Ejection seat pan lifter

• US 9,783,310 B2
• Filed: 08/26/2013
• Issued: 10/10/2017
• Est. Priority Date: 08/26/2013
• Status: Active Grant

• Current Assignee: AMI Industries, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: AMI Industries, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Mastrolia, Bradley, Hampton, John, Tulloch, James, Ochs, Jeremy
• Primary Examiner(s): Allred, David E
• Application Number:
  US14/010,009
• Publication Number:
  US 20150054323A1
• Time in Patent Office: 1,506 Days
• Field of Search: 29725613, 29728411, 297313, 297328, 297337
• CPC Class Codes: B64D 25/10 Ejector seats

Abstract

An aircraft is provided and includes a fixed frame including a ledge and a seat pan on which seating elements for seating an aircraft crewperson are disposable. The seat pan includes a hinge about which the seat pan is pivotable relative to the fixed frame and a flange disposable on the ledge to establish a first pivot position for the seat pan relative to the fixed frame and a seat pan lifter coupled to the fixed frame and selectively interposable between the flange and the ledge to establish a second pivot position for the seat pan relative to the fixed frame.

Claims

1. An aircraft ejection seat assembly, comprising:

a fixed frame including an elongate ledge extending lengthwise in a direction transverse to a forward direction;

a seat pan on which seating elements for seating first and second aircraft crewpersons of differing heights are disposable,

the seat pan being pivotable about a hinge connected at a front edge of the seat pan and configured to assume a first pivot position associated with the first aircraft crewperson; and

a seat pan lifter comprising an elongated block selectively disposed lengthwise in the transverse direction on the ledge at a rear end of the seat pan, the seat pan lifter configured to thereby establish and support the seat pan in a second pivot position associated with the second aircraft crewperson;

wherein the seat pan pivots about the hinge relative to the fixed frame as the seat pan is pivoted from the first pivot positions to the second pivot position.

2. The aircraft ejection seat assembly according to claim 1, wherein the seat pan is configured for ejection from the aircraft.

3. The aircraft ejection seat assembly according to claim 1, wherein the seat pan comprises an ejection handle proximate to the hinge.

4. The aircraft ejection seat assembly according to claim 1, wherein the seat pan comprises a survival kit, the seat pan lifter being selectively disposable in a non-use position proximate to the survival kit.

5. The aircraft ejection seat assembly according to claim 1, further comprising securing members connectable to the seat pan lifter.

6. The aircraft ejection seat assembly according to claim 1, wherein the seat pan lifter has a tapered cross-section.

7. The aircraft ejection seat assembly according to claim 1, wherein the seat pan lifter comprises a body formed to define one or more cavities.