Bi-folding engine cowl having a plurality of open positions to provide access

Patent metadata

Field	Value
Publication number	US-10875656-B2
Application number	US-201715706338-A
Country	US
Kind code	B2
Filing date	Sep 15, 2017
Priority date	Sep 15, 2017
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

In one embodiment of the present disclosure, there is provided an aircraft having a bi-folding cowl for providing full access to equipment without completely removing the cowl. The bi-folding cowl has an upper portion and a lower portion mechanically connected along the adjacent edges, where the upper and lower portions fold so that the inner surfaces face each other when opened. In another embodiment, the bi-folding cowl has at least three maintenance positions, including partially-opened, fully-opened, and fully-opened, lying flat on the surface of the aircraft.

First claim

What is claimed is:

1. An aircraft bi-folding engine cowl comprising:
an upper portion; and
a lower portion, wherein the upper portion and the lower portion are mechanically connected on adjacent edges; and
wherein the aircraft bi-folding engine cowl comprises three distinct open positions:
i. a first position, wherein the upper portion and lower portion are fully folded along an adjacent edge in a fully opened position;
ii. a second position, wherein the upper portion and the lower portion are partially folded along the adjacent side in a partially-opened position; and
iii. a third position, wherein the upper portion and lower portion are fully folded along the adjacent side and rotated to lay on a top surface of an aircraft.

2. The aircraft bi-folding engine cowl of claim 1 , wherein the aircraft bi-folding engine cowl is attached to a track to guide the opening of the aircraft bi-folding engine cowl to one or more of the three distinct open positions.

3. The aircraft bi-folding engine cowl of claim 1 , wherein the aircraft bi-folding engine cowl, when in the second position, is supported by a structure on a firewall.

4. The aircraft bi-folding engine cowl of claim 1 , wherein the aircraft bi-folding engine cowl, when in the second position, is supported by one or more of: a hold open rod assembly, a quick release pin assembly, and a strut channel assembly.

5. An apparatus, comprising:
a bi-folding cowl on an aircraft access opening, the bi-folding cowl comprising:
an upper portion; and
a lower portion, wherein the upper portion and the lower portion are mechanically connected on adjacent sides, and
wherein the bi-folding cowl comprises three distinct open positions:
i. a first position, wherein the upper portion and lower portion are folded along an adjacent side in a fully-opened position;
ii. a second position, wherein the upper portion and the lower portion are partially folded along the adjacent side in a partially-opened position; and
iii. a third position, wherein the upper portion and lower portion are fully folded along the adjacent side and rotated to lay on a surface above the aircraft access opening.

6. The apparatus of claim 5 , wherein the bi-folding cowl is attached to a track to guide the opening of the bi-folding cowl to one or more of the three distinct open positions.

7. The apparatus of claim 6 , wherein the bi-folding cowl, when in the second position, is supported by a structure on the track.

8. The apparatus of claim 5 , wherein the bi-folding cowl, when in the second position, is supported by one or more of: a hold open rod assembly, a quick release pin assembly, and a strut channel assembly.

9. A rotorcraft, comprising:
an equipment access opening having a bi-folding cowl, the bi-folding cowl comprising:
an upper portion; and
a lower portion, wherein the upper portion and the lower portion are mechanically connected on adjacent sides; and
wherein the bi-folding cowl comprises three distinct open positions:
i. a first position, wherein the upper portion and lower portion are folded along an adjacent side in a fully-opened position;
ii. a second position, wherein the upper portion and the lower portion are partially folded along the adjacent side in a partially-opened position; and
iii. a third position, wherein the upper portion and lower portion are fully folded along the adjacent side and rotated to lay on a top surface of the rotorcraft.

10. The rotorcraft of claim 9 , wherein the bi-folding cowl is attached to a track to guide the opening of the bi-folding cowl to one or more of the three distinct open positions.

11. The rotorcraft of claim 9 , wherein the bi-folding cowl, when in the second position, is supported by a structure on a firewall.

12. The rotorcraft of claim 9 , wherein the bi-folding cowl, when in the second position, is supported by one or more of: a hold open rod assembly, a quick release pin assembly, and a strut channel assembly.

13. An aircraft bi-folding cowl comprising:
an upper portion having an inner surface and an opposing outer surface, wherein the upper portion is positioned closer to a top side of an aircraft when the aircraft bi-folding cowl is in a closed position;
a lower portion having an inner surface and an opposing outer surface, wherein the lower portion is positioned closer to a bottom side of the aircraft when the aircraft bi-folding cowl is in the closed position;
wherein the upper portion and the lower portion are pivotally connected on an adjacent side; and wherein the aircraft bi-folding cowl comprises three distinct open positions:
i. a first position, wherein the inner surface of the upper portion and the inner surface of the lower portion face each other;
ii. a second position, wherein the upper portion and the lower portion are partially folded along the adjacent side; and
iii. a third position, wherein the inner surface of the upper portion and the inner surface of the lower portion face each other and the outer surface of the upper portion lays on a top surface of the aircraft.

14. The aircraft bi-folding cowl of claim 13 , wherein the aircraft bi-folding cowl is attached to a track to guide the opening of the aircraft bi-folding cowl to one or more of the three distinct open positions.

15. The aircraft bi-folding cowl of claim 13 , wherein the aircraft bi-folding cowl, when in the second position, is supported by a structure on a firewall.

16. The aircraft bi-folding cowl of claim 13 , wherein the aircraft bi-folding cowl, when in the second position, is supported by one or more of: a hold open rod assembly, a quick release pin assembly, and a strut channel assembly.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Scannell Brent
• Mast Thomas

Classifications

• B64D29/06

  Attaching of nacelles, fairings or cowlings · CPC title

• B64C27/00

  Rotorcraft; Rotors peculiar thereto · CPC title

• B64D29/08 Primary

  Inspection panels for power plants · CPC title

• B64C1/1446

  Inspection hatches (for engine cowls B64D29/08) · CPC title