WO2014004067A1 - Semiconductor package with air pressure sensor - Google Patents
Semiconductor package with air pressure sensor Download PDFInfo
- Publication number
- WO2014004067A1 WO2014004067A1 PCT/US2013/045026 US2013045026W WO2014004067A1 WO 2014004067 A1 WO2014004067 A1 WO 2014004067A1 US 2013045026 W US2013045026 W US 2013045026W WO 2014004067 A1 WO2014004067 A1 WO 2014004067A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- cavity
- air pressure
- semiconductor package
- pressure sensor
- build
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
- G01L9/0041—Transmitting or indicating the displacement of flexible diaphragms
- G01L9/0042—Constructional details associated with semiconductive diaphragm sensors, e.g. etching, or constructional details of non-semiconductive diaphragms
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W90/00—Package configurations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B7/00—Microstructural systems ; Auxiliary parts of microstructural devices or systems
- B81B7/0032—Packages or encapsulation
- B81B7/0058—Packages or encapsulation for protecting against damages due to external chemical or mechanical influences, e.g. shocks or vibrations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B7/00—Microstructural systems ; Auxiliary parts of microstructural devices or systems
- B81B7/0032—Packages or encapsulation
- B81B7/0077—Other packages not provided for in groups B81B7/0035 - B81B7/0074
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
- B81C1/00—Manufacture or treatment of devices or systems in or on a substrate
- B81C1/00015—Manufacture or treatment of devices or systems in or on a substrate for manufacturing microsystems
- B81C1/00222—Integrating an electronic processing unit with a micromechanical structure
- B81C1/00246—Monolithic integration, i.e. micromechanical structure and electronic processing unit are integrated on the same substrate
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
- G01L9/0041—Transmitting or indicating the displacement of flexible diaphragms
- G01L9/0042—Constructional details associated with semiconductive diaphragm sensors, e.g. etching, or constructional details of non-semiconductive diaphragms
- G01L9/0047—Diaphragm with non uniform thickness, e.g. with grooves, bosses or continuously varying thickness
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
- G01L9/0041—Transmitting or indicating the displacement of flexible diaphragms
- G01L9/007—Transmitting or indicating the displacement of flexible diaphragms using variations in inductance
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
- G01L9/0041—Transmitting or indicating the displacement of flexible diaphragms
- G01L9/0072—Transmitting or indicating the displacement of flexible diaphragms using variations in capacitance
- G01L9/0073—Transmitting or indicating the displacement of flexible diaphragms using variations in capacitance using a semiconductive diaphragm
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W70/00—Package substrates; Interposers; Redistribution layers [RDL]
- H10W70/01—Manufacture or treatment
- H10W70/05—Manufacture or treatment of insulating or insulated package substrates, or of interposers, or of redistribution layers
- H10W70/08—Manufacture or treatment of insulating or insulated package substrates, or of interposers, or of redistribution layers by depositing layers on the chip or wafer, e.g. "chip-first" RDLs
- H10W70/09—Manufacture or treatment of insulating or insulated package substrates, or of interposers, or of redistribution layers by depositing layers on the chip or wafer, e.g. "chip-first" RDLs extending onto an encapsulation that laterally surrounds the chip or wafer, e.g. fan-out wafer level package [FOWLP] RDLs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B2201/00—Specific applications of microelectromechanical systems
- B81B2201/02—Sensors
- B81B2201/0264—Pressure sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B2203/00—Basic microelectromechanical structures
- B81B2203/01—Suspended structures, i.e. structures allowing a movement
- B81B2203/0127—Diaphragms, i.e. structures separating two media that can control the passage from one medium to another; Membranes, i.e. diaphragms with filtering function
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B2203/00—Basic microelectromechanical structures
- B81B2203/03—Static structures
- B81B2203/0315—Cavities
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
- B81B2203/00—Basic microelectromechanical structures
- B81B2203/04—Electrodes
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10D—INORGANIC ELECTRIC SEMICONDUCTOR DEVICES
- H10D48/00—Individual devices not covered by groups H10D1/00 - H10D44/00
- H10D48/50—Devices controlled by mechanical forces, e.g. pressure
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W72/00—Interconnections or connectors in packages
- H10W72/90—Bond pads, in general
- H10W72/941—Dispositions of bond pads
- H10W72/9413—Dispositions of bond pads on encapsulations
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W74/00—Encapsulations, e.g. protective coatings
- H10W74/10—Encapsulations, e.g. protective coatings characterised by their shape or disposition
- H10W74/131—Encapsulations, e.g. protective coatings characterised by their shape or disposition the semiconductor body being only partially enclosed
- H10W74/142—Encapsulations, e.g. protective coatings characterised by their shape or disposition the semiconductor body being only partially enclosed the encapsulations exposing the passive side of the semiconductor body
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W90/00—Package configurations
- H10W90/10—Configurations of laterally-adjacent chips
Definitions
- Embodiments of the invention are in the field of semiconductor packages and, in particular, semiconductor packages with air pressure sensors.
- semiconductor packages are used for protecting an integrated circuit (IC) chip or die, and also to provide the die with an electrical interface to external circuitry.
- IC integrated circuit
- semiconductor packages are designed to be even more compact and must support larger circuit density.
- some semiconductor packages now use a coreless substrate, which does not include the thick resin core layer commonly found in conventional substrates.
- the demand for higher performance devices results in a need for an improved semiconductor package that enables a thin packaging profile and low overall warpage compatible with subsequent assembly processing.
- MEMS microelectromechanical systems
- Figures 1A-1E illustrate cross-sectional views of various operations in a method of fabricating a reference cavity using a continuous via ring, in accordance with an embodiment of the present invention.
- Figures 2A-2E illustrate cross-sectional views of various operations in a first method of fabricating structural support for a reference cavity, in accordance with an embodiment of the present invention.
- Figures 3A-3F illustrate cross-sectional views of various operations in a second method of fabricating structural support for a reference cavity, in accordance with an embodiment of the present invention.
- Figures 4A-4C illustrate cross-sectional views of various operational states of a pressure sensor having an underlying reference cavity, in accordance with an embodiment of the present invention.
- Figure 5A illustrates a cross-sectional view and corresponding top view of an air pressure sensor having a single large opening to ambient conditions, in accordance with an embodiment of the present invention.
- Figure 5B illustrates a cross-sectional view and corresponding top view of an air pressure sensor having several small openings to ambient conditions, in accordance with an embodiment of the present invention.
- Figures 6A and 6B illustrate schematics and equations for determining analytical calculations for sensing air pressure in a capacitive manner, in accordance with an embodiment of the present invention.
- Figure 7A is a plot of capacitance change versus negative pressure difference, in accordance with an embodiment of the present invention.
- Figure 7B is a plot of capacitance change versus positive pressure difference, in accordance with an embodiment of the present invention.
- Figure 8 illustrates a plan view and corresponding cross-sectional view of a magnetically- actuated resonant beam air pressure sensor, in accordance with an embodiment of the present invention.
- Figure 9 illustrates schematics and equations for determining analytical calculations for sensing air pressure for a magnetically-actuated resonant beam air pressure sensor, in accordance with an embodiment of the present invention.
