1 , wherein the deployment mechanism comprises:
a linear actuator configured to bias the deployable armrest extension into a deployed configuration; and
a release mechanism configured to retain the linear actuator until released.
4. The aircraft armrest of claim 1 , wherein the deployment mechanism comprises a rotation arm configured to allow the deployable armrest extension to rotate out of the internal space.
5. The aircraft armrest of claim 4 , wherein the top cap is configured to close and cover the opening in the top portion and provide a resting surface for the deployable armrest extension when deployed.
6. The aircraft armrest of claim 1 , wherein the deployable armrest extension comprises a central column configured to remain vertical when the one or more hinged leafs are deployed horizontally.
7. The aircraft armrest of claim 1 , wherein:
the top cap is affixed to the deployable armrest extension;
the deployable armrest extension is configured to vertically translate out of the internal space sufficiently for the one or more hinged leafs to rotate up into a horizontal configuration, and then translate back into the internal space.
8. A deployable armrest extension comprising:
one or more hinged leafs; and
a deployment mechanism comprising:
a translation channel configured to direct the deployable armrest extension upward through an opening in a top portion of an armrest body;
one or more top cap directing channels configured to engage corresponding pins in the top cap and direct the top cap into an internal space of the armrest body;
a linkage connecting the corresponding pins to the deployable armrest extension to actuate movement of the top cap when the deployable armrest extension is deployed;
a linear actuator configured to bias the deployable armrest extension into a deployed configuration; and
a release mechanism configured to retain the linear actuator until released.
9. The aircraft armrest of claim 8 , wherein the linkage comprises a cable and pulley.
10. The aircraft armrest of claim 8 , wherein the deployment mechanism comprises a rotation arm configured to allow the deployable armrest extension to rotate out of the internal space.
11. The aircraft armrest of claim 10 , wherein the deployment mechanism further comprises a translation channel configured to direct the deployable armrest extension upward through the opening in the top portion.
12. The aircraft armrest of claim 8 , wherein the deployable armrest extension comprises a central column configured to remain vertical when the one or more hinged leafs are deployed horizontally.