Method to control residual stress in a film structure and a system thereof

A method for controlling residual stress in a structure in a MEMS device and a structure thereof includes selecting a total thickness and an overall equivalent stress for the structure. A thickness for each of at least one set of alternating first and second layers is determined to control an internal stress with respect to a neutral axis for each of the at least alternating first and second layers and to form the structure based on the selected total thickness and the selected overall equivalent stress. Each of the at least alternating first and second layers is deposited to the determined thickness for each of the at least alternating first and second layers to form the structure.

FIELD OF THE INVENTION

The present invention generally relates to film structures in micro-electrical-mechanical systems (MEMS) and, more particularly, to a method to control residual stress and enhance overall material properties in a film structure for a MEMS device and a system thereof.

BACKGROUND

Since thin-film fabrication techniques were first used to produce MEMS devices, one of the areas that has seen significant research is the reduction of film stresses and stress gradients. A result of thin-film processes is that out-of-plane deformation of freestanding micro machined films could negatively impact the performance of MEMS devices. The principal source of contour errors in micro machined structures is residual strain that results from thin-film fabrication and structural release. Surface micro machined films are deposited at temperatures that are sometimes significantly above ambient, which create the stresses due to the difference in the coefficient of thermal expansion between different material types when the substrate is cooled.

This residual stress for the material that is added to the substrate is usually tensile. Simply supported structures results in an Euler's type of eccentric loading, which causes suspended beams to deflect downward into the area where the sacrificial material had been removed. One example of this is illustrated inFIGS. 1A-1Bwhere a beam12is deposited on a sacrificial material10and a substrate14. When the sacrificial material10has been removed from below the beam12, the beam12is supported at each end by a substrate14and is deflected downward into the trench16.

Another problem that occurs from residual stresses in beam12occurs when releasing the beam12. If the stresses are high enough, beam12collapses downward and impedes the removal process of the sacrificial material10. This increases the amount of time that is required in the etching process. The increase in processing time impacts the process throughput and slows down production. It also requires a higher selectivity for the enchants in order for the sacrificial material10to be removed without etching into the rest of the device.

Existing technologies used to reduce the effects of residual stresses have been in the areas of ion bombardment to soften the material as disclosed in R. Nowack et al, “Post—deposition reduction of internal stress in thin films: the case of HfN coatings bombarded with Au ions”,Mater. Lett. Vol, 33, no. 1-2, pp 31-36, 1997, which is herein incorporated by reference in its entirety, and device design to account for the deformations that occur due to the residual stresses as disclosed in F. Yuan et al, “Using thin films to produce precision, figured x-ray optics”,Thin Solid Films, vol. 220, no. 1-2, pp 284-288, 1992, which is herein incorporated by reference in its entirety. Annealing the materials after processing is another method that has been commonly used to reduce residual stresses.

Unfortunately, there are problems with these existing technologies. For example, ion bombardment can damage the dielectric properties of the material and can alter the behavioral characteristics of the material. Annealing may relieve the stress of the layer, but may cause other stress in other layers through the heating and cooling. The annealing can change the properties of the material from amorphous to crystalline. If dopants are present in the material, the annealing may cause additional driving of the dopants within the material which may not be desirable.

SUMMARY

A method for controlling residual stress in a structure in a MEMS device in accordance with embodiments of the present invention includes selecting a total thickness and an overall equivalent stress for the structure. A thickness for each of at least one set of alternating first and second layers is determined to control an internal stress with respect to a neutral axis for each of the at least alternating first and second layers and to form the structure based on the selected total thickness and the selected overall equivalent stress. Each of the at least alternating first and second layers is deposited to the determined thickness for each of the at least alternating first and second layers to form the MEMS structure.

A structure in a MEMS device in accordance with embodiments of the present invention includes at least one first layer and at least one second layer on the first layer. A thickness for each of the at least one first and second layers is set to control an internal stress with respect to a neutral axis for each of the at least one first and second layers and the thickness for each of the at least one first and second layers are set to obtain an overall total thickness and an overall equivalent stress for the combined at least first and second layers

The present invention allows the fabrication of simply supported beams, cantilevered beams, or diaphragms for MEMS devices that will conform to the design intent for shape and control geometrics. The present invention allows a wider range of designs and final geometries that can be implemented and controlled in the MEMS and semiconductor fields. Additionally, the present invention can be used in the fabrication of semiconductor devices where residual stress between thin films can cause layer separation or creep, which tends to degrade the devices performance.

The present invention also helps reduce the amount of time needed to remove sacrificial layers for MEMS devices. This helps decrease process time and increases production rates. Further, the present invention reduces requirements for higher selectivity with the etchants that are used.

