Movable cargo support having vertically biased wheel members

Patent metadata

Field	Value
Publication number	US-12583587-B2
Application number	US-202318191210-A
Country	US
Kind code	B2
Filing date	Mar 28, 2023
Priority date	Mar 31, 2022
Publication date	Mar 24, 2026
Grant date	Mar 24, 2026

Abstract

A movable cargo support for an aircraft cargo hold or passenger cabin includes a base. The base has a bottom surface with support(s) to support the base member on a floor surface of the cargo hold or passenger cabin. The base has wheel assemblies, each wheel assembly having at least one wheel rotatable about a rotation axis and movably mounted on the base to pivot about a steering axis of the wheel assembly. The at least one wheel of each wheel assembly is movable between an extended position, in which the at least one wheel protrudes beyond the support plane, and a retracted position, in which the at least one wheel does not extend beyond the support plane. Each wheel assembly has a biasing member for biasing the at least one wheel towards the extended position.

First claim

The invention claimed is:

1 . A movable cargo support for being received in a cargo hold or passenger cabin of an aircraft, the movable cargo support comprising:
a base having:
a support surface configured to support one or more cargo elements attached to and/or supported on the support surface; and
a bottom surface, which is opposite the support surface and comprises one or more supports, which extend in a common support plane and are configured to support the base on a floor surface of the cargo hold or of the passenger cabin;
a plurality of wheel assemblies, each wheel assembly comprising a at least one wheel that is configured to rest on the floor surface of the cargo hold or of the passenger cabin and is rotatable about a rotation axis that is parallel to the support plane;
wherein the at least one wheel of each of the plurality of wheel assemblies is movably mounted on the base, such that:
the at least one wheel pivots about a steering axis of that wheel assembly, which steering axis extends perpendicularly to the support plane; and
the position of the at least one wheel parallel to the steering axis is configured to be altered between an extended position and a retracted position;
wherein, in the extended position, the at least one wheel protrudes beyond the support plane;
wherein, in the retracted position, the at least one wheel is retracted from the support plane towards the support surface, so that the at least one wheel does not extend beyond the support plane;
wherein each wheel assembly comprises a biasing member configured to bias the at least one wheel towards the extended position with a biasing force acting in a direction parallel to the steering axis; and
wherein the biasing member is configured such that the biasing force is higher than a maximum gravitational force which acts on the at least one wheel and forces the at least one wheel towards the retracted position when:
the at least one wheel is on the floor surface of the cargo hold or of the passenger cabin; and
one or more cargo elements, which have a maximum allowable weight for the cargo support, are on the support surface; and
wherein the biasing force exceeds the maximum gravitational force by at most 50%.

2 . The cargo support of claim 1 , wherein:
the biasing member is configured such that the biasing force exceeds the maximum gravitational force by at most 40%; and the biasing force acts on the at least one wheel and pushes the at least one wheel towards the retracted position when the at least one wheel is on the floor surface of the cargo hold or of the passenger cabin and one or more cargo elements having the maximum allowable weight of the one or more cargo elements for the cargo support, are on the support surface.

3 . The cargo support of claim 1 , wherein, in each wheel assembly, the steering axis and the rotation axis are arranged such that, when seen in the support plane, the rotation axis is spaced apart from the steering axis, such that the rotation axis does not intersect with the steering axis.

4 . The cargo support of claim 1 , wherein:
each wheel assembly comprises:
a mount fixedly supported on the base; and
a carrier assembly;
the carrier assembly is rotatably supported on the mount member about the steering axis of the wheel assembly; and the at least one wheel of the wheel assembly is rotatably supported about the rotation axis on the carrier assembly.

5 . The cargo support of claim 4 , wherein:
the carrier assembly comprises:
a carrier rotatably coupled to the mount about the steering axis; and
an arm;
a first end of the arm is pivotably connected to the carrier about a pivot axis, which is parallel to the rotational axis; a second end of the arm, which is member opposite the first end of the arm, carries the at least one wheel; and the biasing member is arranged between the carrier and the arm.

6 . The cargo support of claim 5 , wherein:
the at least one wheel comprises a first wheel and a second wheel; the first wheel and the second wheel are spaced apart from each other along the rotational axis and supported on a shaft; and the arm and/or the biasing member extends between the first wheel and the second wheel.

7 . The cargo support of claim 5 , wherein the biasing member comprises a gas spring that extends between the carrier and the arm.

8 . The cargo support of claim 5 , wherein:
the biasing member is formed as ring; wherein the ring extends in a plane perpendicular to the pivot axis; wherein the ring is arranged between the carrier and the arm; and the ring is supported on the arm at a point spaced apart from the pivot axis and on the carrier, such that, when the arm pivots towards the mount, the ring is elastically deformed.

9 . The cargo support of claim 8 , wherein:
when seen along the pivot axis, the cross section of the carrier has:
a coupling section, which extends perpendicularly to the steering axis and is rotatably coupled to the mount; and
an arm section, which extends away from the mount, a distal end of the arm section being spaced apart from the coupling section along the steering axis;
the first end of the arm is pivotably coupled to the distal end of the arm section; and the ring is supported on the coupling section.

10 . The cargo support of claim 8 , wherein:
the first end of the arm is coupled to the carrier by a bolt; wherein each of the wheel assemblies comprises a shaft, which is carried by the arm, at the second end of the arm; and wherein the ring is supported via the bolt and the shaft.

11 . The cargo support of claim 1 , wherein:
the biasing member is configured such that the biasing force exceeds the maximum gravitational force by at most 30%; and the biasing force acts on the at least one wheel and pushes the at least one wheel towards the retracted position when the at least one wheel is on the floor surface of the cargo hold or of the passenger cabin and one or more cargo elements having the maximum allowable weight of the one or more cargo elements for the cargo support, are on the support surface.

12 . The cargo support of claim 5 , wherein the biasing member comprises a helical spring that extends between the carrier and the arm.

13 . The cargo support of claim 5 , wherein:
the biasing member comprises a circular ring; wherein the circular ring extends in a plane perpendicular to the pivot axis; wherein the circular ring is arranged between the carrier and the arm; and the circular ring is supported on the arm at a point spaced apart from the pivot axis and on the carrier, such that, when the arm pivots towards the mount, the circular ring is elastically deformed.

14 . The cargo support of claim 13 , wherein:
when seen along the pivot axis, the cross section of the carrier has:
a coupling section, which extends perpendicularly to the steering axis and is rotatably coupled to the mount; and
an arm section, which extends away from the mount, a distal end of the arm section being spaced apart from the coupling section along the steering axis;
the first end of the arm is pivotably coupled to the distal end of the arm section; and the circular ring is supported on the coupling section.

15 . The cargo support of claim 13 , wherein:
the first end of the arm is coupled to the carrier by a bolt; each of the wheel assemblies comprises a shaft, which is carried by the arm, at the second end of the arm; and the circular ring is supported via the bolt and the shaft.

16 . The cargo support of claim 1 , wherein the at least one wheel is config

Assignees

• Airbus Operations Gmbh

Inventors

• Meiranke Dirk
• Schliwa Ralf
• Benthien Hermann
• Poppe Andreas

Classifications

• B64C1/20

  specially adapted for freight · CPC title

• B64D2009/006

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

• B64D9/003 Primary

  Devices for retaining pallets or freight containers · CPC title

• B64D9/00 Primary

  Equipment for handling freight; Equipment for facilitating passenger embarkation or the like · CPC title