Sandwich structure having hinge assemblies for accommodating differential in-plane expansion of face sheets

Patent metadata

Field	Value
Publication number	US-10288008-B2
Application number	US-201615382603-A
Country	US
Kind code	B2
Filing date	Dec 17, 2016
Priority date	Mar 5, 2012
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

A sandwich structure includes a first skin and a second skin spaced apart from each other and interconnected by a hinge assembly including a first hinge member and a second hinge member. The first hinge member proximal end is coupled to the first skin. The second hinge member proximal end is coupled to the second skin. The first hinge member distal end is coupled to the second member distal end at a member joint. The hinge assembly: prevents movement of the first skin relative to the second skin in an in-plane longitudinal direction of the first skin, allows movement of the first skin relative to the second skin in an in-plane transverse direction of the first skin, and allows movement of the first skin relative to the second skin in an out-of-plane direction that is normal to the in-plane longitudinal direction and the in-plane transverse direction.

First claim

What is claimed is:

1. A sandwich structure, comprising:
a first skin and a second skin spaced apart from each other;
at least one hinge assembly joining the first skin to the second skin, the hinge assembly including:
a first hinge member having a proximal end coupled to the first skin at a first skin joint and allowing the first hinge member to pivot about the first skin joint; and
a second hinge member having a proximal end coupled to the second skin at a second skin joint and allowing the second hinge member to pivot about the second skin joint;
the first hinge member and the second hinge member each having a distal end, the distal end of the first hinge member coupled to the distal end of the second hinge member at a member joint located between the first skin and the second skin;
the hinge assembly:
preventing movement of the first skin relative to the second skin in an in-plane transverse direction of the first skin;
allowing movement of the first skin relative to the second skin in an in-plane longitudinal direction of the first skin that is perpendicular to the in-plane transverse direction of the first skin;
allowing movement of the first skin relative to the second skin in an out-of-plane direction that is perpendicular to both the in-plane longitudinal direction and the in-plane transverse direction; and
allowing movement of the first skin relative to the second skin along the out-of-plane direction independent of movement of the first skin relative to the second skin along the in-plane longitudinal direction; and
allowing movement of the first skin relative to the second skin along the out-of-plane direction in combination with movement of the first skin relative to the second skin along the in-plane longitudinal direction.

2. The sandwich structure of claim 1 , wherein:
the first skin joint defines a first axis;
the second skin joint defining a second axis;
the member joint defining a member axis; and
the first axis, the second axis, and the member axis being substantially parallel to each other.

3. The sandwich structure of claim 1 , wherein:
the first hinge member and the second hinge member are integral with each other such that the hinge assembly comprises a unitary hinge structure.

4. The sandwich structure of claim 1 , wherein:
the hinge assembly comprises two or more unitary hinge structures nested with each other.

5. The sandwich structure of claim 1 , wherein:
the first skin and the second skin are coupled together by a pair of hinge assemblies in back-to-back arrangement.

6. The sandwich structure of claim 1 , wherein:
a plurality of hinge assemblies are arranged in series joining the first skin to the second skin.

7. The sandwich structure of claim 1 , wherein:
the member joint is one of a rigid joint and a movable joint.

8. The sandwich structure of claim 1 , wherein:
at least one of the first and second hinge members is comprised of two bars forming a triangular subassembly;
each bar has a proximal end and a distal end;
the proximal ends of the bars are coupled to the corresponding first and second skins at the corresponding first and second skin joint; and
the distal end of the bars are coupled to each other at the member joint.

9. The sandwich structure of claim 8 , wherein:
the first and second hinge members are each comprised of two bars forming a triangular subassembly; and
the triangular subassemblies are coupled at the member joint resulting in the hinge assembly forming a pyramidal assembly.

10. The sandwich structure of claim 1 , wherein:
the first hinge member and the second hinge member are each configured as a shear panel; and
the proximal ends of the shear panels are one of rigidly coupled and hingedly coupled to respective ones of the first skin and second skin at the respective first skin joint and second skin joint; and
the distal ends of the shear panels are one of rigidly coupled and hingedly coupled to each other at the member joint.

11. The sandwich structure of claim 10 , wherein:
the shear panels each have a trapezoidal shape being wider at the proximal end than at the distal end.

12. The sandwich structure of claim 1 , wherein at least one of the first and second skins has at least one stiffener configured as one of:
a longitudinal stiffener oriented parallel to the longitudinal direction; and
a transverse stiffener oriented parallel to the transverse direction.

13. The sandwich structure of claim 1 , wherein:
the sandwich structure has a closed cross-section.

14. The sandwich structure of claim 1 , wherein:
the hinge members are each aligned with a deflection trajectory of the first skin as the first skin moves in an out-of-plane direction relative to the second skin.

15. The sandwich structure of claim 1 wherein the sandwich structure is at least one of the following:
an engine exhaust nozzle for a vehicle;
a thermal protection system for a vehicle; and
an attachment system for attaching a tank to a structure.

16. The sandwich structure of claim 15 , wherein:
the first skin is a tank wall of a pressurizable tank, the tank wall expanding and contracting in an in-plane circumferential direction in response to changes in internal pressure of the tank;
the second skin is a structure; and
the hinge assembly comprises a plurality of hinge assemblies coupling the tank wall to the structure.

17. The sandwich structure of claim 16 , wherein:
the in-plane transverse direction of the hinge assembly is a circumferential direction of the tank wall.

18. The sandwich structure of claim 15 , wherein:
the tank is a propellant tank; and
the structure is cylindrical wall of a launch vehicle.

19. A sandwich structure, comprising:
a first skin and a second skin spaced apart from each other;
a plurality of hinge assemblies joining the first skin to the second skin, each hinge assembly including:
a first hinge member having a proximal end coupled to the first skin at a first skin joint and allowing the first hinge member to pivot about the first skin joint; and
a second hinge member having a proximal end coupled to the second skin at a second skin joint and allowing the second hinge member to pivot about the second skin joint;
the first hinge member and the second hinge member each having a distal end, the distal end of the first hinge member coupled to the distal end of the second hinge member at a member joint located between the first skin and the second skin;
the plurality of hinge assemblies:
preventing movement of the first skin relative to the second skin in an in-plane transverse direction of the first skin;
allowing movement of the first skin relative to the second skin in an in-plane longitudinal direction of the first skin that is perpendicular to the in-plane transverse direction of the first skin;
allowing movement of the first skin relative to the second skin in an out-of-plane direction that is perpendicular to both the in-plane longitudinal direction and the in-plane transverse direction; and
allowing movement of the first skin relative to the second skin along the out-of-plane direction independent of movement of the first skin relative to the second skin along the in-plane longitudinal direction; and
allowing movement of the first skin relative to the second skin along the out-of-plane direction in combination with movement of the first skin relative to the second skin along the in-plane longitudinal direction.

20. The sandwich structure of claim 19 , wherein:
the sandwic

Assignees

• Boeing Co

Inventors

• Grip Robert E
• Brown John J

Classifications

• F02K1/002 Primary

  with means to modify the direction of thrust vector (F02K1/54 takes precedence; thrust vectoring of rockets F02K9/80) · CPC title

• F05D2250/40

  Movement of components · CPC title

• Y10T29/49229

  Prime mover or fluid pump making · CPC title

• B64C3/48

  by relatively-movable parts of wing structures · CPC title

• F04D29/441

  especially adapted for elastic fluid pumps · CPC title