U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Composites for structural control

Patent 6048622 Issued on April 11, 2000. Estimated Expiration Date: Icon_subject February 9, 2019. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3885758

Airplane wing camber control
Patent #: 3930626
Issued on: 01/06/1976
Inventor: Croswell, Jr.

Wound piezoelectric polymer flexure devices
Patent #: 4330730
Issued on: 05/18/1982
Inventor: Kurz ,   et al.

Piezoelectric composite materials
Patent #: 4400642
Issued on: 08/23/1983
Inventor: Kiraly

Method of making electromechanical transducers using improved flexible composite piezoelectric material
Patent #: 4407054
Issued on: 10/04/1983
Inventor: Zipfel, Jr.

Method and apparatus using a piezoelectric film for active control of vibrations
Patent #: 4565940
Issued on: 01/21/1986
Inventor: Hubbard, Jr.

Transversely reinforced piezoelectric composites
Patent #: 4613784
Issued on: 09/23/1986
Inventor: Haun ,   et al.

Method and apparatus for active control of vibrations
Patent #: 4626730
Issued on: 12/02/1986
Inventor: Hubbard, Jr.

Method of making piezoelectric composites
Patent #: 4726099
Issued on: 02/23/1988
Inventor: Card ,   et al.

Embedded piezoelectric structure and control
Patent #: 4849668
Issued on: 07/18/1989
Inventor: Crawley ,   et al.

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Inventors

Application

No. 247249 filed on 02/09/1999

US Classes:

428/461, Next to addition polymer from unsaturated monomers310/357, Orientation of piezoelectric polarization310/358, Ceramic composition (e.g., barium titanate)428/689Metal-compound-containing layer

Examiners

Primary: Krynski, William
Assistant: Gray, J. M.

Attorney, Agent or Firm

Foreign Patent References

  • 9112953 WO 09/13/1991

International Classes

B32B 018/00
B32B 015/08

Abstract

Composites for actuating or sensing deformation. In embodiments, the composites have a series of flexible, elongated piezoelectric fibers arranged in a parallel array with adjacent fibers separated by relatively soft polymer. The piezoelectric fibers have a common poling direction transverse to their axial extension. The composite further includes flexible conductive material along the axial extension of the fibers for imposing or detecting an electric field.

Other References

  • Newnham, R.E. et al., "Connectivity and Piezoelectric-Pyroelectric Composites," Mat. Res. Bull., vol. 13, pp. 525-536, 1978
  • Skinner, D.P. et al., "Flexible Composite Transducers," Mat. Res. Bull., vol. 13, p. 599-607, 1978
  • Klicker, K.A. et al., "Composites of PZT and Epoxy for Hydrostatic Transducer Applications," Jnl. Of the Amer. Ceramic Soc., vol. 64, No. 1, pp. 5-9, Jan. 19, 1981
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  • Hagood, N.W. et al., "Development of Piezoelectric Fiber Composites for Structural Actuation," 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., pp. 1-15, Apr. 19-22, 1993
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  • Microelectronic Manufacturing and Testing Desk Manual, p. 158, 198
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