IP Library Granted Patent US 12,416,183
Granted Patent B2
US 12,416,183 · App. 18/473,849 · Granted Sep 16, 2025

Latch lock assembly with fault monitoring, and closure structure having such a latch lock assembly

Inventor: Mark Douglas (Newport, GB)
Assignee: Elevate Aircraft Seating LLC
E05B47/0002E05B41/00E05B63/0069E05B2047/0016E05B2047/0069
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Quick Facts
Patent No.
US 12,416,183
App. No.
18/473,849
Granted
Sep 16, 2025
Kind
B2
Abstract

A latch lock assembly to facilitate movement of a closure structure between a stowed position and an open position. The latch lock assembly includes fault detection and electro-mechanical monitoring of components of the latch lock assembly. In the event of a detected fault operating condition by the latch lock assembly, a manual override mechanism may be employed to enable a user to advance the closure structure from the stowed position to the open position.

Claims (59)

1. A latch lock assembly, comprising:

a housing;

a first latch member pivotably mounted to the housing and a second latch member pivotably mounted to the housing, each latch member for rotation between a latched operating state to maintain a base frame of a closure structure system in a stowed position and an unlatched operating state to initiate advancement of the base frame from the stowed position to an open position;

a first trigger member pivotably mounted to the housing and operable to cause rotation of the first latch member;

a second trigger member pivotably mounted to the housing and operable to cause rotation of the second latch member;

an actuator mechanism operable to cause rotation of the first trigger member and the second trigger member to cause rotation of both the first latch member and the second latch member to the unlatched operating state;

a fault detection assembly operable to detect a fault operating condition of at least one of the latch lock assembly and the base frame; and

a manual override mechanism to advance the base frame from the stowed position to the open position in response to the detected fault operating condition, the manual override mechanism operatively connected to the first trigger member and the second trigger member to actuate both the first trigger member and the second trigger member in response to the detected fault operating condition.

2. The latch lock assembly of claim 1 , wherein:

the first trigger member causes the rotation of the first latch member to the unlatched operating state; and

the second trigger member causes the rotation of the second latch member to the unlatched operating state.

3. The latch lock assembly of claim 2 , wherein the fault detection assembly comprises:

a first yoke member operatively connected to the first latch member and the first trigger member for rotation in response to the rotation of the first latch member and the first trigger member, and

a second yoke member operatively connected to the second latch member and the second trigger member for rotation in response to the rotation of the second latch member and the second trigger member.

4. The latch lock assembly of claim 3 , wherein the fault detection assembly comprises:

a first electric microswitch operable to detect of change of operating state of the latch lock assembly in response to engagement by the first yoke member, and

a second electric microswitch operable to detect of change of operating state of the latch lock assembly in response to engagement by the second yoke member.

5. The latch lock assembly of claim 4 , further comprising a control module having one or more processors and a non-transitory memory coupled to the one or more processors, the non-transitory memory including a set of instructions of computer-executable program code, which when executed by the one or more processors, cause the control module to:

monitor the first electric microswitch and the second electric microswitch, and

cause, in response to receipt of an electric signal from at least one of the first electric microswitch and the first electric microswitch that is indicative of the detected fault operating condition, display of at least a visual warning of the detected fault operating condition.

6. The latch lock assembly of claim 1 , wherein the base frame comprises a drawer.

7. The latch lock assembly of claim 1 , wherein the base frame comprises a bin.

8. The latch lock assembly of claim 1 , wherein the base frame comprises a door.

9. The latch lock assembly of claim 1 , wherein the first latch member and the second latch member are operable for rotation about a first pivot axis and the first trigger member and the second trigger member are operable for rotation about a second pivot axis.

10. The latch lock assembly of claim 1 , wherein when the closure structure system is in the stowed position, latch keep members extending from the base frame engage the first latch member and the second latch member.

11. The latch lock assembly of claim 10 , wherein when the closure structure system is in the open position, the latch keep members are disengaged from the first latch member and the second latch member.

