Independently articulating seat pan for aircraft seat

• US 9,452,838 B2
• Filed: 10/20/2014
• Issued: 09/27/2016
• Est. Priority Date: 10/21/2013
• Status: Active Grant

• Current Assignee: B/E Aerospace, Inc. (Rtx Corporation)
• Original Assignee: B/E Aerospace, Inc. (Rtx Corporation)
• Inventors: Meister, Peter C., Mahabaleshwara, Aravinda
• Primary Examiner(s): Brindley, Timothy J
• Application Number:
  US14/518,619
• Publication Number:
  US 20150108804A1
• Time in Patent Office: 708 Days
• Field of Search: 297/344.14, 297/313, 297/322, 297/337, 297/69, 297/423.26
• US Class Current: 1/1
• CPC Class Codes: B60N 2/10 tiltable B60N2/12 , B60N2/2875 take precedence
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats

Abstract

A seat pan assembly including a fixed seat pan frame defining a substantially horizontal forward portion and a rear portion at an angle to horizontal, and a seat pan pivotally supported on the fixed seat pan frame, the seat pan having a pivot axis established through a width of the seat pan such that the seat pan is free to pivot relative to the fixed seat pan frame between substantially horizontal and an angle to horizontal. An aircraft passenger seat including a seat pan assembly adapted to adjust independent of seatback recline motion.

Claims

1. A seat pan assembly, comprising:

a fixed seat pan frame defining a substantially horizontal forward portion and a rear portion at an angle to horizontal; and

a seat pan pivotally supported on the fixed seat pan frame, the seat pan having a pivot axis established through a width of the seat pan such that the seat pan is free to pivot relative to the fixed seat pan frame between substantially horizontal and an angle to horizontal;

wherein a forward end of the seat pan directly engages the substantially horizontal forward portion of the fixed seat pan frame when the seat pan is substantially horizontal and a rearward end of the seat pan directly engages the rear portion of the fixed seat pan frame when the seat pan is at an angle to horizontal, and wherein the rear portion of the fixed seat pan frame dictates the seat pan angle to horizontal and the substantially horizontal forward portion of the fixed seat pan frame prevents the forward end of the seat pan from pivoting downward past substantially horizontal.

2. The seat pan assembly of claim 1, wherein the fixed seat pan frame comprises parallel, spaced left-side and right-side rails, each of the left-side and right-side rails defining the substantially horizontal forward portion and the rear portion at an angle to horizontal.

3. The seat pan assembly of claim 2, wherein the left-side and right-side rails are shaped to dictate the pivoting range of motion of the seat pan relative to the fixed seat pan frame.

4. The seat pan assembly of claim 2, wherein the pivot axis is supported by the left-side and right-side seat rails.

5. The seat pan assembly of claim 1, wherein an object'"'"'s center of gravity is shifted aft of the pivot axis of the seat pan to incline the seat pan, and is shifted forward of the pivot axis to move the seat pan angle toward horizontal.

6. The seat pan assembly of claim 1, wherein the pivot axis is established at a position between a center and a forward edge of the seat pan.

7. The seat pan assembly of claim 1, wherein the seat pan is adapted to pivot relative to the fixed seat pan frame independent of seatback motion of a seat upon which the seat pan assembly is installed.

8. The seat pan assembly of claim 1, wherein the seat pan assembly is adapted to be supported on a fixed seat frame of an aircraft passenger seat.

9. The seat pan assembly of claim 1, wherein the seat pan is configured to pivot relative to the fixed seat pan frame between horizontal and 20 degrees from horizontal.

10. The seat pan assembly of claim 1, further comprising a lock for locking an angle of the seat pan relative to the fixed seat pan frame and an actuator for returning the seat pan to substantially horizontal.

11. The seat pan assembly of claim 1, further comprising a legrest linearly deployable from a front of the seat pan, the legrest pivotally supported on ends of parallel support members.

12. The seat pan assembly of claim 1, wherein the seat pan is constructed from sheet metal bent to define spaced, parallel left and right sides and a forward portion interconnecting the left and right sides and arranged perpendicular thereto.

13. An aircraft passenger seat, comprising:

a fixed seat frame including parallel, spaced left-side and right-side rails each defining a substantially horizontal forward portion and a rear portion at an angle to horizontal;

a seatback pivotally attached at one end to the fixed seat frame, the seatback configured to pivot relative to the fixed seat frame between upright and reclined positions; and

a seat pan frame configured to pivot relative to the underlying fixed seat frame independent of pivoting motion of the seatback, the seat pan frame having a pivot axis established through a width thereof such that the seat pan frame is free to pivot relative to the fixed seat frame between substantially horizontal and an angle to horizontal;

wherein a forward end of the seat pan frame directly engages the substantially horizontal forward portion of the fixed seat frame when the seat pan frame is substantially horizontal and a rearward end of the seat pan frame directly engages the rear portion of the fixed seat frame when the seat pan frame is at an angle to horizontal, and wherein the rear portion of the fixed seat frame dictates the seat pan frame angle to horizontal and the substantially horizontal forward portion of the fixed seat frame prevents the forward end of the seat pan frame from pivoting downward past substantially horizontal.

14. The aircraft passenger seat of claim 13, wherein the left-side and right-side rails are shaped to dictate the pivoting range of motion of the seat pan frame relative to the fixed seat frame.

15. The aircraft passenger seat of claim 13, wherein an object'"'"'s center of gravity is shifted aft of the pivot axis of the seat pan frame to incline the seat pan frame, and is shifted forward of the pivot axis to move the seat pan frame angle toward horizontal.

16. The aircraft passenger seat of claim 13, wherein the pivot axis is established at a position between a center and a forward edge of the seat pan frame.

17. The aircraft passenger seat of claim 13, wherein the seat pan frame is configured to pivot relative to the fixed seat frame between horizontal and 20 degrees from horizontal.

18. The aircraft passenger seat of claim 13, further comprising a lock for locking an angle of the seat pan frame relative to the underlying fixed seat frame and an actuator for returning the seat pan frame to substantially horizontal.

19. The aircraft passenger seat of claim 13, further comprising a legrest linearly deployable from a front of the seat pan frame, the legrest pivotally supported on ends of parallel support members.