- Figure 10A is a plot of estimated response frequency for a magnetically actuated air pressure sensor, in accordance with an embodiment of the present invention.
- Figure 1 OB is a plot of estimated response sensitivity, for a magnetically actuated air pressure sensor, in accordance with an embodiment of the present invention.
- FIGS 11 A- I IP illustrate cross-sectional views of various operations in a process flow using copper mesh support for lamination of ABF above a reference cavity, in accordance with an embodiment of the present invention.
- Figures 12A-12Q illustrate cross-sectional views of various operations in a process flow using a thin plate to support lamination of ABF above a reference cavity, in accordance with an embodiment of the present invention.
- Figures 13A-13T illustrate cross-sectional views of various operations in a process flow for fabricating a magnetically actuated pressure sensor, in accordance with an embodiment of the present invention.
- Figure 14 is a schematic of a computer system, in accordance with an embodiment of the present invention.
- One or more embodiments described herein are directed to semiconductor packages having one or more microelectromechanical systems (MEMS) structures incorporated therein.
- MEMS microelectromechanical systems
- an air pressure sensor is fabricated in package build-up layers.
- One or more embodiments pertain to one or more air pressure sensors, bumpless build-up layer (BBUL) packaging, electrostatic sensors, hermetic sealing, magnetically actuated sensors, or MEMS technologies. Structures or devices described herein may have applications in one or more of mobile/consumer products which use BBUL technology.
- BBUL embedded packaging technology may be considered for mobile chip packaging technology.
- Air pressure sensors are important for consumer mobile devices, providing accurate altitude and barometric measurements. Accordingly, in an embodiment, an air pressure sensor is fabricated in or via BBUL technology. As a comparison, conventional air pressure sensors are typically relatively thick compared to a silicon die. Embedding of such sensors into a package for a silicon die may increase package thickness and cost, rendering the overall package less attractive. Furthermore, MEMS-based air pressure sensors typically use a hermetically- sealed pressure chamber to provide a reference air pressure. Accordingly, in an embodiment, air pressure sensors are fabricated directly in BBUL build-up-layers. Compared with embedding silicon based pressure sensors, approach described herein retain a super-thin feature of BBUL, and also mitigate costs associated with separately fabricated air pressure sensors.
- embodiments described herein target building or fabricating air pressure sensors or other MEMS devices using packaging build-up-layers. It is to be understood that a challenge of using such build-up layer technology for air pressure sensors may be a need for the manufacture of a hermetically-sealed package. Due to the porous nature of standard Ajinomoto build-up film (ABF) build-up layers (or other similar laminated materials), laminated ABF layers may not be adequate for forming an air pressure cavity.
- ABS Ajinomoto build-up film
- a copper via ring is used to form a hermetically sealed package for the reference air pressure. The top surface of the sealed package acts as a diaphragm and is the bottom electrode for the electrostatic sensing mechanism.
- a "continuous via ring” method is adaptable for other MEMS applications requiring a reference air cavity or hermetic sealing of structures.
- a continuous via ring may be fabricated for MEMS-based packaging.
- Figures 1A-1E illustrate cross-sectional views of various operations in a method of fabricating a reference cavity using a continuous via ring, in accordance with an embodiment of the present invention.
- Such an approach may be used where it is difficult to form a sealed cavity for a pressure sensor by using only ABF, due to the porosity of the ABF material.
- a stack 100 including a first insulating laminate layer 102, a plating layer 104 (e.g. a copper plating layer), and a second insulating laminate layer 106.
- Vias 108 e.g., copper vias
- a cavity 110 is formed in second insulating laminate layer 106, between vias 108 and exposing plating layer 104, e.g., by an oxygen plasma etch process.
- a third insulating laminate layer 112 is then formed over the structure of Figure 1C, as depicted in Figure ID.
- a continuous via ring is generated by forming second vias 114 in the third insulating laminate layer 112, and forming a top membrane plating layer 116, e.g., a copper membrane plating layer, above the third insulating laminate layer 112.
- the copper continuous via ring (from vias 108 and 112), as well as the top copper plating 116 and bottom copper plating 104 form a hermetic seal over the air pressure cavity 110.
- Insulating lamination layers described herein may, in an embodiment, refer to alternating conducting and dielectric layers, the latter being, e.g., an ABF or ABF-like layer.
- FIGS. 2A-2E illustrate cross-sectional views of various operations in a first method of fabricating structural support for a reference cavity, in accordance with an embodiment of the present invention.
- a stack 200 including a first insulating laminate layer
- a plating layer 204 e.g. a copper plating layer
- a second insulating laminate layer 206 e.g. a copper plating layer
- Vias 208 e.g., copper vias
- a mesh pattern 209 is formed, as depicted in Figure 2B.
- a cavity 210 is formed below the mesh pattern 209, e.g., by an oxygen plasma etch process.
- a third insulating laminate layer 212 is then formed over the structure of Figure 2C, as depicted in Figure 2D.
- a continuous via ring is generated by forming second vias 214 in the third insulating laminate layer 212, and forming a top membrane plating layer 216, e.g., a copper membrane plating layer, above the third insulating laminate layer 212.
- the copper continuous via ring (from vias 208 and 212), as well as the top copper plating 216 and bottom copper plating 204 form a hermetic seal over the air pressure cavity 210.
- the cavity 210 is structurally supported by the overlying mesh pattern 209.
- Figures 3A-3F illustrate cross-sectional views of various operations in a second method of fabricating structural support for a reference cavity, in accordance with an embodiment of the present invention.
- a stack 300 including a first insulating laminate layer 302, a plating layer 304 (e.g. a copper plating layer), and a second insulating laminate layer 306.
- Vias 308 e.g., copper vias
- a cavity 310 is formed, e.g., by an oxygen plasma etch process.
- a thin plate 311, e.g., a thin polymeric or metal plate, is then formed or placed over the cavity 310, as depicted in Figure 3D.
- a third insulating laminate layer 312 is then formed over the structure of Figure 3D.
- a continuous via ring is generated by forming second vias 314 in the third insulating laminate layer 312, and forming a top membrane plating layer 316, e.g., a copper membrane plating layer, above the third insulating laminate layer 312.
- the copper continuous via ring (from vias 308 and 312), as well as the top copper plating 316 and bottom copper plating 304 form a hermetic seal over the air pressure cavity 310.
- the cavity 310 is structurally supported by the overlying thin plate 311.
- the thin plate 311 has a higher glass transition temperature (Tg) than the ABF cure temperature such that the plate can provide a mechanical shield during ABF lamination.
- Tg glass transition temperature
- the thin plate 311 has some adhesion or stiction to copper in order to enable fixing the plate in position during ABF lamination. The seal, however, need not be perfect since the fabricated copper membrane may be relied on for hermeticity.
- a capacitive pressure sensor may be fabricated to include a reference cavity as described above.
- Figures 4A-4C illustrate cross-sectional views of various operational states of a pressure sensor having an underlying reference cavity, in accordance with an embodiment of the present invention.
- an air pressure sensor 400 is formed from suspended features 402 (e.g., suspended copper features) and electrodes 404 (e.g., copper electrodes) formed above a reference cavity 410.
