Stiffening system of tie rods for stiffening a structure comprising an actuator to deform a deformable linking element

Patent metadata

Field	Value
Publication number	US-11892348-B2
Application number	US-202217986662-A
Country	US
Kind code	B2
Filing date	Nov 14, 2022
Priority date	Nov 16, 2021
Publication date	Feb 6, 2024
Grant date	Feb 6, 2024

Abstract

A system for stiffening a structure has at least one pair of tie rods (3), each tie rod (3) of the pair of tie rods (3) having a first end (4) fastened to the structure (2) and a second end (5), and at least one device (6) for tensioning the tie rods (3) having a deformable linking element (7) fastened to the second end (5) of each tie rod (3) so as to connect the tie rods (3). An actuator (10) is configured to deform the linking element (7) so as to make it pass from an inactive configuration in which the tie rods (3) are in a first state of tension to an active configuration in which the tie rods (3) are in a second state of tension, different than the first state of tension.

First claim

The invention claimed is:

1. A stiffening system of tie rods for stiffening a structure, comprising:
at least one pair of tie rods, each tie rod of the pair of tie rods having a first end fastened to the structure and a second end,
at least one device for tensioning the tie rods, having:
a deformable linking element fastened to the second end of each tie rod so as to connect the tie rods,
an actuator configured to deform the linking element so as to make the linking element to pass from an inactive configuration in which the tie rods are in a first state of tension to an active configuration in which the tie rods are in a second state of tension, different than the first state of tension.

2. The stiffening system as claimed in claim 1 , wherein the second state of tension is a state of tensile loading of the tie rods.

3. The stiffening system as claimed in claim 2 , wherein the tensile load in the tie rods is greater in the second state of tension than in the first state of tension.

4. The stiffening system as claimed in claim 1 , wherein one of the tie rods of the pair of tie rods is fastened by its second end at a first fastening point of the linking element, and the other tie rod of the pair of tie rods is fastened by its second end at a second fastening point of the linking element.

5. The stiffening system as claimed in claim 4 , wherein the deformation of the linking element as it passes from the inactive configuration to the active configuration shortens the distance between the first and second fastening points of the linking element, this distance being measured along a straight line passing through the first and second fastening points of the linking element.

6. The stiffening system as claimed in claim 4 , wherein the linking element has a pair of arms, one of the arms having a proximal end connected to the center of the linking element and a distal end having the first fastening point, and the other arm having a proximal end connected to the center of the linking element and a distal end having the second fastening point.

7. The stiffening system as claimed in claim 6 , wherein the arms of the pair of arms of the linking element are aligned.

8. The stiffening system as claimed in claim 1 , wherein the actuator is configured to deform the linking element by tightening the linking element against the actuator.

9. The stiffening system as claimed in claim 1 , wherein the linking element extends in a first plane and is deformable in a second plane, perpendicular to the first plane.

10. The stiffening system as claimed in claim 1 , wherein each tie rod of the pair of tie rods extends in the same plane as the linking element or in a parallel plane.

11. The stiffening system as claimed in claim 1 , wherein the tie rods of the pair of tie rods are rigid.

12. The stiffening system as claimed in claim 1 , wherein the tie rods of the pair of tie rods lie in the continuation of one another.

13. The stiffening system as claimed in claim 1 , wherein the tie rods of the pair of tie rods are aligned.

14. The stiffening system as claimed in claim 1 , wherein the actuator has a tightening support and is configured to deform the linking element via tightening, preferably by screwing, the linking element in contact with the tightening support.

15. The stiffening system as claimed in claim 1 , which has at least two pairs of tie rods, the tie rods preferably being disposed in a star shape around the linking element.

16. The stiffening system as claimed in claim 15 , wherein the linking element has at least two pairs of arms, the arms preferably being disposed in a star shape around the center of the linking element.

17. The stiffening system as claimed in claim 1 , wherein the structure is a supporting structure, in particular a lattice structure.

18. A method for stiffening a structure with the aid of a stiffening system as defined in claim 1 , said method comprising the steps of:
applying a predetermined deformation force to the linking element with the aid of the actuator so as to deform the linking element in a controlled manner and thus to make it pass from an inactive configuration in which the tie rods are in a first state of tension to an active configuration in which the tie rods are in a second predetermined state of tension, different than the first state of tension.

19. A lattice structure comprising:
at least two longitudinal members extending parallel to one another along a main direction of extension,
a plurality of crossmembers distributed along the main direction of extension in order to connect the longitudinal members together,
a plurality of tie rods disposed so as to connect the adjacent crossmembers together, at least two adjacent crossmembers having, between one another, a stiffening system as claimed in claim 1 .

20. The lattice structure as claimed in claim 19 , wherein at least some crossmembers are movable in translation in both directions along the main direction of extension with respect to the longitudinal members and at least some crossmembers are fixed with respect to the longitudinal members.

21. A solar tracker comprising:
at least one lattice structure as claimed in claim 19 , in particular a lattice beam, extending longitudinally along a main direction of extension,
at least one table supported by the lattice structure, the table being equipped with at least one device for collecting solar energy, the table extending longitudinally along the main direction of extension,
at least two support arches that are rotatable about an axis of rotation extending along the main direction of extension, the arches being mounted on the lattice structure so as to drive the lattice structure in rotation about the axis of rotation of the arches.

22. A solar field having a plurality of solar trackers as claimed in claim 21 , wherein at least some solar trackers are preferably disposed parallel to one another, in particular along the North/South direction.

Assignees

• Nexans

Inventors

• Chartier Emilie
• Amar Jérémy
• Printemps Morgan
• Quevillier Ludovic
• Richard Aymeric
• Gillet Lucas
• Soulie Emile

Classifications

• G01J1/0403 Primary

  Mechanical elements; Supports for optical elements; Scanning arrangements · CPC title

• E04C3/08

  with apertured web, e.g. with a web consisting of bar-like components; Honeycomb girders (E04C3/10, E04C3/11 take precedence) · CPC title

• F16B7/0406

  for rods or tubes being coaxial (F16B7/10 takes precedence) · CPC title

• E04C2003/0495

  the truss elements being located in several non-parallel surfaces · CPC title

• G01J2001/4266

  for measuring solar light · CPC title