Pilot seat armrest assembly with synchronous lift and tilt adjustment

Patent metadata

Field	Value
Publication number	US-12565319-B2
Application number	US-202418429959-A
Country	US
Kind code	B2
Filing date	Feb 1, 2024
Priority date	Feb 1, 2024
Publication date	Mar 3, 2026
Grant date	Mar 3, 2026

Abstract

An adjustable armrest assembly for a seat such as a pilot seat. In embodiments, the armrest assembly includes an armrest frame, a leadscrew rotatably mounted in the armrest frame, a control wheel mounted to the leadscrew, an armpad subassembly pivotally attached to the armrest frame, and a tilt link subassembly coupled between the armrest frame and the armpad subassembly. In use, rotating the leadscrew synchronizes rotational motion of the armrest frame relative to the seat, and armpad subassembly motion relative to the armrest frame. In embodiments, the adjustment capability of the armrest assembly facilitates use with a flight controller positioned forward of the armrest.

First claim

What is claimed is:

1 . An armrest assembly, comprising:
an armrest frame for pivotal attachment to a seat frame member; a leadscrew rotatably mounted in the armrest frame; a control wheel mounted to the leadscrew; an armpad subassembly pivotally attached to the armrest frame, the armpad subassembly including at least one inclined slot; and a tilt link subassembly having a first end mounted on the leadscrew and a second end engaged in and configured to travel along the at least one inclined slot; wherein the leadscrew, the tilt link, and the at least one inclined slot are arranged such that, in use: rotating the leadscrew in a first direction causes the armrest frame to pivot upward and the armpad subassembly to pivot away from the armrest frame; and rotating the leadscrew in a second direction, opposite the first direction, causes the armrest frame to pivot downward and the armpad subassembly to pivot toward the armrest frame.

2 . The armrest assembly according to claim 1 , wherein an aft end of the leadscrew extends to a position outside of the aft end of the armrest frame to bear against a bearing surface positioned on the seat frame member to control angular rotation of the armrest frame.

3 . The armrest assembly according to claim 1 , wherein the tilt link subassembly comprises:
at least one tilt link; a bearing axle mounted to the at least one tilt link; and at least one roller bearing mounted on the bearing axle.

4 . The armrest assembly according to claim 1 , wherein the armpad subassembly comprises:
a first armpad frame member forming a first inclined slot; a second armpad frame member forming a second inclined slot, the second armpad frame member attachable to the first armpad frame member; and an armpad mounted atop the first and second armpad frame members.

5 . The armrest assembly according to claim 4 , wherein the armpad has a convex shape.

6 . The armrest assembly according to claim 1 , wherein the armrest frame and the armpad subassembly are pivotally attached at their respective forward ends.

7 . The armrest assembly according to claim 1 , wherein:
the armrest frame includes a bottom cavity; the leadscrew is threadably engaged in the armrest frame for linear translation; and the control wheel is rotatably fixed to the leadscrew and positioned in the cavity for linear translation.

8 . The armrest assembly according to claim 1 , wherein the arrangement of the leadscrew, the tilt link, and the at least one inclined slot synchronizes pivoting motion of the armrest frame relative to the seat frame member, and pivoting motion of the armpad subassembly relative to the armrest frame.

9 . A pilot seat assembly, comprising:
left and right seat frame members each including an armrest hub; a seat back and a seat bottom positioned between the left and right seat frame members; and an armrest assembly rotatably attached to each of the left and the right seat frame members, the armrest assembly comprising:
an armrest frame rotatably mounted to its respective armrest hub;
a leadscrew rotatably mounted in the armrest frame;
a control wheel mounted to the leadscrew;
an armpad subassembly pivotally attached to the armrest frame, the armpad subassembly including at least one inclined slot; and
a tilt link subassembly having a first end mounted on the leadscrew and a second end engaged in and configured to travel along the at least one inclined slot;
wherein the leadscrew, the tilt link, and the at least one inclined slot are arranged such that, in use:
rotating the leadscrew in a first direction causes the armrest frame to pivot upward and the armpad subassembly to pivot away from the armrest frame; and
rotating the leadscrew in a second direction, opposite the first direction, causes the armrest frame to pivot downward and the armpad subassembly to pivot toward the armrest frame.

10 . The pilot seat assembly according to claim 9 , wherein an aft end of the leadscrew extends to a position outside of the aft end of the armrest frame and bears against a bearing surface positioned on the respective seat frame member to control angular rotation of the armrest frame.

11 . The pilot seat assembly according to claim 9 , wherein the tilt link subassembly comprises:
a first tilt link; a second tilt link attached the first tilt link, the leadscrew captured between the first and second tilt links; a bearing axle mounted to the first and second tilt links; and first and second roller bearings mounted on opposite ends of the bearing axle.

12 . The pilot seat assembly according to claim 9 , wherein the armpad subassembly comprises:
a first armpad frame member forming a first inclined slot; a second armpad frame member forming a second inclined slot, the second armpad frame member attachable to the first armpad frame member; and an armpad mounted atop the first and second armpad frame members.

13 . The pilot seat assembly according to claim 12 , wherein the armpad has a convex shape.

14 . The pilot seat assembly according to claim 9 , wherein:
the armrest frame and the armpad subassembly are pivotally attached at their respective forward ends; and the armrest frame is pivotally at its aft end to the respective seat frame member.

15 . The pilot seat assembly according to claim 9 , wherein:
the armrest frame includes a bottom cavity; the leadscrew is threadably engaged in the armrest frame for linear translation; and the control wheel is rotatably fixed to the leadscrew and positioned in the cavity for linear translation.

16 . The pilot seat assembly according to claim 9 , wherein the arrangement of the leadscrew, the tilt link, and the at least one inclined slot synchronizes pivoting motion of the armrest frame relative to the respective seat frame member, and pivoting motion of the armpad subassembly relative to the armrest frame.

17 . A pilot seat configuration, comprising:
a pilot seat including left and right seat frame members each including an armrest hub; an armrest assembly rotatably attached to each of the left and the right seat frame members, the armrest assembly comprising:
an armrest frame rotatably mounted to its respective armrest hub;
a leadscrew rotatably mounted in the armrest frame;
a control wheel mounted to the leadscrew;
an armpad subassembly pivotally attached to the armrest frame, the armpad subassembly including at least one inclined slot; and
a tilt link subassembly coupled to the leadscrew and engaged in the at least one inclined slot; and
a flight controller positioned forward of one of the armrest assemblies.

18 . The pilot seat configuration according to claim 17 , wherein, in use:
rotating the leadscrew in a first direction causes the tilt link subassembly to travel in a first direction thereby causing the armrest frame to pivot upward and the armpad subassembly to pivot away from the armrest frame; and rotating the leadscrew in a second direction, opposite the first direction, causes the tilt link assembly to travel in a second direction, opposite the first direction, thereby causing the armrest frame to pivot downward and the armpad subassembly to pivot toward the armrest frame.

19 . The pilot seat configuration according to claim 17 , wherein an aft end of the leadscrew extends to a position outside of the aft end of the armrest frame and bears against a bearing surface positioned on the respective seat frame member to control angular rotation of the armrest frame.

20 . The pilot s

Assignees

• Ami Ind Inc

Inventors

• Hoover Douglas E
• Decola Nicholas

Classifications

• B64D11/0689

  specially adapted for pilots · CPC title

• B60N2/77

  Height adjustment · CPC title

• B60N2/767

  Angle adjustment · CPC title

• B64D11/0644 Primary

  Adjustable arm rests · CPC title