Integrated Sensory Systems

Abstract

This invention describes the structure and function of an integrated multi-sensing system. Integrated systems described herein may be configured to form a microphone, pressure sensor, gas sensor or accelerometer. The system uses Fabry-Perot Interferometer in conjunction with beam collimator, beam splitter, optical waveguide and a photodetector integrated. It also describes a configurable method for tuning the integrated system to specific resonance frequency using electrostatic actuators.

Claims

1. A system, comprising: a beam collimator; a beam splitter; an optical waveguide; an interferometer; and a photodetector; wherein said interferometer comprising of a semi-transparent mirror and a fully reflective mirror; wherein said beam collimator, said beam splitter, said optical waveguide, said interferometer and said photodetector are coupled in a stack configuration; wherein said beam collimator, said beam splitter, said optical waveguide, wherein said interferometer is above said beam collimator; wherein said beam collimator is above said beam splitter; wherein said beam splitter is above said photodetector; wherein light is transmitted through said optical waveguide; wherein said light hits said beam splitter; wherein said beam splitter reflects said light towards said beam collimator; wherein said light passes through said beam collimator and is focused on said interferometer; wherein said light passes through said semi-transparent mirror of said interferometer; wherein said light is reflected by said fully reflective mirror of said interferometer; wherein said light is reflected back and forth between said semi-transparent mirror and said fully reflective mirror; wherein said reflected light passes through said semi-transparent mirror followed by said beam collimator followed by said beam splitter and is detected by said photodetector; wherein said system dynamically measures the displacement between said semi-transparent mirror and said fully reflective mirror.

2. A system as in claim 1, wherein any of said mirrors are movable.

3. A system as in claim 1, wherein said system comprises further of a plurality of electrostatic actuators, where said displacement between said mirrors is adjusted by said electrostatic actuators.

4. A system as in claim 3, wherein the surface of said mirrors can function as electrostatic actuator.

5. A system as in claim 3, wherein said displacement between said mirrors is configured by applying electric voltage to said electrostatic actuators.

6. A system as in claim 1, wherein said mirrors are vibrated via acoustic pressure level.

7. A system as in claim 1, wherein said displacement between said mirrors is changed by air pressure.

8. A system as in claim 1, wherein said mirrors are displaced via movement of said system.

9. A system as in claim 1, wherein said system can measure the natural frequency of said mirrors.

10. A system as in claim 1, wherein a single instance of said system can function as any combination of pressure sensor, microphone, accelerometer, and gas sensor.

11. A system as in claim 1, wherein multiple instances of said system are integrated into a single stack, wherein each of said instances may be rotated in any axis and be placed anywhere in said stack.

12. A system as in claim 1, wherein said optical waveguide, said beam collimator, said beam splitter, said interferometer, and said photodetector can be of any shape, size and material.

13. A system as in claiml, wherein said photodetector and said interferometer are stacked by some offset to allow clearance for direct attachment to pads or conductive elements.

14. A system as in claim 13, wherein said photodetector, and said electrostatic actuators are electrically coupled using wire bond or vias; with or without redistribution layer.

15. A system as in claim 1, wherein one or more devices are surface mounted or embedded within said system.

16. A system as in claim 1, wherein an energy source is coupled on any part of said system.

17. A system as in claim 1, wherein said system comprises of two or more of said semi-transparent mirrors and one of said reflective mirror.

18. A system as in claim 1, wherein trenches of any size and shape are etched in said mirrors.

19. A system as in claim 1, wherein said displacement between said mirrors is measured by obtaining the shift in the free spectral range at a particular frequency, or measuring the wavelength modulation of said reflected light.

20. A system as in claim 1, wherein said photodetector converts the optical signal to electrical signal, wherein said electrical signal is transmitted through said system to outside world or to an integrated ASIC chip for further processing.

21. A system, comprising: a beam collimator; a beam splitter; an optical waveguide; a reflective membrane; an interferometer; and a photodetector; wherein said interferometer comprising of two or more semi-transparent mirrors; wherein said beam collimator, said beam splitter, said optical waveguide, said reflective membrane, said interferometer and said photodetector are coupled in a stack configuration; wherein said reflective membrane is above said beam collimator; wherein said beam collimator is above said beam splitter; wherein said beam splitter is above said interferometer; wherein said interferometer is above said photodetector; wherein light is transmitted through said optical waveguide; wherein said light hits said beam splitter; wherein said beam splitter reflects said light towards said beam collimator; wherein said light passes through said beam collimator and is focused on said reflective membrane; wherein said light is reflected from said reflective membrane; wherein said reflected light passes through said beam collimator and said beam splitter and hits said interferometer; wherein said light is reflected back and forth between said semi-transparent mirrors of said interferometer; wherein said reflected light passes through said semi-transparent mirrors and is detected by said photodetector.

