Remotely-activated self-centering cable latch

Patent metadata

Field	Value
Publication number	US-10259559-B2
Application number	US-201514840188-A
Country	US
Kind code	B2
Filing date	Aug 31, 2015
Priority date	Aug 31, 2015
Publication date	Apr 16, 2019
Grant date	Apr 16, 2019

Abstract

A hidden latch system for an interior structure of an aircraft includes at least two engagement features coupled to an interior structure of an aircraft. Each of the at least two engagement features includes an engagement portion, an engagement rod, and a self-centering feature. The engagement portion is configured to engage and release the engagement rod, and the self-centering feature is configured to self-center the engagement rod in at least one direction. Further, the engagement portion is configured to release the engagement rod using a cable pull system.

First claim

We claim:

1. A hidden latch system for an interior structure of an aircraft, the hidden latch system comprising:
at least two engagement features coupled to an interior structure of an aircraft, wherein each of the at least two engagement features comprises:
an engagement portion;
an engagement rod; and
a self-centering feature, wherein the engagement portion comprises a latch that is configured to engage and release the engagement rod, wherein the self-centering feature is configured to self-center the engagement rod in at least one direction, and wherein the latch is configured to release the engagement rod using a cable pull system,

wherein the at least two engagement features comprise a first engagement feature and a second engagement feature,
wherein, for the first engagement feature, the self-centering feature comprises frustoconically shaped portions at ends of a rod of the engagement rod, wherein when the engagement rod is moved toward engagement with the engagement portion, the frustoconically shaped portions self-center the engagement rod during engagement to the engagement portion, positioning the engagement portion between the frustoconically shaped portions,
wherein, for the second engagement feature, the self-centering feature comprises a floating base that comprises at least one biasing member connected to a base of the engagement rod, wherein when the engagement rod is moved toward engagement with the engagement portion, the floating base allows the engagement rod to float relative to the engagement portion thereby self-centering the engagement rod with the engagement portion, wherein the engagement rod is a substantially straight rod,
wherein, for each of the at least two engagement features, the self-centering feature further comprises a cut-out in the engagement portion configured to receive the engagement rod, and wherein the cut-out comprises a slanted portion that self-centers the engagement rod when the engagement rod is moved toward engagement with the engagement portion.

2. The hidden latch system of claim 1 , wherein the interior structure comprises a ceiling panel.

3. The hidden latch system of claim 1 , wherein the engagement rod of the second engagement feature has a length greater than a width of the engagement portion.

4. The hidden latch system of claim 1 , wherein each of the at least two engagement features further comprises the floating base connected to (i) the engagement rod and (ii) the interior structure.

5. The hidden latch system of claim 4 , wherein the floating base is configured to allow movement of the interior structure, relative to the engagement rod.

6. The hidden latch system of claim 5 , wherein the floating base comprises at least one spring that allows the movement of the interior structure relative to the engagement portion in a given direction.

7. The hidden latch system of claim 1 , wherein the cable pull system comprises a cable coupled to the latch.

8. The hidden latch system of claim 7 , wherein the cable comprises a sheath-covered cable, and wherein a sheath of the sheath-covered cable is fixed at both a first end of the sheath and a second end of the sheath.

9. The hidden latch system of claim 7 , wherein the cable is routed from the engagement feature to a remote location at least one foot away from the engagement feature.

10. The hidden latch system of claim 1 , wherein each of the at least two engagement features further comprises a push button release.

11. A hidden latch for an interior structure of an aircraft, the hidden latch comprising:
an engagement feature coupled to an interior structure of an aircraft, wherein the engagement feature comprises:
an engagement portion;
an engagement rod; and
a self-centering feature, wherein the engagement portion comprises a latch that is configured to engage and release the engagement rod, wherein the self-centering feature is configured to self-center the engagement rod in at least one direction, and wherein the latch is configured to release the engagement rod using a cable pull system,
wherein the self-centering feature comprises a floating base that comprises at least one biasing member connected to a base of the engagement rod, wherein when the engagement rod is moved toward engagement with the engagement portion, the floating base allows the engagement rod to float relative to the engagement portion thereby self-centering the engagement rod with the engagement portion, wherein the engagement rod is a substantially straight rod.

12. The hidden latch of claim 11 ,
wherein the floating base is configured to allow movement, relative to the engagement feature, of the interior structure.

13. The hidden latch of claim 11 , wherein the cable pull system comprises a cable coupled to the latch.

14. The hidden latch system of claim 13 , wherein the cable comprises a sheath-covered cable.

15. The hidden latch system of claim 14 , wherein a sheath of the sheath-covered cable is fixed at both a first end of the sheath and a second end of the sheath.

16. The hidden latch system of claim 13 , wherein the cable is routed from the engagement feature to a remote location at least one foot away from the engagement feature.

17. The hidden latch system of claim 11 , wherein the interior structure comprises a ceiling panel.

18. The hidden latch system of claim 11 , wherein the floating base comprises at least one spring that allows the movement of the interior structure relative to the engagement portion in a given direction.

19. The hidden latch system of claim 11 , wherein the engagement feature further comprises a push button release.

20. The hidden latch system of claim 11 , wherein the engagement rod has a length greater than a width of the engagement portion.

Assignees

• Boeing Co

Inventors

• Terry Troy N
• Schoales Jasen P

Classifications

• E05B2015/027

  auto-adjustable · CPC title

• E05B53/005

  Bowden · CPC title

• E05B65/006

  for covers or panels (for manholes E02D29/1427; for holes enabling access to installations in buildings E04F19/08; for pressure vessels F16J13/00) · CPC title

• B64C1/1446 Primary

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

• E05B2015/023

  Keeper shape · CPC title