- reference cavity 410 is formed based on the structure of Figure IE (as depicted in Figure 4A) but could be formed based on structures such as those depicted in 2E or 3F as well.
- the air pressure sensor 400 is able to compare an ambient air pressure 420 with a reference air pressure 422 through capactive coupling (C), as depicted by the arrows in Figures 4A-4C.
- the capactive coupling (C) is based on the distance between the suspended member 402 and the underlying structure formed above reference cavity 410.
- the ambient air pressure 420 is the same as the reference air pressure 422, and the system is effectively at rest with a distance 430 between the suspended member 402 and the underlying structure formed above reference cavity 410 essentially the fabrication height of the two layers.
- the ambient air pressure 420 is greater than the reference air pressure 422, and the distance 430 between the suspended member 402 and the underlying structure formed above reference cavity 410 is greater than the fabrication height of the two layers.
- the ambient air pressure 420 is less than the reference air pressure 422, and the distance 434 between the suspended member 402 and the underlying structure formed above reference cavity 410 is less than the fabrication height of the two layers.
- a barometric pressure sensor may be fabricated using a reference air cavity. The difference between ambient air pressure and reference air pressure is detected by an upwards or downwards deflection of the "diaphragm" formed to include the reference cavity. The sensed capacitance reflects the extent of downward or upward deflection of the diaphragm. Different configurations may be possible for forming an opening to an air pressure sensor.
- Figure 5A illustrates a cross-sectional view and corresponding top view of an air pressure sensor having a single large opening to ambient conditions, in accordance with an embodiment of the present invention.
- an air pressure sensor 500A is formed to include a stiff top layer/electrode 502A, a flexible bottom layer/electrode 504A, and a reference air gap 506A.
- air pressure sensor 500A is fabricated based on the structure of Figure IE, e.g., as structure 400 of Figure 4A (as depicted in Figure 5A) but could be formed based on structures such as those depicted in Figures 2E or 3F as well.
- a single opening 550A is included for exposure of the flexible bottom layer/electrode 504A, as depicted in both views of Figure 5A.
- Figure 5B illustrates a cross- sectional view and corresponding top view of an air pressure sensor having several small openings to ambient conditions, in
- an air pressure sensor 500B is formed to include a stiff top layer/electrode 502B, a flexible bottom
- air pressure sensor 500B is fabricated based on the structure of Figure IE, e.g., as structure 400 of Figure 4A (as depicted in Figure 5B) but could be formed based on structures such as those depicted in Figures 2E or 3F as well.
- a plurality of openings 550B is included for exposure of the flexible bottom
- a sensed capacitance may be based on diaphragm motion in an air pressure sensor.
- Figures 6A and 6B illustrate schematics and equations for determining analytical calculations for sensing air pressure in a capacitive manner, in accordance with an embodiment of the present invention.
- an analytical approach may be developed to model the sensitivity and range of the air pressure sensor. Referring to Figure 6 A, for such estimations, it is assumed that an air pressure sensor 600 includes a top electrode 602 that is rigid and a bottom electrode 604 that is flexible. A capacitance (C) is sensed between 602 and 604. The maximum diaphragm deformation is estimated, and the deformation shape of the diaphragm is approximated to be pyramidal.
- the total capacitance is the integral sum of each individual capacitance dC.
- square diaphragm deflection is determined by 606. Diaphragm deflection is approximated by a pyramidal surface.
- the capacitance dC is integrated along the length and width of the capacitor, via 608.
- the total capacitance 614 is then determined using 610 and 612.
- FIG. 7A is a plot 700 of capacitance change versus negative pressure difference
- Figure 7B is a plot 702 of capacitance change versus positive pressure difference, in accordance with an embodiment of the present invention.
- the target range is approximately 0.5 atm to 1 atm (approximately 50kPa to lOOkPa), with a minimum detectable sensitivity of 50 Pa to lOOPa.
- sufficient sensitivity and range is achieved with a 1.5mm x 1.5mm diaphragm.
- FIG. 8 illustrates a plan view and corresponding cross-sectional view of a magnetically-actuated resonant beam air pressure sensor, in accordance with an embodiment of the present invention.
- a magnetically-actuated resonant beam air pressure sensor 800 includes a diaphragm 802, resonant beams 804 and an embedded magnet 806. Resonant beams are actuated through interaction of an AC current with the permanent magnet.
- diaphragm deflection due to a difference in air pressure transduces a Z-displacement, which applies tension onto the resonant beam and increases the resonant frequency.
- structures may be more sensitive to changes in resonant frequency, and so may have a higher sensitivity in such a configuration.
- Figure 9 illustrates schematics and equations for determining analytical calculations for sensing air pressure for a magnetically-actuated resonant beam air pressure sensor, in accordance with an embodiment of the present invention.
- the maximum diaphragm deflection is given by 902.
- Diaphragm deflection induces Z-change, which applies tension to the resonant beams, as depicted in 904.
- An analytical approach is used to model the sensitivity and range of the magnetically-actuated air pressure sensor. It is assumed that the change in diaphragm height contributes to a change in beam length which translates into beam tension and an increased beam resonant frequency.
- equations 906, 908, 910, 912 and 914 the beam is assumed to be resonating in the y-direction, though in principle, any resonant mode may be used.
- a response may be estimated for a magnetically actuated air pressure sensor.
- Figure 10A is a plot 1000 of estimated response frequency (Hz)
- Figure 10B is a plot 1002 of estimated response sensitivity ( ⁇ /Pa), for a magnetically actuated air pressure sensor, in accordance with an embodiment of the present invention.
- the target range is approximately 0.5 atm to latm (approximately 50kPa to lOOkPa), with a minimum detectable sensitivity of 50 Pa to
- Beam length is lOOOum
- beam resonant frequency is approximately 15000Hz.
- a change in 50 Pa translates into a frequency change of more than lHz, which is sufficient sensitivity for certain applications.
- a packaged MEMS device such as an air pressure sensor, may be housed in a variety of packaging options.
- Figures 1 lA-1 IP illustrate cross-sectional views of various operations in a process flow using copper mesh support for lamination of ABF above a reference cavity, in accordance with an embodiment of the present invention.
- a die 1102 (which may include an amplifier, etc.) is placed on a thin substrate 1104 (e.g., silicon, etc.) adjacent an electrode 1106 (e.g., a copper electrode), above a metal holder 1100 (e.g., a copper holder).
- a laminate organic dielectric film 1108 is disposed above the structure of Figure 11A, as depicted in Figure 1 IB.
- via hole drilling and electroplating is performed to provide vias 1110 and copper layer 1112 (again, a suitable metal other than copper may be used wherever copper is referred to herein).
- a photoresist layer 1114 is then formed and patterned to protect sensitive areas, as depicted in Figure 1 ID.
- oxygen plasma release is then performed to remove a portion of organic dielectric film 1108 and to release structure 1116. Resist stripping is then performed to re-expose layer 1112, as depicted in Figure 1 IF.
- lamination of an organic dielectric film 1118 is then performed. Via drilling and electroplating is then performed to provide vias 1120 and copper layer 1122, as depicted in Figure 11H.
- organic dielectric film 1124 is then laminated on the structure of Figure 11H. Via drilling and electroplating is again performed to provide vias 1126 and copper layer 1128, as depicted in Figure 11J. Additionally, a copper mesh structure 1130 is electroplated for lamination support.
