Hold open j-track locking mechanism for cowling

Patent metadata

Field	Value
Publication number	US-10875657-B2
Application number	US-201715706366-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 that includes a cowling having a j-track mounted on the inwardly facing surface and a rod pivotally connected to a stationary part of the aircraft at a first end and moveable within the j-track at a second end, so that, when the cowling is opened, the second end moves to lock into the j-shaped portion and hold the cowling open. In various embodiments, the first end may be pivotally connected to the aircraft by a quick release pin, and the second end may be connected to the j-track by a torsion spring. In another embodiment of the present disclosure, the cowling is a bi-folding cowl having an upper portion and a lower portion, where the rod and the lower portion may include structures for retaining the lower portion in an opened position.

First claim

What is claimed is:

1. An aircraft hold-open assembly comprising:
a cowling on an aircraft having opposing inwardly-facing and outwardly-facing surfaces; a j-track having a j-shaped portion and a straight portion mounted on the inwardly-facing
surface of the cowling, wherein the j-shaped portion of the j-track is positioned towards an edge of the cowling closest to a top surface of the aircraft; and
a rod having a first end and a second end, wherein the first end is pivotally connected to a stationary part of the aircraft, and wherein the second end is connected to the j-track and, when the cowling is opened, moves into the j-shaped portion and locks the cowling open.

2. The aircraft hold-open assembly of claim 1 , wherein the first end is pivotally connected to the aircraft by a quick release pin.

3. The aircraft hold-open assembly of claim 1 , wherein the first end is pivotally connected to a firewall.

4. The aircraft hold-open assembly of claim 1 , wherein the second end is connected to the j-track by a torsion spring.

5. The aircraft hold-open assembly of claim 1 , wherein the cowling is a bi-folding cowl having an upper portion and a lower portion, and wherein the j-track is mounted on the inwardly-facing surface of the upper portion.

6. The aircraft hold-open assembly of claim 5 , wherein the rod further comprises: a structure for retaining the lower portion of the bi-folding cowl in an opened position.

7. The aircraft hold-open assembly of claim 5 , wherein the rod further comprises a first part of a mated structure and the lower portion of the cowling further comprises a second part of the mated structure, and wherein, when the cowling is open, the first part and second part are mated to retain the lower portion of the cowling in an opened position.

8. The aircraft hold-open assembly of claim 1 , wherein the aircraft is a rotorcraft.

9. An aircraft apparatus comprising:
a cowling on an aircraft, when closed, having a top edge positioned closer to a top surface of the aircraft, a bottom edge positioned closer to a bottom surface of the aircraft, and opposing inwardly-facing and outwardly-facing surfaces;
a j-track having a j-shaped portion and a straight portion mounted on an inwardly-facing surface of the cowling, wherein the j-shaped portion of the j-track is positioned towards the top edge of the cowling; and
a rod having a first end and a second end, wherein the first end is pivotally connected to a stationary part of an aircraft, and wherein the second end is connected to the j-track and, when the cowling is opened, moves into the j-shaped portion and locks the cowling open.

10. The aircraft apparatus of claim 9 , wherein the first end is pivotally connected to the aircraft by a quick release pin.

11. The aircraft apparatus of claim 9 , wherein the first end is pivotally connected to a firewall.

12. The aircraft apparatus of claim 9 , wherein the second end is connected to the j-track by a torsion spring.

13. The aircraft apparatus of claim 9 , wherein the cowling is a bi-folding cowl having an upper portion and a lower portion; wherein, when the cowling is in a closed position, the upper portion is positioned closer to the top side of the aircraft and the lower portion is positioned closer to the bottom side of the aircraft; and wherein the j-track is mounted on the inwardly-facing surface of the upper portion.

14. The aircraft apparatus of claim 13 , wherein the rod further comprises: a structure for retaining the lower portion of the bi-folding cowl in an opened position.

15. The aircraft apparatus of claim 13 , wherein the rod further comprises a first part of a mated structure and the lower portion of the cowling further comprises a second part of the mated structure; and wherein, when the cowling is open, the first part and second part are mated to retain the lower portion of the cowling in an opened position.

16. The aircraft apparatus of claim 9 , wherein the aircraft is a rotorcraft.

17. A rotorcraft, comprising:
a cowling, when closed, having a top edge positioned closer to a top side of the rotorcraft, a bottom edge positioned closer to a bottom side of the rotorcraft, and opposing inwardly facing and outwardly facing surfaces;
a j-track having a j-shaped portion and a straight portion mounted on an inwardly-facing surface of the cowling, wherein the j-shaped portion of the j-track is positioned towards the top edge of the cowling; and
a rod having a first end and a second end, wherein the first end is pivotally connected to a stationary part of the rotorcraft, and wherein the second end is connected to the j-track and, when the cowling is opened, moves into the j-shaped portion and locks the cowling open.

18. The rotorcraft of claim 17 , wherein the first end is pivotally connected to the rotorcraft by a quick release pin.

19. The rotorcraft of claim 17 , wherein the first end is pivotally connected to a firewall.

20. The rotorcraft of claim 17 , wherein the second end is connected to the j-track by a torsion spring.

21. The rotorcraft of claim 17 , wherein the cowling is a bi-folding cowl having an upper portion and a lower portion; wherein, when the cowling is in a closed position, the upper portion is positioned closer to the top side of the rotorcraft and the lower portion is positioned closer to the bottom side of the rotorcraft; and wherein the j-track is mounted on the inwardly-facing surface of the upper portion.

22. The rotorcraft of claim 21 , wherein the rod further comprises: a structure for retaining the lower portion of the bi-folding cowl in an opened position.

23. The rotorcraft of claim 21 , wherein the rod further comprises a first part of a mated structure and the lower portion of the cowling further comprises a second part of the mated structure, and wherein, when the cowling is open, the first part and second part are mated to retain the lower portion of the cowling in an opened position.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Scannell Brent
• Mast Thomas

Classifications

• B64D29/06

  Attaching of nacelles, fairings or cowlings · CPC title

• B64D29/08 Primary

  Inspection panels for power plants · CPC title

• B64C27/00

  Rotorcraft; Rotors peculiar thereto · CPC title

• B64C1/1446

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

• E06B3/483

  folding upwardly (E06B3/482 takes precedence) · CPC title