Tape-spring deployable hinge

• US 7,354,033 B1
• Filed: 08/01/2006
• Issued: 04/08/2008
• Est. Priority Date: 08/01/2006
• Status: Active Grant

• Current Assignee: The Government of United States As Represented By The Secretary of The Air Force
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Murphey, Thomas W, Pollard, Eric L
• Primary Examiner(s): SCHWARTZ, CHRISTOPHER P
• Application Number:
  US11/461,547
• Time in Patent Office: 616 Days
• Field of Search: 162/25, 521/08, 526/46, 526/532, 526/58, 267/47, 267/148, 267/149, 267/36.1, 267/158, 267/151, 267/160
• US Class Current: 267/160
• CPC Class Codes: B64G 1/222 for deploying structures between a stowed and deployed state
• CPC Class Codes: F16F 1/18 Leaf springs planar springs in general F16F1/027; "Belleville"-type springs with generally radial arms F16F1/324
• CPC Class Codes: F16F 2224/0258 Shape-memory metals, e.g. Ni-Ti alloys

Abstract

A tape-spring shaped, articulating member used in deployable structures having a resilient, compliant hinge region and rigid non-hinge regions, thereby enabling a smaller fold radius and greater packaging efficiency. The increased compliance in the hinge region may be obtained by using a more compliant material in the hinge region or reducing the cross-sectional area in the hinge region. The hinge region may be reinforced with integrated shape memory alloy features serving as folding mandrels, to enhance structural stiffness and strength performance of the hinge, and to exhibit authority over the rate and sequencing of strain release when deployed.

Claims

1. A tape spring-type deployable structure of elastic material having a generally prismatic cross-section when extended except in one or more integrated hinge regions located at desired locations along the tape spring-type structure'"'"'s length, said hinge region having a radius of curvature when bent, a hinge region longitudinal length of approximately pi times the radius of curvature of said hinge region when said tape spring structure is longitudinally folded pi radians at said desired hinge region, and a compliance metric in the hinge region that is greater than that of the non-hinge regions of said tape spring structure, whereby the stowed volume of said tape spring-type deployable structure when compressed is reduced while essentially maintaining the geometric stiffness when extended.

2. The tape spring-type structure of claim 1, wherein said greater compliance metric in the hinge region is produce by modifying the cross-sectional geometry of said tape spring-type structure in the hinge region by uniformly reducing the thickness of the hinge region.

3. The tape spring-type structure of claim 1, wherein said greater compliance metric in the hinge region is produce by modifying the cross-sectional geometry of said tape spring-type structure in the hinge region by reducing the thickness of the edges of the hinge region more than central area.

4. The tape spring-type structure of claim 1, wherein said greater compliance metric in the hinge region is produced by replacing the elastic material of said tape spring-type structure with a more compliant material in said hinge region.

5. The tape spring structure of claim 4, wherein the more compliant material is a viscoelastic material that is integrated into a reduced cross-sectional area hinge region, whereby authority over the rate of strain release from a folded hinge can be obtained.