Latches for cargo hold loading and storage system and associated methods

US12049327B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12049327-B2
Application numberUS-202117361934-A
CountryUS
Kind codeB2
Filing dateJun 29, 2021
Priority dateDec 31, 2018
Publication dateJul 30, 2024
Grant dateJul 30, 2024

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In an aircraft, latches are used to secure cargo within the cargo hold of the aircraft. Such latches include a base plate configured for rigid attachment to a surface of the cargo hold, a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a Y-direction and a Z-direction and to allow a movement of the at least one cargo unit in an X-direction, and a roller assembly attached to the base plate, opposite the latch head, and comprising at least one roller, the roller being configured to provide a vertical support to the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction.

First claim

Opening claim text (preview).

The invention claimed is: 1. A latch for a cargo management system of a cargo hold, the latch comprising: a base plate configured for rigid attachment to a surface of the cargo hold; a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a Y-direction and a Z-direction and to allow a movement of the at least one cargo unit in an X-direction; and a roller assembly attached to the base plate, opposite the latch head, and comprising at least one roller, the at least one roller being configured to provide a vertical support to the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction; wherein the base plate comprises, formed therein, a latch head slot and a roller assembly slot; wherein the latch head is configured to engage within the latch head slot via a pivoting movement of the latch head; and wherein the roller assembly is configured to engage within the roller assembly slot by a pivoting movement of the roller assembly. 2. The latch of claim 1 , wherein the at least one cargo unit is at least one unit load device (ULD). 3. The latch of claim 1 , wherein; the latch head comprises a latch toe that is formed on an edge of the latch head about which the latch head pivots during the pivoting movement of the latch head; the base plate comprises, formed at an edge of the latch head slot, a base-latch heel; and the latch toe is configured to engage against the base-latch heel to secure the latch head within the latch head slot. 4. The latch of claim 3 , wherein: the base plate and the latch head comprise corresponding latch-base alignment features, including a protuberance on the base plate and a cavity formed in a bottom surface of the latch head; when the latch toe is engaged against the base-latch heel, the latch head is configured to pivotably rotate, according to the pivoting movement of the latch head, into an installed position; and in the installed position, the protuberance is located within the cavity. 5. The latch of claim 4 , wherein; the protuberance comprises a first through-hole formed through a thickness of the protuberance; the latch head comprises a second through-hole formed through a thickness of the latch head; the first and second through-holes are substantially coaxial to each other when the protuberance is located within the cavity, in the installed position; and a pull pin is configured for removable insertion through the first and second through-holes to rigidly attach the latch head to the base plate in the installed position. 6. The latch of claim 1 , wherein: the roller assembly comprises a frame having a roller toe that is formed on an edge of the roller assembly about which the roller assembly pivots during the pivoting movement of the roller assembly; the base place comprises, formed at an edge of the roller assembly slot, a base-roller heel; and the roller toe is configured to engage against the base-roller heel to secure the roller assembly within the roller assembly slot. 7. The latch of claim 6 , wherein: the base plate and the roller assembly comprise corresponding roller-base alignment features, including a rib on the base plate and a recess formed in a bottom surface of the roller assembly; when the roller toe is engaged against the base-roller heel, the roller assembly is configured to pivotably rotate, according to the pivoting movement of the roller assembly, into an installed position; and in the installed position, the rib is located within the recess. 8. The latch of claim 7 , wherein: the roller-base alignment features further comprise; at least two slots formed in opposite sides, in the X-direction, of the base plate; and at least two lateral tabs attached to the roller assembly; each lateral tab of the at least two lateral tabs is configured to engage within a corresponding slot of the at least two slots when the roller assembly is in the installed position. 9. The latch of claim 8 , wherein, when the roller assembly is only partially engaged over the base plate, the at least two lateral tabs protrude from the roller base in the X-direction as a visual indicator of the partial engagement of the roller assembly over the base plate. 10. The latch of claim 8 , wherein the at least two slots comprise a keyed portion with which the corresponding lateral tabs engage to provide a retention force to prevent, along with the engagement of the roller toe with the base-roller toe, separation of the roller assembly from the base plate in the Y-direction and/or the Z-direction. 11. The latch of claim 7 , wherein the roller-base alignment features are configured to prevent relative movement between the base plate and the roller assembly in the X-direction. 12. A method of installing a latch in a cargo management system in a cargo hold, the method comprising: attaching a base plate to a surface of the cargo hold, wherein the base plate comprises, formed therein, a latch head slot and a roller assembly slot; attaching a latch head to the base plate, wherein the latch head prevents a movement of at least one cargo unit in a Y-direction and a Z-direction and to allow a movement of the at least one cargo unit in an X-direction; and attaching a roller assembly to the base plate opposite the latch head, wherein the roller assembly comprises at least one roller, the at least one roller vertically supporting the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction; wherein the latch head engages within the latch head slot via a pivoting movement of the latch head; and wherein the roller assembly engages within the roller assembly slot by a pivoting movement of the roller assembly. 13. The method of claim 12 , wherein: the latch head comprises a latch toe that is formed on an edge of the latch head about which the latch head pivots during the pivoting movement of the latch head; the base plate comprises, formed at an edge of the latch head slot, a base-latch heel; and attaching the latch head to the base plate comprises: engaging the latch toe against the base-latch heel; pivotably rotating the latch head against the base plate into an installed position, according to the pivoting movement of the latch head, such that a protuberance extending from the base plate towards and/or within a cavity of the latch head is covered; and inserting a pull pin through a first through-hole, which is formed through the protuberance, and a second through-hole, which is formed through the latch head, when the latch head is in the installed position, such that the latch head is rigidly attached to the base plate; wherein, in the installed position, the first and second through-holes are substantially coaxial to each other. 14. The method of claim 13 , wherein pivotably rotating the latch head against the base plate into the installed position prevents a movement of the latch head relative to the base plate in the X-direction and the Y-direction. 15. The method of claim 12 , wherein: the roller assembly comprises a frame having a roller toe that is formed on an edge of the roller assembly about which the roller assembly pivots during the pivoting movement of the roller assembly; the base place comprises, formed at an edge of the roller assembly slot, a base-roller heel; and attaching the roller assembly to the base plate comprises: engaging the roller toe against the base-roller heel; and pivotably rotating the roller assembly against the base plate into an installed positi

Assignees

Inventors

Classifications

  • specially adapted for freight · CPC title

  • Rollers or drives for pallets of freight containers, e.g. PDU · CPC title

  • Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

  • B64D9/003Primary

    Devices for retaining pallets or freight containers · CPC title

Patent family

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External sources

Frequently asked questions

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What does patent US12049327B2 cover?
In an aircraft, latches are used to secure cargo within the cargo hold of the aircraft. Such latches include a base plate configured for rigid attachment to a surface of the cargo hold, a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a Y-direction and a Z-direction and to allow a movement of the at least one cargo unit in an X-direction…
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B64D9/003. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 30 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).