Since their market introduction in 1995, fiber Bragg gratings (FBGs) [wherein “fiber” signifies optical fiber] have emerged as excellent means of measuring such parameters as strain and temperature. Distributed-grating sensing is particularly beneficial for such structural-health monitoring applications such as those of “smart” structures or integrated vehicle health management in aerospace vehicles. Because of the variability of their output wavelengths, tunable lasers have become widely used as means of measuring FBGs.
Two other versions of the assembly can be characterized as follows:
- During the fabrication of one of the piezoelectric actuators, the optical fiber containing the Bragg grating(s) is embedded in the actuator in place of one of the piezoceramic fibers.
- The surface of an MFC actuator is roughened by sandblasting to improve subsequent bonding, then the optical fiber containing the Bragg grating(s) is bonded to the roughened surface by use of an adhesive.
In operation of any version of the assembly, when the optical fiber is strained by the actuator(s), the wavelength of light reflected from the Bragg grating(s) changes by an amount that depends on the amount of strain. This method of straining an optical fiber containing Bragg gratings to produce a shift in the reflected wavelength holds promise because it may also be useful for tuning an optical-fiber laser.
Bonding an FBG directly into an MFC actuator greatly reduces the complexity, relative to assemblies, of the type described in the immediately preceding article, that include piezoceramic fiber composite actuators, hinges, ferrules, and clamp blocks with setscrews. Unlike the curved actuators, MFC actuators are used in a flat configuration and are less bulky than are the assemblies described in the immediately preceding article. In addition, the MFC offers some vibration dampening and support for the optical fiber whereas, in an assembly of the type described in the immediately preceding article, the optical fiber is exposed, and there is nothing to keep the exposed portion from vibrating.
This work was done by Qamar A. Shams, Sidney G. Allison, and Robert L. Fox of Langley Research Center. LAR-17073-1