Aircraft ejection seat with adjustable headrest

• US 7,500,639 B2
• Filed: 06/02/2006
• Issued: 03/10/2009
• Est. Priority Date: 06/02/2006
• Status: Active Grant

• Current Assignee: AMI Industries, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Mastrolia, Brad
• Primary Examiner(s): Carone; Michael
• Assistant Examiner(s): Lee; Benjamin P
• Application Number:
  US11/445,879
• Publication Number:
  US 20070278347A1
• Time in Patent Office: 1,012 Days
• Field of Search: 244/122.R, 244/122.A, 244/122.AB, 244/122.AC, 244/122.AD, 244/122.AE, 297/344.1, 297/344.12, 297/344.17, 297/410, 297/468, 297/474, 297/475
• US Class Current: 244/122.00R
• CPC Class Codes: B60N 2/02246 Electric motors therefor
• CPC Class Codes: B60N 2/0296 Central command actuator to selectively switch on or engage one of several special purpose circuits or mechanisms
• CPC Class Codes: B60N 2/164 Linear actuator, e.g. screw mechanism
• CPC Class Codes: B60N 2/821 with continuous positioning
• CPC Class Codes: B60N 2/829 characterised by their adjusting mechanisms, e.g. electric motors
• CPC Class Codes: B64D 25/10 Ejector seats

Abstract

An aircraft ejection seat includes a frame and a headrest. The vertical position of the seat is adjusted by a pair of motor driven lead screws that cooperate with threaded barrel nuts attached to the seat frame. The upper end of one of these motor driven lead screws drives a slip coupling driving a splined shaft. The splined shaft then drives a gearbox mounted to the seat frame. The gearbox in turn drives an upper lead screw, which acts on an upper barrel nut to move the headrest up and down relative to the seat frame. The upper lead screw is driven in the opposite direction from the lower lead screws. Consequently, as the seat moves up to accommodate a shorter pilot, the headrest moves down to accommodate the shorter torso of the shorter pilot.

Claims

1. An adjustable seat for mounting to an airframe of an aircraft, said adjustable seat comprising:

a seat frame, said seat frame having a back portion, a seat portion and a headrest,

a first lifting mechanism operatively attached to said seat frame for moving said seat frame from a first, lowered position to a second, elevated position, said first lifting mechanism comprising a first lead screw and a barrel nut, said first lead screw having a lower end driven by a motor attached to said airframe and an upper end extending upward from said lower end relative to said airframe when said airframe is in a normal horizontal orientation, said barrel nut being attached to said seat frame and engaging a threaded portion of said first lead screw for converting rotational motion of said first lead screw into linear motion of said barrel nut for lifting said seat frame relative to said airframe, said upper end of said first lead screw further including a splined extension;

a second lifting mechanism operatively attached to said headrest for moving said headrest from a first elevated position to a second lowered position, said second lifting mechanism comprising a coupling and a second lead screw, said coupling supported by a bearing attached to said seat frame and slidingly engaging said splined extension for transmitting torque from said splined extension to said second lead screw, said second lifting mechanism further comprising a second barrel nut attached to said headrest and engaging a threaded portion of said second lead screw for converting rotational motion of said second lead screw into linear motion of said barrel nut for lifting said headrest relative to said seat frame, said second lead screw having an effective pitch opposite to said first lead screw, whereby as said seat frame is elevated relative to said airframe, said head rest is synchronously lowered relative to said seat frame.

2. The adjustable seat of claim 1, wherein:

said head rest moves at a linear rate between 50 percent and 90 percent of the linear motion of said seat frame.

3. The adjustable seat of claim 1, further comprising:

a gearbox interposed between said coupling and said second lead screw, said gearbox causing said second lead screw to counter rotate relative to said first lead screw.

4. The adjustable seat of claim 1, further comprising:

a gearbox interposed between said coupling and said second lead screw, said gearbox causing said second lead screw to rotate more slowly than said first lead screw.

5. The adjustable seat of claim 3, wherein:

said second lead screw rotates at a speed between 50 percent and 90 percent of said first lead screw.

6. The adjustable seat of claim 1, further comprising:

a flight harness system, said flight harness system comprising

a reel attached to said seat frame;

a harness strap, said harness strap having a first portion having a first end stored on said reel and a second portion terminating in a second end having an attachment point attached to said seat frame proximal said headrest;

a harness pulley having a roller portion and a fitting for attaching said harness pulley to an occupant, said harness strap passing over said roller portion of said harness pulley;

a headrest mounting bracket attached to said headrest, said headrest mounting bracket having an upper guide and a lower guide for guiding said harness strap, said harness strap being routed so that it passes from said reel, then through said lower guide, through said roller portion of said harness pulley through said upper guide to said attachment point;

whereby as said headrest is elevated and lowered, said upper guide and said lower guide move with said headrest to align said harness pulley with said headrest.