- photoresist layer 1132 is formed and patterned to protect sensitive areas. An oxygen plasma release is the performed to release structure 1134, as depicted in Figure 11L.
- photoresist layer 1132 is then stripped, re- exposing layer 1128.
- Lamination of another insulator layer 1136 is then performed above the structure of Figure 11M, as depicted in Figure 1 IN.
- via drilling and electroplating is performed to provide vias 1138 and copper layer 1140.
- the copper holder 1100 is then removed, as depicted in Figure 1 IP.
- a reference cavity 1150 and capacitor 1152 is thus formed.
- the structure as depicted can be viewed as a completed package for the semiconductor die included therein.
- an array of external contacts e.g., BGA contacts
- the resulting structure may then be coupled to a printed circuit board (PCB) or like receiving surface.
- PCB printed circuit board
- Figures 12A-12Q illustrate cross-sectional views of various operations in a process flow using a thin plate to support lamination of ABF above a reference cavity, in accordance with an embodiment of the present invention.
- a die 1202 (which may include an amplifier, etc.) is placed on a thin substrate 1204 (e.g., silicon, etc.) adjacent an electrode 1206 (e.g., a copper electrode), above a metal holder 1200 (e.g., a copper holder).
- a laminate organic dielectric film 1208 is disposed above the structure of Figure 12A, as depicted in Figure 12B.
- via hole drilling and electroplating is performed to provide vias 1210 and copper layer 1212.
- a photoresist layer 1214 is then formed and patterned to protect sensitive areas, as depicted in Figure 12D.
- oxygen plasma release is then performed to remove a portion of organic dielectric film 1208 and to release structure 1216. Resist stripping is then performed to re-expose layer 1212, as depicted in Figure 12F.
- lamination of an organic dielectric film 1218 is then performed. Via drilling and electroplating is then performed to provide vias 1220 and copper layer 1222, as depicted in Figure 12H.
- organic dielectric film 1224 (e.g., ABF) is then laminated on the structure of Figure 12H.
- Via drilling and electroplating is again performed to provide vias 1226 and copper layer 1228, as depicted in Figure 12J.
- photoresist layer 1230 is formed and patterned to protect sensitive areas.
- An oxygen plasma release is the performed to release structure 1232, as depicted in Figure 12L.
- photoresist layer 1230 is then stripped, re-exposing layer 1228.
- a pick and place approach is then performed to provide a thin plate 1234, as depicted in Figure 12N.
- lamination of another insulator layer 1236 is then performed above the structure of Figure 12N.
- Via drilling and electroplating is performed to provide vias 1238 and copper layer 1240, as depicted in Figure 12P.
- the copper holder 1200 is then removed.
- a reference cavity 1250 and capacitor 1252 is thus formed.
- the structure as depicted can be viewed as a completed package for the semiconductor die included therein.
- an array of external contacts e.g., BGA contacts
- the resulting structure may then be coupled to a printed circuit board (PCB) or like receiving surface.
- PCB printed circuit board
- Figures 13A-13T illustrate cross-sectional views of various operations in a process flow for fabricating a magnetically actuated pressure sensor, in accordance with an embodiment of the present invention.
- a die 1302 which may include an amplifier, etc.
- a thin substrate 1304 e.g., silicon, etc.
- a metal holder 1300 e.g., a copper holder
- a laminate organic dielectric film 1308 is disposed above the structure of Figure 13 A, as depicted in Figure 13B.
- via hole drilling and electroplating is performed to provide vias 1310 and copper layer 1312.
- a laminate organic dielectric film 1314 is then disposed above the structure of Figure 13C, as depicted in Figure 13D.
- via hole drilling and electroplating is performed to provide vias 1316 and copper layer 1318.
- a photoresist layer 1320 is then formed and patterned to protect sensitive areas, as depicted in Figure 13F.
- oxygen plasma release is then performed to remove a portion of organic dielectric film 1314 and to release structure 1322. Resist stripping is then performed to re-expose layer 1318, as depicted in Figure 13H.
- a thin metal plate 1324 may be optionally provided for support or, alternatively, a mesh structure may be formed.
- organic dielectric film 1326 is then performed. Via drilling and electroplating is then performed to provide vias 1328 and copper layer 1330, as depicted in Figure 13K.
- organic dielectric film 1332 e.g., ABF
- a trace layer including resonant beam coils may be formed during this process operation.
- organic dielectric film 1338 is then laminated on the structure of Figure 13M. Via drilling and electroplating is again performed to provide vias 1340 and copper layer 1342, as depicted in Figure 130. This operation may be used if, e.g., support meshing is to be formed. In such a case, plate protection mesh is formed as an optional structural support and is anchored at many locations not occupied by MEMS structure.
- photoresist layer 1344 is formed and patterned to protect sensitive areas. An oxygen plasma release is then performed to release structure 1346, as depicted in Figure 13Q.
- photoresist layer 1344 is then stripped, re-exposing layer 1342.
- an array of external contacts may optionally be formed above or below the structure depicted in Figure 13T.
- the resulting structure may then be coupled to a printed circuit board (PCB) or like receiving surface.
- PCB printed circuit board
- an air pressure sensor may be fabricated in BBUL layers.
- the BBUL layer may be part of a larger BBUL system.
- BBUL is a processor packaging technology that is bumpless since it does not use the usual small solder bumps to attach the silicon die to the processor package wires.
- electrically conductive vias and routing layers are formed above the active side of a semiconductor die using a semi- additive process (SAP) to complete remaining layers.
- SAP semi- additive process
- An air pressure sensor may be formed in BBUL layers during packaging of a
- a carrier may include panels with 1000 recesses on either side, allowing for fabrication of 2000 individual packages from a single carrier.
- the panel may include an adhesion release layer and an adhesive binder.
- a cutting zone may be provided at each end of the apparatus for separation processing.
- a backside of a semiconductor die may be bonded to the panel with a die-bonding film.
- Encapsulating layers may be formed by a lamination process. In another embodiment, one or more encapsulation layers may be formed by spinning on and curing a dielectric upon a wafer- scale array of apparatuses.
- the substrate formed is a coreless substrate since a panel is used to support the packaging of a semiconductor die through to formation of an array of external conductive conducts. The panel is then removed to provide a coreless package for the semiconductor die.
- the term "coreless” is used to mean that the support upon which the package was formed for housing a die is ultimately removed at the end of a build-up process.
- a coreless substrate is one that does not include a thick core after completion of the fabrication process.
- a thick core may be one composed of a reinforced material such as is used in a motherboard and may include conductive vias therein. It is to be understood that die-bonding film may be retained or may be removed. In either case, inclusion or exclusion of a die-bonding film following removal of the panel provides a coreless substrate. Still further, the substrate may be considered a coreless substrate because it does not include a thick core such as a fiber reinforced glass epoxy resin.
- an active surface of the packaged semiconductor die includes a plurality of semiconductor devices, such as but not limited to transistors, capacitors and resistors interconnected together by a die interconnection structure into functional circuits to thereby form an integrated circuit.
- the device side of the semiconductor die includes an active portion with integrated circuitry and interconnections.
