Aircraft Seat

Patent metadata

Field	Value
Publication number	US-2025388324-A1
Application number	US-202418752485-A
Country	US
Kind code	A1
Filing date	Jun 24, 2024
Priority date	Jun 24, 2024
Publication date	Dec 25, 2025
Grant date	—

Abstract

Contemporary aircraft seats are often designed to meet specifications regarding safety and flightworthiness without much consideration for occupant comfort. The aircraft seats disclosed are designed to achieve a high level of occupant comfort while maintaining a simple, symmetrical, and lightweight construction. The seat comprises a mechanism with an actuator that can reconfigure the seat in TTOL, Task, Enhanced, Zero-G, and Slumber positions that each suit different activities a crew member or passenger may undertake while aboard an aircraft. At least one of the positions supports a neutral body posture, and the chair is thoroughly outfitted with rigid supports, comfortable padding, and a design contoured to the human body to maximize comfort. The seat can be configured with a control mechanism that may allow users to adjust the position of the seat via a mobile device or a control panel configured on the seat.

First claim

What is claimed is:

1 . An adjustable aircraft seat comprising:
a plurality of contoured seat components including a seat bottom, a seat back, a leg rest, and armrests, wherein each component of the plurality comprises a cushioned portion mounted on a base portion; a frame configured to support the seat bottom, seat back, leg rest, and armrests via each respective base portion; a motor mounted on the frame; and a mechanical linkage operatively coupling the motor with components of the frame such that operation of the motor moves the seat bottom, seat back, leg rest and armrests simultaneously, wherein adjustment of the aircraft seat by the motor occurs through a single joint pivotally coupled to the mechanical linkage.

2 . The adjustable aircraft seat of claim 1 , wherein the base portions and the frame comprise a lightweight rigid material configured to prevent deformation of the aircraft seat when an occupant is seated.

3 . The adjustable aircraft seat of claim 1 , wherein a cushioned portion of the seat back comprises a relief configured to distribute pressure around an occupant's spine.

4 . The adjustable aircraft seat of claim 1 , wherein the cushioned portions comprise memory foam contoured to partially envelop an occupant seated within the aircraft seat.

5 . The adjustable aircraft seat of claim 1 , wherein the contoured seat components and the frame each possess left-right symmetry such that inboard and outboard portions of the aircraft seat are indistinguishable.

6 . The adjustable aircraft seat of claim 1 , comprising a controller configured to send commands to the motor to adjust the seat by adjusting the mechanical linkage.

7 . The adjustable aircraft seat of claim 6 , wherein the motor, the mechanical linkage, and the single joint are configured to move the aircraft seat to a pre-defined seating position based on a selection received via the controller.

8 . The adjustable aircraft seat of claim 7 , wherein one of the pre-defined seating positions configures the seat into a position which supports a neutral body posture.

9 . The adjustable aircraft seat of claim 7 , comprising a spine linked to the motor such that the motor reclines the spine at the single joint to engage the mechanical linkage.

10 . A crew seat adjustment system comprising:
a frame comprising a pair of rigid trusses, wherein the pair of trusses are arranged substantially parallel with one another; a frame arm linked to the frame at a joint such that the frame arm is pivotable relative to the frame while the frame remains static; a first mechanical linkage comprising two branches of arms linked at a plurality of joints, wherein one branch comprises the frame arm and whereby pivoting the frame arm extends the mechanical linkage; and a second mechanical linkage with a platform and a spine, wherein the second mechanical linkage is configured to pitch the platform up and pivot the frame arm upon reclining of the spine.

11 . The crew seat adjustment system of claim 10 , comprising a motor configured to recline the spine at a joint, thereby engaging the first and second mechanical linkages when the spine is reclined by the motor.

12 . The crew seat adjustment system of claim 10 , comprising a leg rest having a cushioned portion and a rigid base portion, wherein the rigid base portion is mechanically coupled to an end of the first mechanical linkage.

13 . The crew seat adjustment system of claim 10 , wherein the two branches of arms of the first mechanical linkage comprise arms of differing lengths such that a leg rest mounted to both of the two branches of arms rotates upward when the first mechanical linkage is extended.

14 . The crew seat adjustment system of claim 10 , wherein the second mechanical linkage comprises a plurality of bushings such that each bushing constrains movement of the platform, and wherein the platform slides relative to the bushings.

15 . The crew seat adjustment system of claim 10 , comprising a plurality of cushioned components configured to seat an occupant and to distribute pressure between the seat and a seated occupant in a neutral body posture.

16 . The crew seat adjustment system of claim 10 , comprising a plurality of linking members linked to each rigid truss such that the plurality of linking members maintain symmetry and a common width between the rigid trusses.

17 . The crew seat adjustment system of claim 10 , comprising an attachment member operatively coupled to the frame, wherein the attachment member is configured to rigidly secure the crew seat to a floor of an aircraft.

18 . A method for adjusting a crew seat into a plurality of positions, including:
defining a plurality of seating positions on a control surface, including a TTOL, Task, Enhanced, Zero-G, and Slumber position, wherein the seating positions may be assumed by a crew seat with a rigid frame; providing an instruction from the control surface to an electric actuator configured to extend a first mechanical linkage and to raise a second mechanical linkage; raising a leg rest upward and outward by extending the first mechanical linkage; dropping a rear portion of a seat bottom by raising the second mechanical linkage; and reclining a seat back by raising the second mechanical linkage.

19 . The method of claim 18 , further comprising:
adjusting the crew seat to the Task position; providing an option on the control surface for adjusting the position of the crew seat along a range of non-discrete motion; and adjusting the crew seat along the range of non-discrete motion while remaining in the Task position.

20 . The method of claim 18 , wherein the electric actuator is configured to operate the first and second mechanical linkages independently of one another.

Assignees

• Textron Aviation Inc

Inventors

• Robinson Michael Scott
• Davis David Wayne
• Decker Jason Michael
• Rowe Frank Joseph
• Williams Merril Binford

Classifications

• B64D11/0641

  Seats convertible into beds · CPC title

• B64D11/06395

  characterised by the arrangement of electric motors for adjustment · CPC title

• B64D11/064 Primary

  Adjustable inclination or position of seats · CPC title

• B64D11/0644

  Adjustable arm rests · CPC title

• B64D11/0696

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