22. A system as in claim 21, wherein any of said mirrors and said reflective membrane are movable.

23. A system as in claim 21, wherein said system comprises further of a plurality of electrostatic actuators, where said displacement between said mirrors is adjusted by said electrostatic actuators.

24. A system as in claim 23, wherein the surface of said mirrors can function as electrostatic actuator.

25. A system as in claim 23, wherein said displacement between said mirrors is configured by applying electric voltage to said electrostatic actuators.

26. A system as in claim 22, wherein said reflective membrane is vibrated via acoustic pressure level.

27. A system as in claim 22, wherein said reflective membrane and said mirrors are displaced by air pressure.

28. A system as in claim 22, wherein said reflective membrane and said mirrors are displaced via movement of said system.

29. A system as in claim 22, wherein said system can measure the natural frequency of said mirrors.

30. A system as in claim 22, wherein a single instance of said system can function as any combination of pressure sensor, microphone, accelerometer, and gas sensor.

31. A system as in claim 22, wherein multiple instances of said system are integrated into a single stack, wherein each of said instances may be rotated in any axis and be placed anywhere in said stack.

32. A system as in claim 22, wherein said optical waveguide, said reflective membrane, said beam collimator, said beam splitter, said interferometer, and said photodetector can be of any shape, size and material.

33. A system as in claim 22, wherein said photodetector and said interferometer are stacked by some offset to allow clearance for direct attachment to pads or conductive elements.

34. A system as in claim 33, wherein said photodetector, and said electrostatic actuators are electrically coupled using wire bond or vias; with or without redistribution layer.

35. A system as in claim 22, wherein one or more devices are surface mounted or embedded within said system.

36. A system as in claim 22, wherein an energy source is coupled on any part of said system.

37. A system as in claim 22, wherein trenches of any size and shape are etched in said mirrors.

38. A system as in claim 22, wherein said displacement of said reflective membrane and said mirrors are measured by obtaining the shift in the free spectral range at a particular frequency, or measuring the wavelength modulation of said reflected light.

39. A system as in claim 22, wherein said photodetector converts the optical signal to electrical signal, wherein said electrical signal is transmitted through said system to outside world or to an integrated ASIC chip for further processing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0012] FIG. 1 is a side-view of a multi-sensing integrated MEMS system in accordance with an exemplary embodiment.

[0013] FIG. 2 is a side-view of thick upper and lower mirrors with trenches in accordance with an exemplary embodiment.

[0014] FIG. 3 is a side-view of multi-mirror assembly in accordance with an exemplary embodiment.

[0015] FIG. 4 is a side view of two mirrors used in multi-sensing integrated system, where it shows the light beam reflections in accordance with an exemplary embodiment.

[0016] FIG. 5 is a side view of another stacked arrangement of the components of the multi-sensing system in accordance with an exemplary embodiment.

DETAILED DESCRIPTION OF THE INVENTION

[0017] The various embodiments are described more fully with reference to the accompanying drawings. These example embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to readers of this specification having knowledge in the technical field. Like numbers refer to like elements throughout.

[0018] A new apparatus 100, method of making multi-sensing systems in stacked configuration are disclosed herein. Multi-sensing systems described herein may be configured to form a microphone, pressure sensor, accelerometer or gas sensor.

[0019] FIG. 1 is a side view of a multipurpose multi-sensing systems constructed to sense acoustic signal and act as a sensor such as microphone in accordance with an exemplary embodiment. The multipurpose sensing element of this invention is constructed around Fabry-Perot Interferometer (FPI) 196. In this embodiment, FPI 196 makes use of multiple reflections between a closely spaced partially transmitting mirrors 180, and totally reflective mirror 160 separated by spacers 150.