- the semiconductor die may be any appropriate integrated circuit device including but not limited to a microprocessor (single or multi-core), a memory device, a chipset, a graphics device, an application specific integrated circuit according to several different embodiments.
- more than one die is embedded in the same package.
- a packaged semiconductor die further includes a secondary stacked die.
- the first die may have one or more through-silicon vias disposed therein (TSV die).
- TSV die through-silicon vias disposed therein
- the second die may be electrically coupled to the TSV die through the one or more through-silicon vias.
- both dies are embedded in a coreless substrate.
- the packaged semiconductor die may, in an embodiment, be a fully embedded and surrounded semiconductor die.
- "fully embedded and surrounded” means that all surfaces of the semiconductor die are in contact with an encapsulating film (such as a dielectric layer) of substrate, or at least in contact with a material housed within the encapsulating film. Said another way, “fully embedded and surrounded” means that all exposed surfaces of the semiconductor die are in contact with the encapsulating film of a substrate.
- the packaged semiconductor die may, in an embodiment, be a fully embedded semiconductor die.
- "fully embedded” means that an active surface and the entire sidewalls of the semiconductor die are in contact with an encapsulating film (such as a dielectric layer) of a substrate, or at least in contact with a material housed within the encapsulating film.
- "fully embedded” means that all exposed regions of an active surface and the exposed portions of the entire sidewalls of the semiconductor die are in contact with the encapsulating film of a substrate.
- the semiconductor die is not “surrounded” since the backside of the semiconductor die is not in contact with an encapsulating film of the substrate or with a material housed within the encapsulating film.
- a back surface of the semiconductor die protrudes from the global planarity surface of the die side of a substrate.
- no surface of the semiconductor die protrudes from the global planarity surface of the die side of a substrate.
- a “partially embedded” die is a die having an entire surface, but only a portion of the sidewalls, in contact with an encapsulating film of a substrate (such as a coreless substrate), or at least in contact with a material housed within the encapsulating film.
- a “non- embedded” die is a die having at most one surface, and no portion of the sidewalls, in contact with an encapsulating film of a substrate (such as a coreless substrate), or in contact with a material housed within the encapsulating film.
- an array of external conductive contacts may subsequently be formed.
- the external conductive contacts couple the formed substrate to a foundation substrate.
- the external conductive contacts may be used for electrical
- the array of external conductive contacts is a ball grid array (BGA). In other embodiments, the array of external conductive contacts is an array such as, but not limited to, a land grid array (LGA) or an array of pins (PGA).
- BGA ball grid array
- LGA land grid array
- PGA array of pins
- the substrate is a BBUL substrate.
- an air pressure sensor is embedded within the buildup layers along with a semiconductor die.
- a semiconductor die is housed in a core of a substrate.
- fan-out layers are used.
- MEMS generally refers to an apparatus incorporating some mechanical structure having a dimensional scale that is comparable to microelectronic devices.
- the mechanical structure is typically capable of some form of mechanical motion and having dimensions below approximately 250 microns; however, some embodiments may include MEMS sensors that are a few millimeters across a package.
- MEMS structures are typically capable of some form of mechanical motion and having dimensions below approximately 250 microns; however, some embodiments may include MEMS sensors that are a few millimeters across a package.
- a MEMS structure may be any mechanical and electronic structure having a critical dimension of less than approximately 250 microns and fabricated using lithography, deposition, and etching processes above a substrate.
- the MEMS structure is a device such as, but not limited to, a resonator, a sensor, a detector, a filter or a mirror.
- the MEMS structure is a resonator.
- the resonator is one such as, but not limited to, a beam, a plate and a tuning fork or a cantilever arm.
- an electroplated copper layer is used to form a hermetic seal for a reference air pressure cavity for a MEMS based air pressure sensor.
- Embodiments of the present invention may be suitable for fabricating a system on a chip (SOC), e.g., for a smartphone or a tablet.
- SOC system on a chip
- an air pressure sensor is integrated and fabricated in a BBUL packaging fab.
- the same backend processing used for existing BBUL coreless packaging may be used as a base flow.
- the process flow for die integration with MEMS may be applicable to other packaging substrate technologies.
- Figure 14 is a schematic of a computer system 1400, in accordance with an embodiment of the present invention.
- the computer system 1400 (also referred to as the electronic system 1400) as depicted can embody a semiconductor package having an air pressure sensor according to any of the several disclosed embodiments and their equivalents as set forth in this disclosure.
- the computer system 1400 may be a mobile device such as a netbook computer.
- the computer system 1400 may be a mobile device such as a wireless smart phone.
- the computer system 1400 may be a desktop computer.
- the computer system 1400 may be a hand-held reader.
- the computer system 1400 may be a watch.
- the electronic system 1400 is a computer system that includes a system bus 1420 to electrically couple the various components of the electronic system 1400.
- the system bus 1420 is a single bus or any combination of busses according to various embodiments.
- the electronic system 1400 includes a voltage source 1430 that provides power to the integrated circuit 1410. In some embodiments, the voltage source 1430 supplies current to the integrated circuit 1410 through the system bus 1420.
- the integrated circuit 1410 is electrically coupled to the system bus 1420 and includes any circuit, or combination of circuits according to an embodiment.
- the integrated circuit 1410 includes a processor 1412 that can be of any type.
- the processor 1412 may mean any type of circuit such as, but not limited to, a microprocessor, a microcontroller, a graphics processor, a digital signal processor, or another processor.
- the processor 1412 includes or is included in a semiconductor package having an air pressure sensor, as disclosed herein.
- SRAM embodiments are found in memory caches of the processor.
- circuits that can be included in the integrated circuit 1410 are a custom circuit or an application-specific integrated circuit (ASIC), such as a communications circuit 1414 for use in wireless devices such as cellular telephones, smart phones, pagers, portable computers, two-way radios, and similar electronic systems.
- ASIC application-specific integrated circuit
- the processor 1410 includes on-die memory 1416 such as static random-access memory (SRAM).
- the processor 1410 includes embedded on-die memory 1416 such as embedded dynamic random- access memory (eDRAM).
- the integrated circuit 1410 is complemented with a subsequent integrated circuit 1411.
- Useful embodiments include a dual processor 1413 and a dual communications circuit 1415 and dual on-die memory 1417 such as SRAM.
- the dual integrated circuit 1410 includes embedded on-die memory 1417 such as eDRAM.
- the electronic system 1400 also includes an external memory 1440 that in turn may include one or more memory elements suitable to the particular application, such as a main memory 1442 in the form of RAM, one or more hard drives 1444, and/or one or more drives that handle removable media 1446, such as diskettes, compact disks (CDs), digital variable disks (DVDs), flash memory drives, and other removable media known in the art.
- the external memory 1440 may also be embedded memory 1448 such as the first die in an embedded TSV die stack, according to an embodiment.
- the electronic system 1400 also includes a display device 1450 and an audio output 1460.
- the electronic system 1400 includes an input device such as a controller 1470 that may be a keyboard, mouse, trackball, game controller, microphone, voice-recognition device, or any other input device that inputs information into the electronic system 1400.
- an input device 1470 is a camera.
- an input device 1470 is a digital sound recorder.
