Page 57 - MEMS and Microstructures in Aerospace Applications
P. 57

Osiander / MEMS and microstructures in Aerospace applications DK3181_c003 Final Proof page 47  1.9.2005 8:59pm




                    MEMS Fabrication                                                 47


                    Howe and Muller 18  provided a basic definition of polycrystalline silicon surface
                    micromachining, and Fan et al. 19  illustrated an array of mechanical elements such
                    as fixed-axle pin joints, self-constraining pin joints, and sliding elements. Pister
                    et al. 20  demonstrated the design for microfabricated hinges, which enable the
                    erection of optical mirror elements.
                       Surface micromachining is a fabrication technology based upon the deposition,
                    patterning, and etching of a stack of materials upon a substrate. The materials
                    consist of alternating layers of a structural material and a sacrificial material. The
                    sacrificial material is removed at the end of the fabrication process via a release
                    etch, which yields an assembled mechanical structure or mechanism. Figure 3.9
                    illustrates the fabrication sequence for a cantilever beam fabrication in a surface
                    micromachine process that has two structural layers and one sacrificial layer.
                       Surface micromachining uses the planar fabrication methods common to the
                    microelectronics industry. The tools for depositing alternating layers of structural
                    and sacrificial materials, photolithographical patterning, and etching the layers have
                    their roots in the microelectronics industry. Etches of the structural layers define the
                    shape of the mechanical structure, while the etching of the sacrificial layers define
                    the anchors of the structure to the substrate and between structural layers. Depos-
                    ition of a low-stress structural layer is a key goal in a surface micromachine process.
                    From a device-design standpoint, it is preferable to have a slightly tensile average
                    residual stress with minimal or zero residual stress gradient, which eliminates the
                    design consideration of structural buckling. The stress in a thin film is a function of
                    the deposition conditions such as temperature. A postdeposition anneal is frequently
                    used to reduce the layer stress levels. For polysilicon the anneal step can require
                    several hours at 11008C.


                                                                            Patterned first
                    Patterned first                                         structural layer
                    sacrificial layer


                    Substrate and
                    isolation layers















                    FIGURE 3.9 Surface micromachined cantilever beam with underlying electrodes showing
                    the effect of topography induced by conformal layers.




                    © 2006 by Taylor & Francis Group, LLC
   52   53   54   55   56   57   58   59   60   61   62