IP Library Granted Patent US 12,459,646
Granted Patent B2
US 12,459,646 · App. 18/334,227 · Granted Nov 4, 2025

Galley insert system

Inventors: Robert Jhon Smakman (Houten, NL); Frederik Adrian Stephan Panjer (Maarsbergen, NL)
Assignee: B/E AEROSPACE, INC.
B64D11/04
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,459,646
App. No.
18/334,227
Granted
Nov 4, 2025
Kind
B2
Abstract

A galley insert system for an aircraft galley comprises a galley support structure, a galley insert configured to be coupled to the support structure, and a latch mechanism for coupling the insert to the support structure, the latch mechanism configured to automatically engage to couple the insert to the support structure when the insert is moved into a latching position on the support structure, wherein the latch mechanism comprises a control mechanism configured to be actuated to disengage the latch mechanism.

Claims (29)

1 . A galley insert system for an aircraft galley, the system comprising:

a galley support structure;

a galley insert configured to be coupled to the galley support structure;

a latch mechanism for coupling the galley insert to the galley support structure, the latch mechanism configured to automatically engage to couple the galley insert to the galley support structure when the galley insert is moved into a latching position on the galley support structure,

wherein the latch mechanism comprises a control mechanism configured to be actuated to disengage the latch mechanism, and

wherein the latch mechanism comprises:

a first latch element; and

a second latch element;

wherein the first latch element is configured to engage with the second latch element to couple the galley insert to the galley support structure,

wherein the first latch element includes a flange with a first contact surface,

wherein the second latch element includes a hook with a second complementary contact surface, and

wherein a downward force from the first contact surface of the flange when exerted on the second complementary contact surface of the hook causes the hook to pivot about a pivot point against a bias force of a spring into a position to allow the flange to be lowered past a tip of the hook.

2 . The galley insert system of claim 1 , wherein the latch mechanism is configured to couple a base of the galley insert to the galley support structure, and wherein at least a portion of the control mechanism is positioned beside the galley insert, on a side or front surface of the galley insert, on top of the galley insert, or in front of the galley insert.

3 . The galley insert system of claim 1 , wherein the latching position comprises the first latch element being aligned with the second latch element.

4 . The galley insert system of claim 3 , wherein the first latch element is integrated with the galley insert and the second latch element is integrated with the galley support structure.

5 . The galley insert system of claim 3 , wherein at least one of the first latch element and the second latch element is movable between an engagement position and a disengaged position and is biased to the engagement position.

6 . The galley insert system of claim 3 , wherein the first latch element is configured to automatically move under gravity into engagement with the second latch element when the first latch element is aligned with the second latch element.

7 . The galley insert system of claim 3 , wherein the second latch element is movable between an engagement position and a disengaged position and is biased to the engagement position by a spring force, the second latch element configured to move from the engagement position to the disengaged position to receive and be aligned with the first latch element when the insert is moved into the latching position, and then revert to the engagement position under the spring force to retain the first latch element to engage the latch mechanism.

8 . The galley insert system of claim 7 , wherein the latch mechanism is configured such that, when the insert is moved into the latching position on the support structure, the first latch element moves the second latch element from the engagement position to the disengaged position.

9 . The galley insert system of claim 7 , wherein the control mechanism is configured to be actuated to move the second latch element against the spring force from the engagement position to the disengaged position to disengage the latch mechanism, the latch mechanism configured such that the first latch element is automatically released from the second latch element when the second latch element moves to the disengaged position.

10 . The galley insert system of claim 1 , wherein the insert is biased by the support structure from the latching position to an unlatched position for removal of the insert from the support structure such that, when the latch mechanism is disengaged, the support structure automatically moves the insert to the unlatched position.

11 . The galley insert system of claim 1 , wherein the latch mechanism comprises a retaining mechanism configured to selectively prevent the latch mechanism automatically engaging when the insert is in the latching position.

12 . The galley insert system of claim 1 , wherein the latch mechanism is a primary latch mechanism, and further comprising at least one secondary latch mechanism, wherein the at least one secondary latch mechanism is configured to be engaged after the primary latch mechanism has engaged, and wherein the at least one secondary latch mechanism is configured to automatically engage in response to a sensor signal indicating that the primary latch mechanism has engaged.

13 . A method of operating the galley insert system of claim 1 , the method comprising:

placing the galley insert on the galley support structure;

moving the galley insert into the latching position on the galley support structure; and

automatically engaging the latch mechanism to couple the galley insert to the galley support structure.

14 . The method of claim 13 , wherein moving the galley insert into the latching position on the galley support structure comprises aligning the first latch element with the second latch element such that the first latch element and second latch element automatically engage to couple the galley insert to the galley support structure, wherein the first latch element is integrated with the galley support structure and the second latch element is integrated with the galley insert.

15 . The method of claim 14 , wherein aligning the first latch element with the second latch element comprises moving the second latch element against a spring bias force.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 13, 2023
From: SMAKMAN, ROBERT JHON; PANJER, FREDERIK ADRIAN STEPHAN
To: KONINKLIJKE FABRIEK INVENTUM B.V.
Reel/Frame 063938/0283 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 13, 2023
From: KONINKLIJKE FABRIEK INVENTUM B.V.
To: B/E AEROSPACE, INC.
Reel/Frame 063938/0361 →
Priority Claims (1)
EP 22182059 · Jun 29, 2022 · regional
Continuity (1)
Related Publication 20240002055A1 · Jan 4, 2024
References Cited (19)
US 3912206A · Jong · 1975 [cited by applicant]
US 5236153A · Laconte · 1993 [cited by applicant]
US 6318672B1 · Traylor · 2001 [cited by applicant]
US 7954761B2 · Johnson et al. · 2011 [cited by applicant]
US 8322654B2 · Gomes et al. · 2012 [cited by applicant]
US 8776353B2 · Herzog · 2014 [cited by examiner]
US 8814087B2 · Koschberg · 2014 [cited by examiner]
US 9254919B2 · Schootstra et al. · 2016 [cited by applicant]
US 9802704B2 · Young · 2017 [cited by examiner]
US 10065748B2 · Forbes · 2018 [cited by applicant]
US 10137987B2 · Burd · 2018 [cited by examiner]
US 11021254B2 · Swanson et al. · 2021 [cited by applicant]
US 11235879B2 · Elshaw et al. · 2022 [cited by applicant]
US 11273915B2 · Rowe et al. · 2022 [cited by applicant]
US 20120217342A1 · Tan · 2012 [cited by examiner]
US 20130200123A1 · Orozco · 2013 [cited by examiner]
US 20190210730A1 · Riedel et al. · 2019 [cited by applicant]
DE 102007036449 · 2009 [cited by applicant]
European Patent Office, European Search Report dated Dec. 8, 2022 in Application No. 22182059.0. [cited by applicant]