- an input device 1470 is a camera and a digital sound recorder.
- the integrated circuit 1410 may be implemented in a number of different embodiments, including a semiconductor package having an air pressure sensor according to any of the several disclosed embodiments and their equivalents, an electronic system, a computer system, one or more methods of fabricating an integrated circuit, and one or more methods of fabricating an electronic assembly that includes a semiconductor package having an air pressure sensor according to any of the several disclosed embodiments as set forth herein in the various embodiments and their art-recognized equivalents.
- the elements, materials, geometries, dimensions, and sequence of operations can all be varied to suit particular I/O coupling requirements including array contact count, array contact configuration for a
- microelectronic die embedded in a processor mounting substrate according to any of the several disclosed semiconductor package having an air pressure sensor embodiments and their equivalents.
- a foundation substrate may be included, as represented by the dashed line of Figure 14.
- Passive devices may also be included, as is also depicted in Figure 14.
- Embodiments of the present invention include semiconductor packages with air pressure sensors.
- a semiconductor package includes a plurality of build-up layers.
- a cavity is disposed in one or more of the build-up layers.
- An air pressure sensor is disposed in the plurality of build-up layers and includes the cavity and an electrode disposed above the cavity.
- the cavity is a hermetically sealed cavity.
- the hermetically sealed cavity is composed of a continuous via ring.
- one or more of the build-up layers having the hermetically sealed cavity disposed therein is an Anjinomoto build-up film (ABF) layer, and the continuous via ring is composed of copper.
- ABSF Anjinomoto build-up film
- the air pressure sensor includes a MEMS device.
- a diaphragm of the MEMS device includes the cavity, and the electrode includes a suspended portion of the MEMS device.
- the suspended portion of the MEMS device is composed of copper.
- the semiconductor package further includes a layer having a mesh pattern disposed in the cavity, the layer providing structural support for the cavity.
- the semiconductor package further includes a thin metal plate disposed between the cavity and the electrode, the thin metal plate providing structural support for the cavity.
- the cavity provides a reference pressure for the air pressure sensor.
- the semiconductor package further includes a bumpless build-up layer (BBUL) substrate.
- BBUL bumpless build-up layer
- the BBUL substrate is a coreless substrate.
- a semiconductor package in an embodiment, includes a substrate composed of a plurality of build-up layers.
- a semiconductor die is housed in the substrate.
- a cavity is disposed in one or more of the build-up layers, above the semiconductor die.
- An air pressure sensor is disposed in the plurality of build-up layers and includes the cavity and an electrode disposed above the cavity. The electrode is electrically coupled to the semiconductor die.
- the semiconductor package also includes one or more openings exposing a portion of the air pressure sensor to air pressure ambient to the semiconductor package.
- the substrate is a bumpless build-up layer (BBUL) substrate.
- BBUL bumpless build-up layer
- the BBUL substrate is a coreless substrate.
- the cavity is a hermetically sealed cavity.
- the hermetically sealed cavity is composed of a continuous via ring.
- one or more of the build-up layers having the hermetically sealed cavity disposed therein is an Anjinomoto build-up film (ABF) layer, and the continuous via ring is composed of copper.
- ABSF Anjinomoto build-up film
- the air pressure sensor includes a MEMS device.
- a diaphragm of the MEMS device includes the cavity, and the electrode includes a suspended portion of the MEMS device.
- the suspended portion of the MEMS device is composed of copper.
- the MEMS device is disposed proximate to an active surface of the semiconductor die and distal from a back surface of the semiconductor die.
- the semiconductor package further includes a layer having a mesh pattern disposed in the cavity, the layer providing structural support for the cavity.
- the semiconductor package further includes a thin metal plate disposed between the cavity and the electrode, the thin metal plate providing structural support for the cavity.
- the cavity provides a reference pressure for the air pressure sensor.
- the semiconductor package further includes a permanent magnet coupled with the air pressure sensor.
- a method of sensing air pressure ambient to a semiconductor package includes determining an extent of capacitive coupling between a diaphragm of an air pressure sensor and an electrode of the air pressure sensor.
- the diaphragm includes a hermetically sealed cavity disposed below the electrode and in build-up layers of the semiconductor package.
- the hermetically sealed cavity has a reference pressure.
- the method also includes correlating the extent of capacitive coupling with a difference between the reference pressure and the ambient pressure.
- the diaphragm reduces the size of the hermetically sealed cavity, and increases a distance between the diaphragm and the electrode, when the ambient air pressure is greater than the reference pressure.
- the diaphragm increases the size of the hermetically sealed cavity, and decreases a distance between the diaphragm and the electrode, when the ambient air pressure is less than the reference pressure.
- the air pressure sensor includes a resonant beam.
- the method further includes actuating the resonant beam through interaction of an AC current with a permanent magnet.
- a diaphragm deflection is due to a difference in air pressure and transduces a Z- displacement which applies tension onto the resonant beam and increases a resonant frequency of the resonant beam.
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Computer Hardware Design (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Health & Medical Sciences (AREA)
- Measuring Fluid Pressure (AREA)
- Micromachines (AREA)
- Pressure Sensors (AREA)
Abstract
Description
Claims
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE112013003193.0T DE112013003193B4 (en) | 2012-06-28 | 2013-06-10 | Semiconductor package with an air pressure sensor |
| KR1020147033154A KR101693171B1 (en) | 2012-06-28 | 2013-06-10 | Semiconductor package with air pressure sensor |
| CN201380028085.8A CN104321868B (en) | 2012-06-28 | 2013-06-10 | Semiconductor package with air pressure sensor |
