Hatch assembly for use in a vehicle and method of assembling the same

Patent metadata

Field	Value
Publication number	US-9592902-B2
Application number	US-201414182015-A
Country	US
Kind code	B2
Filing date	Feb 17, 2014
Priority date	Feb 17, 2014
Publication date	Mar 14, 2017
Grant date	Mar 14, 2017

Abstract

A hatch assembly for use in a vehicle is provided. The hatch assembly includes a hatch structure including an upper portion and a lower portion, an armrest support rail coupled to the hatch structure and defining a shade slot between the hatch structure and the armrest support rail, and a shade sized for insertion through the shade slot. The shade is configured to selectively translate between the upper portion and the lower portion of the hatch structure through the shade slot.

First claim

What is claimed is:

1. A hatch assembly for use in an aircraft, said hatch assembly comprising:
a hatch structure comprising an upper portion and a lower portion;
an armrest support rail coupled to said lower portion of said hatch structure and defining a shade slot between said hatch structure and said armrest support rail;
a lanyard attachment coupled to said armrest support rail and oriented within said lower portion of said hatch structure;
a shade sized for insertion through said shade slot, wherein said shade is configured to selectively translate between said upper portion and said lower portion of said hatch structure through said shade slot; and a shade sheath coupled to said hatch structure, said shade sheath oriented between said armrest support rail and said hatch structure, wherein said shade is slidably coupled to said shade sheath.

2. The assembly in accordance with claim 1 further comprising a sheath cover positioned about said shade sheath, wherein a first clearance configured to receive said shade therein is defined between said sheath cover and said shade sheath.

3. The assembly in accordance with claim 1 , further comprising a side wall panel coupled to said hatch structure, wherein said lanyard attachment is oriented between said side wall panel and said armrest support.

4. The assembly in accordance with claim 1 , wherein said lanyard attachment is coupled directly to said armrest support.

5. The assembly in accordance with claim 1 , wherein said armrest support rail comprises:
a body portion extending from a first end to a second end; and
at least one connection point extending from each of said first end and said second end for coupling to an outer peripheral portion of said hatch structure.

6. The assembly in accordance with claim 5 , wherein said body portion extends across said hatch structure such that a second clearance that allows said shade to selectively translate therethrough is defined between said body portion and an inner surface of said hatch structure.

7. An aircraft assembly comprising:
a fuselage; and
an over-wing hatch assembly coupled to said fuselage, wherein said over-wing hatch assembly comprises:
a hatch structure comprising an upper portion and a lower portion;
an armrest support rail coupled to said lower portion of said hatch structure and defining a shade slot between said hatch structure and said armrest support rail;
a lanyard attachment coupled to said armrest support rail and oriented within said lower portion of said hatch structure;
a shade sized for insertion through said shade slot, wherein said shade is configured to selectively translate between said upper portion and said lower portion of said hatch structure through said shade slot; and a shade sheath coupled to said hatch structure, said shade sheath oriented between said armrest support rail and said hatch structure, wherein said shade is slidably coupled to said shade sheath.

8. The assembly in accordance with claim 7 further comprising a sheath cover positioned about said shade sheath, wherein a first clearance configured to receive said shade therein is defined between said sheath cover and said shade sheath.

9. The assembly in accordance with claim 7 , further comprising a side wall panel coupled to said hatch structure, wherein said lanyard attachment is oriented between said side wall panel and said armrest support.

10. The assembly in accordance with claim 9 , wherein said lanyard attachment is coupled directly to said armrest support.

11. The assembly in accordance with claim 7 , wherein said armrest support rail comprises:
a body portion extending from a first end to a second end; and
at least one connection point extending from each of said first end and said second end for coupling to an outer peripheral portion of said hatch structure.

12. The assembly in accordance with claim 11 , wherein said body portion extends across said hatch structure such that a second clearance that allows said shade to selectively translate therethrough is defined between said body portion and an inner surface of said hatch structure.

13. A method of assembling an over-wing hatch assembly for use in an aircraft, said method comprising:
coupling a hatch structure to the aircraft, wherein the hatch structure includes an upper portion and a lower portion,
coupling an armrest support rail to the lower portion of the hatch structure, wherein a shade slot is defined between the hatch structure and the armrest support rail;
coupling a lanyard attachment to the armrest support rail such that the lanyard attachment is oriented within the lower portion of the hatch structure;
coupling a shade with the shade slot, wherein the shade is configured to selectively translate between the upper portion and the lower portion of the hatch structure through the shade slot; and coupling a shade sheath to the hatch structure such that the shade sheath is oriented between the armrest support rail and the hatch structure; and slidably coupling the shade with the shade sheath.

14. The method in accordance with claim 13 further comprising positioning a sheath cover about the shade sheath, wherein a first clearance configured to receive the shade therein is defined between the sheath cover and the shade sheath.

15. The method in accordance with claim 13 , wherein coupling an armrest support rail to the hatch structure comprises coupling the armrest support rail to an outer peripheral portion of the hatch structure.

16. The method in accordance with claim 15 , wherein coupling the armrest support rail to the hatch structure comprises extending the armrest support rail across the hatch structure such that a second clearance that allows said shade to selectively translate therethrough is defined between said body portion and an inner surface of said hatch structure.

17. The method in accordance with claim 13 wherein coupling a lanyard attachment to the armrest support rail comprises coupling the lanyard attachment directly to the armrest support rail.

Assignees

• Boeing Co

Inventors

• Perkins Thomas
• Hinderer David J
• Ho Kalai Ben
• Tatum Jeremy Ryan Glaze

Classifications

• B64C1/1423 Primary

  Passenger doors · CPC title

• B64C1/1484

  Windows (B64C1/1492 takes precedence) · CPC title

• B64C1/1461 Primary

  Structures of doors or surrounding frames · CPC title

• B64D11/0646

  Seats characterised by special features of stationary arms, foot or head rests · CPC title