With the present invention, any combination of materials can be used for the fabrication of MEMS devices. There is no need to limit the selection of materials that can be used or to add secondary processes to overcome problems that are the result of residual stresses between thin films, such as annealing or ion bombardment.

DETAILED DESCRIPTION

A structure20in a MEMS device22with residual stress controlled and enhanced overall material properties in accordance with embodiments of the present invention is illustrated inFIGS. 2A-2B. The structure22includes layers of titanium24(1)-24(4) and layers of tungsten26(1)-26(3), although the structure10can comprise other numbers and types of layers in other configurations, such as having the same material deposited in different manners. The present invention provides a number of advantages including allowing the fabrication of structures, such as simply supported clamped, fixed, or pinned beams, which are attached at one end or both ends, or diaphragms for MEMS devices that will conform to the design intent for shape and control geometries.

Referring toFIG. 2A, the MEMS device22includes the structure20which extends across a trench30in a substrate28, although the MEMS device22can comprise other numbers and types of elements in other configurations. The opposing ends of the structure20which extends over the trench30are supported by the substrate28, although the structure22can have other configurations, such as having only one end of the structure22supported by the substrate28. Typically, a structure20in a MEMS device22will have a total thickness of less than at least about twenty microns.

The structure20includes alternating layers of tungsten24(1)-24(4) and layers of titanium26(1)-26(3), although the structure20can have other numbers and types of layers in other thicknesses and which are deposited in other manners. The layers of tungsten24(1)-24(4) are thicker than the layers of titanium26(1)-26(3), although each of the layers24(1)-24(4) and26(1)-26(3) could have other thicknesses. The structure20has a neutral or substantially zero equivalent stress to have a substantially straight or flat shape over the trench30in the substrate28, although the structure20could be designed to have other configurations, such as bowed upward or bowed downward configuration with respect to the trench30in the substrate28.

The number and thickness of the layers24(1)-24(4) and of the layers26(1)-26(3) is based on the selected or desired total thickness for the final structure20, the selected overall equivalent stress for the structure20, and the material or materials used for each of the layers24(1)-24(4) and26(1)-26(3). Residual stress control is accomplished by balancing the amount of each material used in each layer24(1)-24(4) and26(1)-26(3) to create offsetting stresses within and/or between the layers24(1)-24(4) and26(1)-26(3). Controlling the thickness of each of the layers24(1)-24(4) and26(1)-26(3) allows control of the layers24(1)-24(4) and26(1)-26(3) internal stress with respect to a neutral axis for each layer24(1)-24(4) and26(1)-26(3). This allows overall equivalent stress of the structure20suspended over the trench30in the substrate28to be controlled for the final geometry.

The build-up of internal stresses within each layer24(1)-24(4) and26(1)-26(3) also makes the structure20stronger. This means it will take greater external forces to overcome the internal stresses that exist inside the structure20and effectively results in a stronger structure20. Further, this build-up of internal stresses increases the effective Young's modulus of the structure20.

The type of stresses within and/or between the layers, such as between layers24(1)-24(4) and26(1)-26(3), will be described with reference to a simpler example shown in the graphs and diagrams inFIGS. 3A-3C. There is a relationship that creates thin film stresses at the interface where two layers of materials bond. These stresses are a direct result of the nucleation where the two layers of materials are joined. The nucleation forces are caused by the difference in the atomic spacing of different layers of materials. This difference induces a compressive force at the surface of the layer of material that is being added and a tensile force on the layer of material that was already present. As the layer of material that is being added becomes thicker, and homogenous, the internal forces on that thin film undergo a transition from a compressive stress to neutral stress and eventually to tensile stress, due to the difference between the coefficients of thermal expansion between the layer of material44being added and the substrate40, although the transition can take place in other sequences, such as from tensile stress to neutral stress to compressive stress. Accordingly, by controlling the stresses within each layer, the overall equivalent stress of the structure can be controlled to a have a desired geometry. Additionally, by controlling the geometry of the structure, in this example the layer44, the process of removing the sacrificial material42is simplified which decreases processing time impacts and increases throughput. Further, less selective and less expensive enchants for removing the sacrificial material42can be used.

By way of example only, a structure manufactured in accordance with the present invention which is ten microns wide and one hundred microns long and has a substantially zero equivalent stress can withstand much higher loading than a homogenous beam. This particular structure withstood direct application of compressed air and water spray with no visible damage. Additionally, this particular structure underwent bending stresses from a profilometer and recovered to its original form. Further, this particular structure has been deflected more than six microns downward into contact with the underlying substrate and returned to its original position, overcoming the van der Waals forces that occur when a micro device comes in contact with another device or surface, this is commonly referred to as stiction.