| JP2015515288A JP5869183B2 (en) | 2012-06-28 | 2013-06-10 | Semiconductor package having air pressure sensor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/536,210 | 2012-06-28 | ||
| US13/536,210 US9200973B2 (en) | 2012-06-28 | 2012-06-28 | Semiconductor package with air pressure sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2014004067A1 true WO2014004067A1 (en) | 2014-01-03 |
Family
ID=49776764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US2013/045026 Ceased WO2014004067A1 (en) | 2012-06-28 | 2013-06-10 | Semiconductor package with air pressure sensor |
Country Status (7)
| Country | Link |
|---|---|
| US (2) | US9200973B2 (en) |
| JP (1) | JP5869183B2 (en) |
| KR (1) | KR101693171B1 (en) |
| CN (1) | CN104321868B (en) |
| DE (1) | DE112013003193B4 (en) |
| TW (1) | TWI523191B (en) |
| WO (1) | WO2014004067A1 (en) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9200973B2 (en) | 2012-06-28 | 2015-12-01 | Intel Corporation | Semiconductor package with air pressure sensor |
| US8866287B2 (en) | 2012-09-29 | 2014-10-21 | Intel Corporation | Embedded structures for package-on-package architecture |
| US9429427B2 (en) | 2012-12-19 | 2016-08-30 | Intel Corporation | Inductive inertial sensor architecture and fabrication in packaging build-up layers |
| WO2015047257A1 (en) | 2013-09-25 | 2015-04-02 | Intel Corporation | Device, system and method for providing mems structures of a semiconductor package |
| US9791470B2 (en) * | 2013-12-27 | 2017-10-17 | Intel Corporation | Magnet placement for integrated sensor packages |
| US10305019B1 (en) | 2014-03-28 | 2019-05-28 | Intel Corporation | Piezoelectric devices fabricated in packaging build-up layers |
| CN105329837A (en) * | 2014-06-03 | 2016-02-17 | 中芯国际集成电路制造(上海)有限公司 | Semiconductor device and electronic device |
| US9541462B2 (en) * | 2014-08-29 | 2017-01-10 | Kionix, Inc. | Pressure sensor including deformable pressure vessel(s) |
| US9505607B2 (en) * | 2015-03-27 | 2016-11-29 | Intel Corporation | Methods of forming sensor integrated packages and structures formed thereby |
| US9559037B2 (en) * | 2015-06-02 | 2017-01-31 | Intel Corporation | Package integrated synthetic jet device |
| US20170026729A1 (en) * | 2015-07-23 | 2017-01-26 | Knowles Electronics, Llc | Microphone with pressure sensor |
| CN106612485B (en) * | 2015-10-23 | 2024-03-29 | 钰太芯微电子科技(上海)有限公司 | MEMS microphone and radio device |
| US10000373B2 (en) | 2016-01-27 | 2018-06-19 | Taiwan Semiconductor Manufacturing Co., Ltd. | Nano-electromechanical system (NEMS) device structure and method for forming the same |
| JP6908391B2 (en) * | 2017-02-17 | 2021-07-28 | アズビル株式会社 | Capacitive pressure sensor |
| EP3533386A1 (en) * | 2018-02-28 | 2019-09-04 | Koninklijke Philips N.V. | Pressure sensing with capacitive pressure sensor |
| US11131595B2 (en) * | 2019-07-26 | 2021-09-28 | Raytheon Technologies Corporation | Pressure sensing device and method for using the same |
| CN111473805B (en) * | 2020-04-17 | 2021-09-21 | 江苏多维科技有限公司 | Micro-electro-mechanical environment sensor and preparation method thereof |
| CN112161738B (en) * | 2020-09-17 | 2022-04-08 | 五邑大学 | Air pressure sensor and method of making the same |
| CN114582828B (en) * | 2020-11-30 | 2025-02-07 | 华为技术有限公司 | Packaging substrate and communication equipment |
| CN112723301B (en) * | 2020-12-21 | 2024-09-13 | 苏州长风航空电子有限公司 | High-frequency response pressure sensor chip for aviation and preparation method |
| CN113232031A (en) * | 2021-01-20 | 2021-08-10 | 北京航空航天大学 | Novel electronic skin with adjustable pressure sensing range |
| CN113125069A (en) * | 2021-03-10 | 2021-07-16 | 潍坊歌尔微电子有限公司 | Air pressure sensor chip and preparation method thereof |
| KR20240037025A (en) * | 2022-09-14 | 2024-03-21 | 삼성전자주식회사 | Integrated Circuit |
| DE102023109409B4 (en) * | 2023-04-14 | 2025-03-27 | Infineon Technologies Ag | Semiconductor package with floating metal part and method of manufacturing |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5883779A (en) * | 1994-11-24 | 1999-03-16 | Siemens Aktiengesellschaft | Pressure sensor |
| US20050132814A1 (en) * | 1999-08-20 | 2005-06-23 | Hitachi, Ltd. | Semiconductor pressure sensor and pressure sensing device |
| JP2006170785A (en) * | 2004-12-15 | 2006-06-29 | Kyocera Corp | Pressure detection device package, pressure detection device, and pressure sensitive element |
| KR20080101010A (en) * | 2007-05-15 | 2008-11-21 | (주)미코엠에스티 | Capacitive pressure sensor and its manufacturing method |
| US20090127590A1 (en) * | 2007-11-16 | 2009-05-21 | Seiko Epson Corporation | Micro electro mechanical device, method for manufacturing the same, semiconductor device, and method for manufacturing the same |
Family Cites Families (104)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3875502A (en) | 1973-05-24 | 1975-04-01 | Foerster Inst Dr Friedrich | Coil arrangement and circuit for eddy current testing |
| US3943557A (en) * | 1974-02-19 | 1976-03-09 | Plessey Incorporated | Semiconductor package with integral hermeticity detector |
| US4380041A (en) * | 1978-09-25 | 1983-04-12 | Motorola Inc. | Capacitor pressure transducer with housing |
| JPS6293668A (en) | 1985-10-21 | 1987-04-30 | Hitachi Ltd | Angular velocity/acceleration detector |
| JPH05240874A (en) | 1991-12-06 | 1993-09-21 | Canon Inc | Angular velocity sensor |
| JPH06350105A (en) | 1993-06-07 | 1994-12-22 | Nec Corp | Micromachine and its manufacture |
| JPH0720140A (en) | 1993-06-30 | 1995-01-24 | Toshiba Corp | Angular velocity sensor |
| US5364497A (en) | 1993-08-04 | 1994-11-15 | Analog Devices, Inc. | Method for fabricating microstructures using temporary bridges |
| US5698784A (en) | 1996-01-24 | 1997-12-16 | Gyration, Inc. | Vibratory rate gyroscope and methods of assembly and operation |
| JP3702412B2 (en) | 1996-07-29 | 2005-10-05 | アイシン精機株式会社 | Angular velocity detector |
| US5881963A (en) | 1998-03-19 | 1999-03-16 | Hinkle; David W. | Strap retractor |
| US6278379B1 (en) * | 1998-04-02 | 2001-08-21 | Georgia Tech Research Corporation | System, method, and sensors for sensing physical properties |
| JP3811304B2 (en) | 1998-11-25 | 2006-08-16 | 株式会社日立製作所 | Displacement sensor and manufacturing method thereof |
| US6501107B1 (en) | 1998-12-02 | 2002-12-31 | Microsoft Corporation | Addressable fuse array for circuits and mechanical devices |
| US6636826B1 (en) | 1998-12-17 | 2003-10-21 | Nec Tokin Corporation | Orientation angle detector |
| US6571631B1 (en) | 1999-03-05 | 2003-06-03 | Fdk Corporation | Displacement sensor and movement information collecting device comprising the same |
| US7541214B2 (en) | 1999-12-15 | 2009-06-02 | Chang-Feng Wan | Micro-electro mechanical device made from mono-crystalline silicon and method of manufacture therefore |
| JP2001194153A (en) | 2000-01-11 | 2001-07-19 | Matsushita Electric Ind Co Ltd | Angular velocity sensor, acceleration sensor and manufacturing method |
