Aircraft crew egress hatch assembly, system, and method

Patent metadata

Field	Value
Publication number	US-11987342-B2
Application number	US-202117517917-A
Country	US
Kind code	B2
Filing date	Nov 3, 2021
Priority date	Nov 3, 2021
Publication date	May 21, 2024
Grant date	May 21, 2024

Abstract

Crew egress pathways and crew egress pathway exits in aircraft, with the crew egress pathway exits comprising apparatuses, systems, and methods for reliable deployment and stowage of support straps within crew egress pathway exit hatches positioned, with crew egress pathway exit hatches configured to deploy within aircraft passenger compartments in aircraft.

First claim

What is claimed is:

1. A crew egress pathway exit comprising:
a crew egress pathway exit assembly, said crew egress pathway exit assembly comprising: an exit hatch support structure, said exit hatch support structure positioned at a crew egress pathway exit assembly, said crew egress pathway exit assembly in communication with a crew egress pathway; a movable exit hatch, said movable exit hatch in movable communication with the exit hatch support structure, a one-piece support strap in communication with the exit hatch support structure, said one-piece support strap further in communication with said movable exit hatch, said one-piece support strap comprising:
a support strap first end and a support strap second end, said support strap first end fixedly attached to the exit hatch support structure, said support strap second end fixedly attached to the movable exit hatch, said one-piece support strap comprising a plurality of support strap first sections, said plurality of support strap first sections comprising a first bending stiffness, at least two of the plurality of the support strap first sections adjoining an adjacent support strap second section, said support strap second section comprising a second bending stiffness, said second bending stiffness less than the first bending stiffness, said support strap second section interposed between two of the plurality of support strap first sections, said adjacent support strap second section configured to bend at the support strap second section as a flexible joint along a length of the one-piece support strap; wherein said movable exit hatch is in movable communication with the exit hatch support structure, said movable exit hatch configured to move through a range of motion from a stowed position to a deployed position with the movable exit hatch at least partially disengaged from the exit hatch support structure in the deployed position, with the movable exit hatch in substantial contact with the exit hatch support structure in the stowed position, and with the one-piece support strap in a stacked orientation in the stowed position;
wherein during moving the movable exit hatch from the deployed position to the stowed position the one-piece support strap is configured to form a folded one-piece support strap, said folded one-piece support strap configured to return into the stacked orientation and to occupy a predetermined folded one-piece support strap footprint in the stacked orientation;
wherein during moving the movable exit hatch from the stowed position to the deployed position the one-piece support strap is further configured to unfold at predetermined positions along the length of the one-piece support strap to form an unfolded one-piece support strap configured to unfold from the stacked orientation;
wherein the one-piece support strap comprises a plurality of flexible joints along a length of the one-piece support strap, said plurality of flexible joints configured to each rotate about an opposite axis of rotation relative to each prior and subsequent flexible joint, with the one-piece support strap configured to repeatedly fold upon itself into the stacked orientation; and
wherein the plurality of the support strap first sections each comprise a support strap first section diameter thickness, and said support strap second section comprises a support strap second section diameter thickness that differs from support strap first section diameter thickness.

2. The crew egress pathway exit of claim 1 , wherein the one-piece support strap is configured to fold and form a folded one-piece support strap, said folded support strap configured to remain within the predetermined folded support strap footprint, said folded one-piece support strap further configured to facilitate intimate contact of a movable exit hatch perimeter with the exit hatch support structure in the closed position.

3. The crew egress pathway exit of claim 1 , wherein the plurality of support strap first sections are made from a material comprising at least one of: nylon, cloth, plastic, metal, and combinations thereof.

4. The crew egress pathway exit of claim 1 , wherein the support strap second section is made from a material comprising at least one of: nylon, cloth, plastic, metal, and combinations thereof.

5. The crew egress pathway exit of claim 1 , wherein said one-piece support strap in the deployed position comprises a tensile strength sufficient to support a weight up to 500 lbs.

6. The crew egress pathway exit of claim 1 , wherein a support strap second section defines a flexible joint in the one-piece support strap, said flexible joint operable about an axis of rotation.

7. An aircraft comprising:
an aircraft cabin, said aircraft cabin comprising:
a crew egress pathway exit assembly, said crew egress pathway exit assembly in communication with a crew egress pathway, said crew egress pathway exit assembly comprising:
an exit hatch support structure; a movable exit hatch, said movable exit hatch in movable communication with the movable exit hatch support structure, a one-piece support strap, said one-piece support strap in communication with the exit hatch support structure, said one-piece support strap further in communication with the movable exit hatch, said one-piece support strap comprising:
a support strap first end and a support strap second end, said support strap first end fixedly attached to the exit hatch support structure, said support strap second end fixedly attached to the movable exit hatch, said one-piece support strap comprising a plurality of support strap first sections, said plurality of support strap first sections comprising a first bending stiffness, at least two of the plurality of the support strap first sections adjoining an adjacent support strap second section, said support strap second section comprising a second bending stiffness, said second bending stiffness less than the first bending stiffness, said support strap second section interposed between two of the plurality of support strap first sections, said adjacent support strap second section configured to bend at the support strap second section as a flexible joint along a length of the one-piece support strap;
wherein said movable exit hatch is in movable communication with the exit hatch support structure, said movable exit hatch configured to move through a range of motion from a stowed position with the movable exit hatch in a closed position with the movable exit hatch in substantial contact with the exit hatch support structure in the stowed position to a deployed position with the movable exit hatch in an open position with the movable exit hatch at least partially disengaged from the exit hatch support structure in the deployed position;
wherein during moving the movable exit hatch from the deployed position to the stowed position the one-piece support strap is configured to fold to form a folded one-piece support strap, with the folded one-piece support strap configured to return to a predetermined folded one-piece support strap footprint; wherein during moving the movable exit hatch from the stowed position to the deployed position the one-piece support strap is further configured to fold at predetermined positions along the length of the one-piece support strap; and
wherein the plurality of the support strap first sections each comprise a support strap first section diameter thickness, and said support strap second section comprises a support strap second section diameter thickness that differs from support strap first section diameter thickness.

8. The aircraft of claim 7 , wherein the plurality of support strap first sections is made from a material comprising at least one of: nylon, cloth, plastic, metal, and combinations thereof, and

Assignees

• Boeing Co

Inventors

• Rhynard Steven Ellis
• Files Joe
• Fraker Randall Vincent
• Keleher Andrew P
• Leblanc Thomas Leonard

Classifications

• B64C1/1407 Primary

  Doors; surrounding frames · CPC title

• B64D11/00 Primary

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

• B64D11/0023

  Movable or removable cabin dividers, e.g. for class separation · CPC title

• B64D2011/0076

  for crew members, e.g. for sleeping during flight · CPC title