A method for making a structure which controls the residual stress in accordance with will the present invention will now be described with reference toFIGS. 2A-2B. First, the total thickness and overall equivalent stress for the final structure20are selected. Next, the material or materials for the layers in the structure20are selected for the behavioral characteristics that are desired for the structure20in the MEMS device22. The characteristics or requirements for the structure20in the device, include: (1) the correct thickness of each layer24(1)-24(4) and26(1)-26(3) is determined to position the neutral axis at the desired position and to regulate the internal stresses of the layers24(1)-24(4) and26(1)-26(3); (2) the proper ratio of thickness for each layer24(1)-24(4) and26(1)-26(3) is determined that will allow the individual stresses from each layer24(1)-24(4) and26(1)-26(3) to offset each other to provide the selected overall equivalent stress; and (3) the number of layers24(1)-24(4) and26(1)-26(3) in the structure20is determined by the selected total thickness that is needed by the structure20in the device22. More specifically, the materials for the layers in structure20are selected based on characteristics, such as the desired design intent, function, size, strength, residual frequency, response time, and electrical properties. The ratios of the thicknesses of the materials for each of the layers are based on factors, such as the properties of the selected materials and the desired overall equivalent stress for the structure20. The selected total thickness of the structure20controls the thickness of each of the layers24(1)-24(4) and26(1)-26(3). The deposition of a material can be used to control the properties of each of the layers, but unfortunately, during operation these deposition parameters can drift affecting the resulting properties of the layers. With the present invention as described herein, less precise control over the deposition techniques for each of the layers is required because the layers are deposited to thicknesses to have certain desired characteristics.

Next, the layers24(1)-24(4) and26(1)-26(3) are each sequentially applied over the substrate28and a sacrificial material in the trench30, which has a depth of about 500 angstrom, to the determined thickness for each of the layers24(1)-24(4) and26(1)-26(3). More specifically, the layer24(1) of tungsten was deposited on the substrate28and a sacrificial material in the trench30to a thickness of 220.5 A, because it was determined that this thickness put the neutral axis of this material for the layer24(1) in a controllable location. Next, the layer26(1) of titanium was deposited on the layer24(1) to a thickness of 249.0 A, so that the internal stresses in the layer26(1) put the neutral axis of this material for the layer26(1) in a controllable location. Next, the layer24(2) of tungsten was deposited on the layer26(1) to a thickness of 220.5 A, so that the internal stresses in the layer24(2) put the neutral axis of this material for the layer24(2) in a controllable location. Next, the layer26(2) of titanium was deposited on the layer24(2) to a thickness of 249.0 A, so that the internal stresses in the layer26(2) put the neutral axis of this material for the layer26(2) in a controllable location. Next, the layer24(3) of tungsten was deposited on the layer26(2) to a thickness of 220.5 A, so that the internal stresses in the layer24(3) put the neutral axis of this material for the layer24(3) in a controllable location. Next, the layer26(3) of titanium was deposited on the layer24(3) to a thickness of 249.0 A, so that the internal stresses in the layer26(3) put the neutral axis of this material for the layer26(3) in a controllable location. Next, the layer24(4) of tungsten was deposited on the layer26(3) to a thickness of 220.5 A, so that the internal stresses in the layer24(4) put the neutral axis of this material for the layer24(4) in a controllable location. Although tungsten and titanium are shown in this example as materials for the layers24(1)-24(4) and26(1)-26(3), other materials can be used for the layers24(1)-24(4) and26(1)-26(3), such as insulating materials and one or more of the layers could have other thicknesses.

Once the application of the layers24(1)-24(4) and26(1)-26(3) is completed, the sacrificial material in the trench30below at least a portion of the structure20is removed. The residual forces in the layers24(1)-24(4) and26(1)-26(3) of the structure20create a moment which suspends the structure20flat across the trench30, although the residual forces in the layers24(1)-24(4) can be set to result in other moments, such as one that causes the structure20to deflect upward or to deflect downward. With the present invention, the process of removing this sacrificial material in the trench30is simplified.

Additionally, by way of example only, images of other structures in MEMS devices in accordance with the present invention are illustrated inFIGS. 4A-5B. More specifically, an example of a released simply supported beam is illustrated inFIG. 4A, of a simply supported cantilever beam is illustrated inFIG. 4B, of a released thin film structure is illustrated inFIG. 5A, of a multilayered thin film composite is illustrated inFIG. 5B.

Accordingly, as illustrated and described herein the present invention allows the fabrication of simply supported beams, cantilevered beams, or diaphragms for MEMS devices that will conform to the design intent for shape and control geometries. The present invention allows a wider range of designs and final geometries that can be implemented and controlled in the MEMS and semiconductor fields. Further, the present invention helps reduce the amount of time needed to remove sacrificial layers for MEMS devices which decreases process time and increases production rates. The present invention also reduces requirements for higher selectivity with the etchants that are used.