12. A closure structure system, comprising:

a base frame moveable between a stowed position and an open position; and

a latch lock assembly including:

a housing;

a first latch member pivotably mounted to the housing and a second latch member pivotably mounted to the housing, each latch member for rotation between a latched operating state to maintain the base frame in a stowed position and an unlatched operating state to initiate the base frame advancing from the stowed position to an open position;

a first trigger member pivotably mounted to the housing and operable to cause rotation of the first latch member;

a second trigger member pivotably mounted to the housing and operable to cause rotation of the second latch member;

an actuator mechanism operable to cause rotation of the first trigger member and the second trigger member to cause rotation of both the first latch member and the second latch member to the unlatched operating state;

a fault detection assembly operable to detect a fault operating condition of at least one of the latch lock assembly and the base frame; and

a manual override mechanism to advance the base frame from the stowed position to the open position in response to the detected fault operating condition, the manual override mechanism operatively connected to the first trigger member and the second trigger member to actuate both the first trigger member and the second trigger member in response to the detected fault operating condition.

13. The closure structure system of claim 12 , wherein:

the first trigger member causes the rotation of the first latch member to the unlatched operating state; and

the second trigger member causes the rotation of the second latch member to the unlatched operating state.

14. The closure structure system of claim 13 , wherein the fault detection assembly comprises:

a first yoke member operatively connected to the first latch member and the first trigger member for rotation in response to the rotation of the first latch member and the first trigger member, and

a second yoke member operatively connected to the second latch member and the second trigger member for rotation in response to the rotation of the second latch member and the second trigger member.

15. The closure structure system of claim 14 , wherein the fault detection assembly comprises:

a first electric microswitch operable to detect of change of operating state of the latch lock assembly in response to being engaged by the first yoke member, and

a second electric microswitch operable to detect of change of operating state of the latch lock assembly in response to being engaged by the second yoke member.

16. The closure structure system of claim 15 , further comprising a control module having one or more processors and a non-transitory memory coupled to the one or more processors, the non-transitory memory including a set of instructions of computer-executable program code, which when executed by the one or more processors, cause the control module to:

monitor the first electric microswitch and the second electric microswitch, and

cause, in response to receipt of an electric signal from at least one of the first electric microswitch and the first electric microswitch that is indicative of a detected fault operating condition, display of at least a visual warning of the detected fault operating condition.

17. The closure structure system of claim 12 , wherein the base frame comprises a drawer.

18. The closure structure system of claim 12 , wherein the base frame comprises a bin.

19. The closure structure system of claim 12 , wherein the base frame comprises a door.

20. A latch lock assembly, comprising:

a housing;

a first latch member pivotably mounted to the housing for rotation about a first pivot axis;

a second latch member pivotably mounted to the housing for rotation about the first pivot axis, wherein each latch member rotates between a latched operating state to maintain a base frame of a closure structure system in a stowed position and an unlatched operating state to initiate advancement of the base frame from the stowed position to an open position;

a first trigger member pivotably mounted to the housing for rotation about a second pivot axis and operable to cause rotation of the first latch member to the unlatched operating state;

a second trigger member pivotably mounted to the housing for rotation about the second pivot axis and operable to cause rotation of the second latch member to the unlatched operating state;

an actuator mechanism operable to cause rotation of the first trigger member and the second trigger member about the first pivot axis; and

a manual override mechanism operatively connected to the first trigger member and the second trigger member such that in the event of a fault operating condition of the closure structure system, the manual override mechanism causes rotation of both the first trigger member and the second trigger member which causes rotation of the first latch member and the second latch member to the unlatched operating state in order to initiate advancement of the base frame from the stowed position to the open position.

Assignments (3)
CHANGE OF NAME Recorded Jul 2, 2025
From: ADIENT AEROSPACE, LLC
To: ELEVATE AIRCRAFT SEATING LLC
Reel/Frame 071786/0571 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE'S NAME AND ADDRESS PREVIOUSLY RECORDED AT REEL: 065040 FRAME: 0264. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT . Recorded Dec 29, 2023
From: DOUGLAS, MARK
To: ADIENT AEROSPACE, LLC
Reel/Frame 066130/0674 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 27, 2023
From: DOUGLAS, MARK
To: THE BOEING COMPANY
Reel/Frame 065040/0264 →
Continuity (1)
Related Publication 20250101771A1 · Mar 27, 2025
References Cited (3)
US 6135513A · Hamada · 2000 [cited by examiner]
US 20180171689A1 · Kalathil · 2018 [cited by examiner]
US 20180266159A1 · Bito · 2018 [cited by examiner]