CONFORMING TUNING COUPLER FOR FLEXTENSIONAL TRANSDUCERS
Assignee
US Government
Filed as: UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Filed
Jan 7, 1993
Granted
Nov 8, 1994
Location
San Diego CA (SAIC/General Dynamics)
Abstract
A flextensional transducer includes a stack of driving elements disposed ng a linear axis to convert a driving power into vibrational energy. End pieces, disposed at each end of the stack, have outwardly facing arcuate surfaces. A flexural shell, formed into a loop, is disposed to circumscribe the stack and the end pieces to present an elliptical cross-section with the major axis thereof being generally coincident with the stack's linear axis. The shell is reactively coupled to the end pieces at the outwardly facing arcuate surfaces. A pliant assembly is positioned between each end piece and the flexural shell for maintaining conformal engagement between portions of the end pieces and the flexural shell. The pliant assembly is designer such that its stiffness may be adjusted.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 11, 1993
Rescinded
May 17, 1993
Duration
2 months
Inventor
- 1JOHN D. MALTBY
Sensitive facility: San Diego CA (SAIC/General Dynamics)
Record Details
- Patent number
- US 5363346
- Application
- 08001438
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
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