[0020] As shown in FIG. 4, part of the light 660 that passes through partially transmitting mirror 180 (beam 640) gets reflected (beam 650) by totally reflective mirror 160. This process continues and some portion of the light is re-transmitted each time the light reaches the lower mirror 180, resulting in multiple offset beams 660 which can interfere with each other. The large number of interfering rays 660 produces an interferometer with extremely high resolution, i.e. sub-nanometer resolution. In a microphone exemplary of this embodiment, the incident light from a monochromatic, or broadband light source is partially transmitted through mirror 180 and is reflected off of mirror 160 which senses the acoustic vibrations. Displacement of the mirror 160 correlated to the incident wave can be measure by either obtaining the shift in the free spectral range at a particular frequency, or measuring the wavelength modulation of the reflected signal. The transmitted optical signal from FPI mirror 180 is then absorbed by the photodetector 192 (FIG. 1), which converts the optical signal to electrical signal. Electrical signal is transmitted through the substrate 194 to the outside world or to an integrated ASIC chip 350 for further processing.

[0021] In one embodiment of this disclosure, an optical waveguide is used to deliver light from an outside light source (not shown). The light is partially reflected off of a micro fabricated beam splitter 103. The partially reflected beam then passes through a micro fabricated collimating lens and then into the Fabry-Perot Interferometer (FPI) 196.

[0022] FIG. 1 also shows the 3D construction of a multi-sensing system for concurrent measurement of multiple parameters. In one embodiment of this disclosure 100, structures 196 and 198 are stacked and offset to allow clearance for direct access to one or more pads 310 or one or more conductive elements 310. Combinations of one or more wire bonds 320, with or without redistribution layers (RDL) 340 or vias 330 can be used to communicate among the structures 196 and 198. System 100 may be integrated on a PCB (not shown) using conductive solder balls 380 or wire bonds 320. It is understood that order of stacking of structures 196 and 198 can vary and that any combination of solder balls, direct pad-to-pad or wire bonds (just to name a few) can be used to connect and assemble the structures 196, 198 and a host carrier (not shown). Structure 100 can be bonded/assembled on an ASIC chip 350 for various signal processing purposes. To further miniaturize the system 100, one or more ASIC chips 350 may be mounted on the surface or embedded within any of the stacked structures 196, 198. Structures 196 and 198 may be electrically/mechanically coupled to each other. For example, FIG. 5 shows a different order of stacking of the multi-sensing system 500 components. In this embodiment, mirror membrane 502 with fully reflective surface 370 is situated above the light delivery structure 501, followed by Fabry-Perot Interferometer (FPI) 196 consisting of two partially reflective mirrors 160, 180, followed by photo-detector 192.

[0023] In the combined microphone gas sensor exemplary of this embodiment, an adjustable mirror gap is required in order to produce the emission spectra of the target gas. This requires the placement of electrostatic actuators 360 between the Fabry-Perot mirrors 180, 160 in order to control the spacing gap between the mirrors for spectral tuning as depicted in FIG. 1. In combined microphone gas sensor configuration, the structure of the coupled components 196, 198 will remain the same as microphone, except for the addition of conducting electrostatic actuators in between the mirrors. Also, in order to maintain parallelism between the two mirrors during actuation, variable geometries that include tethered mirror may be employed during the fabrication.

[0024] In another embodiment of this invention, upon absorption of particular gas on the top mirror surface 370 gas sensing may be realized be measuring the natural frequency of the mirror 160. The change in the natural frequency can then be measured through the same process as explained earlier in paragraph [0021]. It is understood that structure 100 can be constructed in numerous shapes and sizes to optimize the position of the waveguide 101 while enhancing the FPI 198 exposure to the environment.

[0025] The advantage of multi-sensing system 100 is that it allows high precision optical deflection measurement, i.e. sub-nanometer deflection detection. It provides combined optical interferometric and emission spectra sensing capability as well as combined microphone and gas sensing capability. It provides tuning capability based on sound pressure level (SPL). In addition, it provides microphone with high sensitivity and wide frequency response with low noise floor better than 15 dB. More importantly, the system 100 has reduced power consumption, by using modulated light with low duty cycle.

[0026] In another embodiment of this invention a configurable FPI 198 structure is disclosed. An electrostatic actuation pad 360 may be placed inside the FPI 198 cavity 170 on both opposing sides of the mirrors 160, 180 facing each other. The actuation pads can be used to adjust the gap 170 for specific wavelength and can be used as a band pass filter. Band pass filter enables tuning in/out specific wavelengths.

