Method for building large-dimension structures in space

Patent metadata

Field	Value
Publication number	US-11505340-B2
Application number	US-201816637473-A
Country	US
Kind code	B2
Filing date	Aug 7, 2018
Priority date	Aug 10, 2017
Publication date	Nov 22, 2022
Grant date	Nov 22, 2022

Abstract

A method for manufacturing in space a rigid structure having a lattice is disclosed. The method includes creating of at least two framework elements from a coil of metal strip or wire, and creating of the lattice by cold-connecting the framework elements.

First claim

The invention claimed is:

1. A method for manufacturing in space a rigid structure comprising a lattice, comprising implementing, in space, steps of:
creating a plurality of framework elements from a coil of metal strip or wire, the creation of each framework element comprising:
unwinding and extending a length of metal strip or wire from said coil,
cutting off said length of metal strip or wire, and

creating the lattice by cold-connecting the plurality of framework elements to one another.

2. The manufacturing method according to claim 1 , wherein the creation of each framework element further comprises folding the cut length of metal strip or wire in at least one fold orthogonal to the main direction of the cut length of metal strip or wire.

3. The manufacturing method according to claim 1 , wherein each framework element is created from a coil of metal strip, and the creation of each framework element further comprises folding the cut length of metal strip along a fold parallel to the main direction of said length in order to give it an L-shaped cross-section.

4. The manufacturing method according to claim 1 , wherein creating the lattice further comprises the cold-connecting framework elements to form a plurality of basic structural modules, and cold-connecting of basic structural modules so as to form the lattice.

5. The manufacturing method according to claim 1 , wherein the cold-connection is implemented by stapling, clinching, magnetic fastening, or cold welding by molecular adhesion.

6. The manufacturing method according to claim 1 , further comprising the attachment to the lattice of at least one functional tile from the group comprising:
an antenna reflector tile comprising a metal grid suitable for reflecting radiofrequency waves,
an optical reflector tile comprising an optical surface reflecting in the visible range,
a protective tile comprising a frame on which is stretched a single- or multi-layer insulation sheet, or
a screen tile comprising a dense surface with or without emissive surface treatment for protection against micrometeorites.

7. The manufacturing method according to claim 6 , wherein the attachment of a tile on the lattice is reversible and implemented by cold welding by molecular adhesion, magnetic attachment, or by means of a clip, double-sided adhesive, or hook-and-loop strips.

8. The manufacturing method according to claim 1 , wherein the material of the metal strip or wire is Invar, titanium, an aluminum-based alloy, or a carbon-based alloy.

9. A rigid structure comprising a lattice, the rigid structure being obtained by implementing the method according to claim 1 , comprising a lattice and at least one functional tile fixed to the lattice, wherein the structure further comprises a robot configured to manipulate the at least one functional tile in order to change the at least one functional tile or its orientation, the robot comprising a battery and/or one or more photovoltaic-powered sensors.

10. A machine for manufacturing a rigid structure in space, comprising:
a reel for dispensing a metal strip or wire,
a device suitable for unwinding a portion of strip or wire,
a tool for cutting the metal strip or wire, and
assembly equipment comprising at least one articulated arm suitable for cold-connecting two framework elements formed from metal strip or wire, and
a dimensional control member for verifying the dimensions of the structure during manufacturing,
the machine being suitable for implementing a method for manufacturing in space a rigid structure comprising a lattice, comprising:
creating at least two framework elements from a coil of metal strip or wire, and
creating the lattice by cold-connecting the framework elements.

11. The machine according to claim 10 , further comprising a remote communication interface suitable for receiving control instructions from the ground.

12. A satellite comprising a manufacturing machine according to claim 10 .

13. A method for controlling, from the ground, a machine for manufacturing a structure in space, wherein the machine comprises:
a reel for dispensing a metal strip or wire,
a device suitable for unwinding a portion of strip or wire,
a tool for cutting the metal strip or wire, and
assembly equipment comprising at least one articulated arm suitable for cold-connecting two framework elements formed from metal strip or wire, and
a dimensional control member for verifying the dimensions of the structure during manufacturing, and
a remote communication interface suitable for receiving control instructions from the ground,
the method comprising the sending to the machine of a sequence of instructions configured for implementing the method according to claim 1 .

Assignees

• Airbus Defence & Space Sas

Inventors

• Carponcin Delphine
• Figus Christophe

Classifications

• B64G4/00 Primary

  Tools specially adapted for use in space · CPC title

• B64G99/00

  Subject matter not provided for in other groups of this subclass · CPC title

• B21F1/008

  in 3D with means to rotate the wire about its axis · CPC title

• B64G1/222

  for deploying structures between a stowed and deployed state · CPC title

• B64G1/2225

  Rolling or unfurling (B64G1/2227 takes precedence) · CPC title