IP Library › Granted Patent US 12,559,239
Granted Patent B2
US 12,559,239 · App. 18/615,117 · Granted Feb 24, 2026

Integrated seat assembly with headrest and neck support

Inventors: Sambasiva Rao Kodati (Vinjaram, IN); Chandra Sekhar Gudla (Hyderabad, IN); Guruswamy Prasad Gundra (Hyderabad, IN)
Assignee: B/E Aerospace, Inc.
B64D11/0642
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Quick Facts
Patent No.
US 12,559,239
App. No.
18/615,117
Granted
Feb 24, 2026
Kind
B2
Abstract

An integrated seat assembly including a fixed subassembly attachable to a seat backrest, a headrest subassembly configured to translate along a rail of the fixed subassembly, and a neck support subassembly also configured to translate along the rail, independently of the translation of the headrest subassembly. Each of the headrest subassembly and the neck support subassembly include articulating supports configured to enhance support of comfort of the respective subassemblies. Each of the headrest subassembly and the neck support subassembly may include a cushion for further comfort.

Claims (41)

1 . A headrest assembly for mounting to a passenger seat, comprising:

a support plate for mounting to the passenger seat;

a rail mounted to the support plate;

a headrest subassembly including a headrest support plate translatably mounted to the rail, a left headrest support rotatably mounted to the headrest support plate, and a right headrest support rotatably mounted to the headrest support plate; and

a neck support subassembly including a neck support plate translatably mounted to the rail, a left neck support mounted to the neck support plate, and a right neck support mounted to the neck support plate;

wherein the headrest subassembly and the neck support subassembly are independently translatable along the rail.

2 . The headrest assembly according to claim 1 , wherein each of the left neck support and the right neck support comprise a plurality of rotatably connected individual segments.

3 . The headrest assembly according to claim 1 , wherein each of the left neck support and the right neck support are fully articulating gooseneck supports.

4 . The headrest assembly according to claim 1 , wherein each of the left headrest support, the right headrest support, the left neck support, and the right neck support are configured to deploy, independently, in a forward direction away from the support plate.

5 . The headrest assembly according to claim 1 , wherein each of the headrest support plate, the left headrest support, the right headrest support, the neck support plate, the left neck support, and the right neck support carries a cushion.

6 . The headrest assembly according to claim 1 , wherein:

each of the headrest subassembly and the neck support subassembly further comprises a cushion;

the cushion of the headrest subassembly is continuous across the left headrest support, the headrest support plate, and the right headrest support; and

the cushion of the neck support subassembly is continuous across the left neck support, the neck support plate, and the right neck support.

7 . The headrest assembly according to claim 1 , wherein the headrest subassembly and the rail interface through a first set of rollers, and the neck support subassembly and the rail interface through a second set of rollers.

8 . The headrest assembly according to claim 1 , wherein at least one of the headrest subassembly and the neck support subassembly further comprises an internal speaker.

9 . The headrest assembly according to claim 1 , wherein at least one of the headrest subassembly and the neck support subassembly further comprises at least one of an internal massager, an internal fan, and an internal heater.

10 . An aircraft passenger seat, comprising:

a backrest; and

a headrest assembly, comprising:

a support plate mounted to the backrest;

a rail mounted to the support plate;

a headrest subassembly including a headrest support plate translatably mounted to the rail, a left headrest support rotatably mounted to the headrest support plate, and a right headrest support rotatably mounted to the headrest support plate; and

a neck support subassembly including a neck support plate translatably mounted to the rail, a left neck support mounted to the neck support plate, and a right neck support mounted to the neck support plate;

wherein the headrest subassembly and the neck support subassembly are independently translatable along the rail.

11 . The aircraft passenger seat according to claim 10 , wherein each of the left neck support and the right neck support comprise a plurality of rotatably connected individual segments.

12 . The aircraft passenger seat according to claim 10 , wherein each of the left neck support and the right neck support are fully articulating gooseneck supports.

13 . The aircraft passenger seat according to claim 10 , wherein each of the left headrest support, the right headrest support, the left neck support, and the right neck support are configured to deploy, independently, in a forward direction away from the support plate.

14 . The aircraft passenger seat according to claim 10 , wherein:

each of the headrest subassembly and the neck support subassembly further comprises a cushion;

the cushion of the headrest subassembly is continuous across the left headrest support, the headrest support plate, and the right headrest support; and

the cushion of the neck support subassembly is continuous across the left neck support, the neck support plate, and the right neck support.

15 . The aircraft passenger seat according to claim 10 , wherein at least one of the headrest subassembly and the neck support subassembly further comprises at least one of an internal speaker, an internal massager, an internal fan, and an internal heater.

16 . The aircraft passenger seat according to claim 10 , wherein the headrest subassembly and the fixed subassembly interface through a first set of rollers, and the neck support subassembly and the fixed subassembly interface through a second set of rollers.

17 . A headrest assembly for mounting to a passenger seat, comprising:

a support plate mountable to the passenger seat;

a vertical rail mounted to the support plate;

a headrest subassembly translatably mounted to the rail, the headrest subassembly configured to translate vertically along the rail, the headrest subassembly including a headrest support plate, a left headrest support rotatably mounted to the headrest support plate, and a right headrest support rotatably mounted to the headrest support plate; and

a neck support subassembly translatably mounted to the rail, the neck support subassembly configured to translate vertically along the rail, the neck support subassembly including a neck support plate, a left neck support mounted to the neck support plate, and a right neck support mounted to the neck support plate;

wherein the headrest subassembly and the neck support subassembly are configured for independent vertical translation along the rail.

18 . The headrest assembly according to claim 17 , wherein each of the left neck support and the right neck support comprise a plurality of rotatably connected individual segments or articulating gooseneck supports.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 8, 2024
From: BE ENGINEERING SERVICES INDIA PRIVATE LIMITED
To: B/E AEROSPACE, INC.
Reel/Frame 067350/0517 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 25, 2024
From: KODATI, SAMBASIVA RAO; GUDLA, CHANDRA SEKHAR; GUNDRA, GURUSWAMY PRASAD
To: BE ENGINEERING SERVICES INDIA PRIVATE LIMITED
Reel/Frame 066886/0062 →
Priority Claims (1)
IN 202311041897 · Jun 23, 2023 · national
Continuity (1)
Related Publication 20240425182A1 · Dec 26, 2024
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