Transport and referencing carriage for wings of an aircraft

Patent metadata

Field	Value
Publication number	US-11345486-B2
Application number	US-201916699898-A
Country	US
Kind code	B2
Filing date	Dec 2, 2019
Priority date	Dec 4, 2018
Publication date	May 31, 2022
Grant date	May 31, 2022

Abstract

A transport carriage for wings that are secured together, wherein the transport carriage comprises a chassis mounted on wheels, cradles mounted on positioning cylinders, support cylinders that each have a support mounted on the stem of the support cylinder, a central support having a frame and, for each wing, a rotatable lateral cradle, wherein the frame is movable vertically, for each wing, a lifting system with a mast and an arm, wherein each arm is movable vertically on the mast between a low position and a high position, and for each arm, at least two bearing points for the wing. The use of different movable elements allows good loading of the wings and makes it easier to move the wings thus loaded.

First claim

The invention claimed is:

1. A transport carriage for wings of an aircraft, having a structure where the wings are secured together, the transport comprising:
a chassis mounted on pivotable wheels,
a front cradle and a rear cradle that are configured to come to bear under the structure of the aircraft,
for each cradle, a positioning cylinder, wherein the cradle is mounted on the positioning cylinder, wherein each cradle is positioned in a centered manner with respect to the chassis,

two front support cylinders and two rear support cylinders, each of which has a support that is mounted on the support cylinder and is configured to come to bear under the structure of the aircraft, wherein the two front support cylinders are positioned on either side of a center of the chassis and the two rear support cylinders are positioned on either side of the center of the chassis,
a central support having a frame and, for each wing, a lateral cradle configured to come to bear under the wing, wherein each lateral cradle is mounted on the frame to be freely rotatable about a cradle axis of rotation perpendicular to a longitudinal direction of the transport carriage, wherein the frame is mounted to be vertically movable with respect to the chassis between a retracted position and a lifted position,
the frame actuated from the retracted position to the lifted position and vice versa,
for each wing, a lifting system that comprises a mast and an arm, wherein the two arms are positioned on either side of the center of the chassis, wherein each arm is movable vertically in translation on the mast between a low position and a high position,
each arm actuated from the low position to the high position and vice versa,
for each arm, at least two bearing points, each of which is intended to come to bear under the corresponding wing during a movement of the arm to the high position, and

a control unit configured to control each positioning cylinder, each support cylinder, the frame, and each arm.

2. The transport carriage according to claim 1 , wherein each positioning cylinder is mounted on the chassis to be rotatable about a first axis of rotation and to be movable between a lying position and a raised position, wherein, in the raised position, each cradle is positioned in a centered manner with respect to the center of the chassis, and wherein, for each positioning cylinder, wherein the control unit controls actuation of said positioning cylinder from the lying position to the raised position and vice versa.

3. The transport carriage according to claim 1 , wherein each support cylinder is mounted on the chassis to be rotatable about a support cylinder axis of rotation and is movable between a lying position and a raised position, wherein, in the raised position, the two front support cylinders are positioned on either side of the center of the chassis and the two rear support cylinders are positioned on either side of the center of the chassis, and wherein, for each support cylinder, wherein the control unit controls actuation of said support cylinder from the lying position to the raised position and vice versa.

4. The transport carriage according to claim 1 ,
wherein each mast is mounted on the chassis to be rotatable about a mast axis of rotation between a lying position and a raised position,
wherein, in the raised position, the two arms are positioned on either side of the center of the chassis,
wherein, when the mast is in the raised position, each arm is movable vertically in translation on the mast between the low position and the high position, and
wherein, for each mast, wherein the control unit controls actuation of said mast from the lying position to the raised position and vice versa.

5. The transport carriage according to claim 1 , wherein each bearing point is mounted on the arm via a third compound sliding table, which allows, in the high position, the bearing point to be moved in two orthogonal and horizontal directions.

6. The transport carriage according to claim 5 , wherein each third compound sliding table is mounted on a lifting cylinder that is fastened to the arm and controlled by the control unit.

7. The transport carriage according to claim 1 , wherein each cradle is mounted on the positioning cylinder via a first compound sliding table, which allows the cradle to be moved in two orthogonal and horizontal directions.

8. The transport carriage according to claim 1 , wherein the support is mounted on the support cylinder via a second compound sliding table, which allows the support to be moved in two orthogonal and horizontal directions.

9. The transport carriage according to claim 1 , wherein the central support has an additional frame, which is shared by the two lateral cradles and which is mounted on the frame to be rotatable about the cradle axis of rotation, and wherein each lateral cradle is mounted on the additional frame to be rotatable.

Assignees

• Airbus Sas
• Airbus Operations Sas

Inventors

• Darbonville Nicolas
• Datas Jean-Marc
• Bouriquet Jacques
• Brindeau Jean-Mickael
• Guibert Patrick

Classifications

• B64F5/50 Primary

  Handling or transporting aircraft components · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B23P2700/01

  Aircraft parts · CPC title

• B64F5/00

  Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for · CPC title

• B64C3/00

  Wings (ornithopter wings B64C33/02) · CPC title