Embedded piezoelectric structure and control

• US 4,849,668 A
• Filed: 05/19/1987
• Issued: 07/18/1989
• Est. Priority Date: 05/19/1987
• Status: Expired due to Term

• Current Assignee: Massachusetts Institute of Technology
• Original Assignee: Massachusetts Institute of Technology
• Inventors: de Luis, Javier, Crawley, Edward F.
• Primary Examiner(s): BUDD, MARK OSBORNE
• Application Number:
  US07/051,945
• Time in Patent Office: 791 Days
• Field of Search: 310/328, 310/316, 310/317, 310/326, 310/330-332, 310/340, 310/338, 310/339
• US Class Current: 310/328
• CPC Class Codes: H10N 30/00 Piezoelectric or electrostrictive devices integrated devices or assemblies of multiple devices H10N39/00
• CPC Class Codes: H10N 30/88 Mounts; Supports; Enclosures; Casings
• CPC Class Codes: H10N 30/883 Additional insulation means preventing electrical, physical or chemical damage, e.g. protective coatings
• CPC Class Codes: Y10T 29/42 Piezoelectric device making

Abstract

A composite structural member includes multiple layers with one or more embedded piezoelectric elements. In a conductive member, an insulating sheath electrically isolates each piezoelectric element while mechanically coupling it to the surrounding layers, forming a unitary structure with substantially homogeneous mechanical properties. In a graphite fiber composite structure, the piezoelectric elements are fitted in recesses in one or more interior layers, and located away from strain nodes of the structural members. Preferably pairs of elements are placed on opposite sides of a node and are driven in opposing phases to induce displacement of the structure. In a preferred prototype structure Kapton film insulates the piezoelectric elements, maintaining its integrity during a high temperature, high pressure curing process. An acrylic cement secures the insulator to the elements. Systems according to the invention include vibration damping systems, and aerodynamic lift surfaces or RF reflective surfaces with high authority control. A tubular truss member with axial control characteristics is described.

Claims

1. A structure formed of plies of conductive composite material which is assembled and then hardened by curing at elevated temperature or pressure, such structure comprising an assembly of

plural plies of conductive composite structural material arranged to form a body of said structure, at least one ply including a coupling face,

a piezoelectric element incorporated within said body and having an electrically actuable surface bounded by said coupling face, and

a film formed of electrically insulative sheet material located between the electrically actuable surface of said element and the coupling face for electrically insulating the surface from the conductive composite, said film being cemented to said electrically actuable surface with a cement which hardens during the curing of said plies of composite structural material to provide a mechanical shear coupling for the transmission of shear forces between the piezoelectric element and the coupling face, whereby said cured assembly forms a conductive structure of substantially homogeneous mechanical properties with a piezoelectric element effectively coupled to apply strain to the coupling face without shorting.

2. A structure according to claim 1, wherein a pair of piezoelectric elements are located on opposing sides of a neutral axis within said structure.

3. A structure according to claim 2, further comprising at least one strain gauge attached to the structure for sensing strain therein.

4. A structure according to claim 3, further comprising control means in communication with said at least one strain gauge and with at least one embedded piezoelectric element for actuating a said piezoelectric element in response to sensed strain so as to control said composite structure.

5. A structure according to claim 4, wherein said control means includes means for actuating a said piezoelectric element to shift the stiffness or damping of said structure.

6. A structure according to claim 5, having a surface shaped as an aerodynamic lifting surface.

7. A structure according to claim 1, wherein said film is a polyimide.

8. A structure according to claim 1, wherein said member is an airfoil.

9. A structure according to claim 1, wherein said member is a structural support member.

10. A controllable composite structure according to claim 1, further comprising control means for applying an electrical control signal to said conductive means to produce said strain.

11. A structure according to claim 1, wherein said plies are arranged to form a tubular member having an interior surface at least a portion of which constitutes said coupling face, wherein said piezoelectric element is located within the tubular member, and said electrically actuable surface is a round surface mating with said coupling face and further comprising conductive means for actuating the piezoelectric element for controlling the structural member.