Temperature compensated spacer

Patent metadata

Field	Value
Publication number	US-12411305-B2
Application number	US-202218266864-A
Country	US
Kind code	B2
Filing date	Mar 20, 2022
Priority date	Jun 24, 2021
Publication date	Sep 9, 2025
Grant date	Sep 9, 2025

Abstract

A temperature compensated spacer includes first and second anchoring configurations for anchoring the spacer relative to first and second elements, and a frame providing a mechanical connection between the anchoring configurations. The frame has a polygonal opening with a first diagonal extending across the width of a gap between the elements and a second diagonal extending transversely to the first diagonal. A crossbar is associated with the polygonal opening so as to span the second diagonal. The frame and the crossbar are formed from materials having differing coefficients of thermal expansion. The crossbar is deployed so as to determine a length of the second diagonal such that variation in temperature causes deformation of the frame, thereby varying a length of the first diagonal.

First claim

What is claimed is:

1. A temperature compensated spacer for mounting a first element relative to a second element where a width of a gap between the first and second elements varies as a function of temperature, the spacer comprising:
(a) a first anchoring configuration for anchoring the spacer relative to the first element;
(b) a second anchoring configuration for anchoring the spacer relative to the second element;
(c) a frame providing a mechanical connection between said first and second anchoring configurations, said frame having a polygonal opening with a first diagonal extending across the width of the gap and a second diagonal extending transversely to said first diagonal; and
(d) a crossbar associated with said polygonal opening so as to span said second diagonal,

wherein said frame is formed from a first material having a first coefficient of thermal expansion and said crossbar is formed from a second material having a second coefficient of thermal expansion, said crossbar being associated with said second diagonal such that a length of said second diagonal is determined by a dimension of said crossbar, said first and second coefficients of thermal expansion differing such that variation in temperature causes deformation of said frame, thereby varying a length of said first diagonal according to an effective coefficient of thermal expansion greater than both said first and said second coefficients of thermal expansion.

2. The spacer of claim 1 , wherein said crossbar is wedged inside said second diagonal of said polygonal opening.

3. The spacer of claim 1 , wherein said first coefficient of thermal expansion is at least twice said second coefficient of thermal expansion.

4. The spacer of claim 1 , wherein said first coefficient of thermal expansion is at least 7 times greater than said second coefficient of thermal expansion.

5. The spacer of claim 1 , wherein said length of said first diagonal varies with temperature with an effective coefficient of thermal expansion in excess of 60×10 −6 per kelvin.

6. The spacer of claim 1 , wherein said first material is aluminum and wherein said second material is a ceramic material.

7. The spacer of claim 1 , wherein said polygonal opening is a substantially kite-shaped opening.

8. The spacer of claim 1 , wherein said polygonal opening is a substantially rhombic opening.

9. The spacer of claim 1 , wherein said frame comprises first and second corner regions at opposite ends of said second diagonal, a first pair of arms extending from said first and second corner regions, respectively, towards said first anchoring configuration and a second pair of arms extending from said first and second corner regions, respectively, towards said second anchoring configuration.

10. The spacer of claim 9 , wherein said first and second pairs of arms each have a thickness, corresponding to a smallest dimension of said arms, that is measured in a plane parallel to said first and second diagonals, and a width measured perpendicular to said plane that is at least 5 times greater than said thickness.

11. The spacer of claim 10 , wherein said first pair of arms is provided with torsion-resisting reinforcements.

12. The spacer of claim 1 , wherein at least one of said first and second anchoring configurations comprises a resilient member for resiliently engaging the first or second element.

13. The spacer of claim 12 , wherein said resilient member is attached to said frame via an attachment structure which includes flexible elements arranged to accommodate motion of said resilient member relative to said frame in a direction perpendicular to said first and second diagonals.

14. An assembly comprising:
(a) a circular optical element having an outer periphery;
(b) a support structure circumscribing said outer periphery and spaced from said outer periphery so as to define a gap around said circular optical element; and
(c) a plurality of the spacers of claim 1 deployed within said gap so as to suspend said circular optical element relative to said support structure.

Assignees

• Rafael Advanced Defense Systems Ltd

Inventors

• Lahav Oded
• Stoller Omer

Classifications

• F16B1/00

  Devices for securing together, or preventing relative movement between, constructional elements or machine parts · CPC title

• B81B3/0081

  Thermal properties · CPC title

• B32B7/027

  Thermal properties · CPC title

• G02B7/028

  with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation · CPC title

• G02B7/181 Primary

  with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation · CPC title