[0027] In another embodiment of this invention as depicted in FIG. 2, FPI structure 400 is constructed using thick mirrors 450, 460 to maximize the mirrors finesse. The mirror finesse value has a direct effect on the sensitivity of the sensor. Similar to the thin mirrors 160, 180 used in FPI 196 in FIG. 1, the thick mirror FPI 400 may consist of two free mirrors 450, 460 to comprise a microphone only device. Or, one of the mirrors may be electrostatically actuated to enable the interferometer to measure the emission spectra of a target gas. In this embodiment, trenches 410 are etched on the thick mirror 450 to ensure flexibility of the top mirror 440 for acoustic sensitivity and electrostatic actuation. The bottom mirror 460 could be the same thickness or different thickness as the top mirror 450. Spacers 420 can be of variable thicknesses to vary the distance between the top mirror 440 and bottom mirror 430. To create an electrostatic actuator, the mirrors 430, 440 can also act as electrodes to vary the separation of the mirrors 430, 440. It is noted that trenches 410 can be any shape or size.

[0028] In another embodiment of this invention as depicted in FIG. 3, multiple mirrors 540 are stacked 500 to mitigate factors such as finesse, fabrication defects and parallelism that effects FPI performance. The separation between the mirrors 540 is determined by spacers 550. Multi-mirror FPI configuration 500, increases the sensitivity and resolution of the system. Another advantage of the multi-mirror FPI 500 is that it allows frequency ranges between two adjacent transmitted peaks and the Full Width Half Maximum (FWHM) of an FPI to be independently controlled. The cavity gaps 510, 520, 530 determines the Free Spectral Range (FSR). The mirrors reflectivity controls the Full Width Half Maximum (FWHM). The transmission peaks can be made sharper by increasing the reflectivity of the mirror surfaces in multi-mirror FPI. FPI mirror finesse is determined by the ratio of the spectral width over FWHM of the peaks, thus, the narrower FWHM peaks results in higher finesse of the overall FPI. Multi-mirror FPI 500 provides higher resolution and broader spectral range. As a result, multi-mirror FPI provides wider Sound Pressure Level (SPL) in microphone applications and wider emission spectrum for gas detection applications. In addition, multi-mirror FPI has lower optical transmission loss which results in lower power consumption.

[0029] In another embodiment of this invention, multiple sensors described in this invention, may be stacked and integrated in to one integrated system. Each individual sensor may be rotated in any axis and be placed anywhere in the stack. An example is to stack Three integrated sensors to enable X, Y and Z direction accelerometers. It is understood that structure 400 (FIG. 2) can be oriented/positioned in any spatial directions to be used as a multi-axis accelerometer. Additionally, each individual sensor may measure different parameter. For example, an integrated system may comprise of 3 sensors, one to measure CO2, another one to measures CO and yet another one to measures the movements in any dimension. Each of the integrated sensors in the stack may have its own characteristics, dimensions, shape and material. For example, in one integrated system, one of the sensors in the stack may have 2 parallel mirrors, while another sensor may have 4 parallel mirrors. Each of the sensors may have their own optical waveguide 101, which may be different from each other, or they may share the same optical waveguide 101. Similarly, each of the sensors may have their own photodetector 192, which may be different from each other, or they may share the same photodetector 192.

[0030] Having disclosed several embodiments, it will be recognized by those of skill in the art that various modifications, alternative constructions, and equivalents may be used without departing from the spirit of the disclosed embodiments. Additionally, a number of well-known processes and elements have not been described to avoid unnecessarily obscuring the embodiments described herein. Accordingly, the above description should not be taken as limiting the scope of the claims.

[0031] Where a range of values is provided, it is understood that each intervening value, to the tenth of the unit of the lower limit unless the context clearly dictates otherwise, between the upper and lower limits of that range is also specifically disclosed. Each smaller range between any stated value or intervening value in a stated range and any other stated or intervening value in that stated range is encompassed. The upper and lower limits of these smaller ranges may independently be included or excluded in the range, and each range where either, neither or both limits are included in the smaller ranges is also encompassed within the embodiments described, subject to any specifically excluded limit in the stated range. Where the stated range includes one or both of the limits, ranges excluding either or both of those included limits are also included.

[0032] As used herein and in the appended claims, the singular forms “a”, “an”, and “the” include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to “a process” includes a plurality of such processes and reference to “the dielectric material” includes reference to one or more dielectric materials and equivalents thereof known to those skilled in the art, and so forth.

[0033] Also, the words “comprise,” “comprising,” “include,” “including,” and “includes” when used in this specification and in the following claims are intended to specify the presence of stated features, integers, components, or steps, but they do not preclude the presence or addition of one or more other features, integers, components, steps, acts, or groups.