| DE10012960A1 (en) | 2000-03-16 | 2001-09-20 | Bosch Gmbh Robert | Micromechanical component for acceleration sensor, e.g. for motor vehicle, has adjustable sensitivity since spring constant can be adjusted in steps |
| US6510032B1 (en) | 2000-03-24 | 2003-01-21 | Littelfuse, Inc. | Integrated overcurrent and overvoltage apparatus for use in the protection of telecommunication circuits |
| DE10117486A1 (en) * | 2001-04-07 | 2002-10-17 | Bosch Gmbh Robert | Method for producing a semiconductor component and a semiconductor component produced using the method |
| US6635506B2 (en) | 2001-11-07 | 2003-10-21 | International Business Machines Corporation | Method of fabricating micro-electromechanical switches on CMOS compatible substrates |
| US7265429B2 (en) * | 2002-08-07 | 2007-09-04 | Chang-Feng Wan | System and method of fabricating micro cavities |
| US6860419B2 (en) | 2002-08-30 | 2005-03-01 | Agilent Technologies, Inc. | Apparatus and method for controlling movement of a device after packaging |
| US6919508B2 (en) | 2002-11-08 | 2005-07-19 | Flipchip International, Llc | Build-up structures with multi-angle vias for chip to chip interconnects and optical bussing |
| EP1450406A1 (en) | 2003-02-19 | 2004-08-25 | Cavendish Kinetics Limited | Micro fuse |
| JP2004301662A (en) | 2003-03-31 | 2004-10-28 | Tdk Corp | Gyroscopic sensor |
| TWI246761B (en) * | 2003-05-14 | 2006-01-01 | Siliconware Precision Industries Co Ltd | Semiconductor package with build-up layers formed on chip and fabrication method of the semiconductor package |
| JP4058378B2 (en) | 2003-05-16 | 2008-03-05 | Tdk株式会社 | Angular velocity sensor and angular velocity detector |
| US7586868B2 (en) | 2003-07-14 | 2009-09-08 | Motorola, Inc | Method and apparatus for controlling distributed transcoders |
| JP2005195574A (en) | 2003-10-20 | 2005-07-21 | Sony Corp | Angular velocity detection device, angular velocity detection method using angular velocity detection device, and method of manufacturing angular velocity detection device |
| JP2005159715A (en) | 2003-11-26 | 2005-06-16 | Seiko Epson Corp | Micro-resonator, manufacturing method thereof, and electronic device |
| US7464590B1 (en) | 2004-03-12 | 2008-12-16 | Thomson Licensing | Digitally programmable bandwidth for vibratory rate gyroscope |
| JP4676428B2 (en) | 2004-03-30 | 2011-04-27 | パイオニア株式会社 | Electron emission device, manufacturing method thereof, and imaging device or display device using electron emission device |
| US7178400B2 (en) | 2004-04-14 | 2007-02-20 | Denso Corporation | Physical quantity sensor having multiple through holes |
| KR100511926B1 (en) | 2004-04-29 | 2005-09-02 | 주식회사 하이닉스반도체 | Semiconductor chip package and method for forming the same |
| US7442918B2 (en) | 2004-05-14 | 2008-10-28 | Microvision, Inc. | MEMS device having simplified drive |
| DE102005041059B4 (en) | 2004-09-02 | 2014-06-26 | Denso Corporation | Angular rate sensor and mounting structure of an angular rate sensor |
| JP4487710B2 (en) | 2004-09-28 | 2010-06-23 | ヤマハ株式会社 | Sensor and method of measuring physical quantity using the same |
| TWI241695B (en) * | 2004-11-19 | 2005-10-11 | Ind Tech Res Inst | Structure of an electronic package and method for fabricating the same |
| JP2006229629A (en) | 2005-02-17 | 2006-08-31 | Seiko Epson Corp | Method for adjusting resonance frequency of vibrator and vibrator |
| CA2598186A1 (en) * | 2005-04-12 | 2006-10-19 | Cardiomems, Inc. | Electromagnetically coupled hermetic chamber |
| US20060231821A1 (en) | 2005-04-18 | 2006-10-19 | Troy Gavin | Gate for fence enclosures |
| EP1746648A3 (en) * | 2005-07-22 | 2008-09-03 | Marvell World Trade Ltd. | Packaging for high speed integrated circuits |
| US8335084B2 (en) * | 2005-08-01 | 2012-12-18 | Georgia Tech Research Corporation | Embedded actives and discrete passives in a cavity within build-up layers |
| US7528529B2 (en) | 2005-10-17 | 2009-05-05 | Semiconductor Energy Laboratory Co., Ltd. | Micro electro mechanical system, semiconductor device, and manufacturing method thereof |
| JP4895604B2 (en) * | 2005-12-22 | 2012-03-14 | 京セラ株式会社 | Pressure detection device package and pressure detection device |
| US7684051B2 (en) | 2006-04-18 | 2010-03-23 | Halliburton Energy Services, Inc. | Fiber optic seismic sensor based on MEMS cantilever |
| US7824943B2 (en) | 2006-06-04 | 2010-11-02 | Akustica, Inc. | Methods for trapping charge in a microelectromechanical system and microelectromechanical system employing same |
| WO2007147137A2 (en) | 2006-06-15 | 2007-12-21 | Sitime Corporation | Stacked die package for mems resonator system |
| JP4910512B2 (en) | 2006-06-30 | 2012-04-04 | 富士通セミコンダクター株式会社 | Semiconductor device and manufacturing method of semiconductor device |
| JP4215076B2 (en) | 2006-07-10 | 2009-01-28 | ヤマハ株式会社 | Condenser microphone and manufacturing method thereof |
| TWI301823B (en) | 2006-08-29 | 2008-10-11 | Ind Tech Res Inst | Package structure and packaging method of mems microphone |
| EP1908727A1 (en) | 2006-10-03 | 2008-04-09 | Seiko Epson Corporation | Wafer-level MEMS package and manufacturing method thereof |
| US20080142606A1 (en) | 2006-12-19 | 2008-06-19 | Ping-Chang Wu | E-fuse bar code structure and method of using the same |
| JP4850722B2 (en) * | 2007-01-05 | 2012-01-11 | ヒタチグローバルストレージテクノロジーズネザーランドビーブイ | Magnetic disk device, preamplifier for magnetic disk device, flexible printed cable assembly for magnetic disk device |
| TWI341002B (en) * | 2007-02-09 | 2011-04-21 | Unimicron Technology Corp | Coreless flip-chip packing substrate and method for making coreless packing substrate |
| US20090005157A1 (en) | 2007-06-28 | 2009-01-01 | Netley Neil J | Electronic funds transfer system and method of use in gaming environment |
| JP2009009067A (en) | 2007-06-29 | 2009-01-15 | Canon Inc | Oscillator device and manufacturing method thereof |
| WO2009022991A1 (en) | 2007-08-14 | 2009-02-19 | Agency For Science, Technology And Research | Die package and method for manufacturing the die package |
| TWI338941B (en) * | 2007-08-22 | 2011-03-11 | Unimicron Technology Corp | Semiconductor package structure |
| US7745892B1 (en) | 2007-12-13 | 2010-06-29 | Rf Micro Devices, Inc. | Integrated MEMS switch |
| US20090282917A1 (en) | 2008-05-19 | 2009-11-19 | Cenk Acar | Integrated multi-axis micromachined inertial sensing unit and method of fabrication |
| US8093704B2 (en) | 2008-06-03 | 2012-01-10 | Intel Corporation | Package on package using a bump-less build up layer (BBUL) package |
| JP4726927B2 (en) | 2008-06-19 | 2011-07-20 | 株式会社日立製作所 | Integrated microelectromechanical system and manufacturing method thereof |
| JP5345346B2 (en) | 2008-07-08 | 2013-11-20 | 株式会社日立製作所 | Mounting method of micro electro mechanical system |
| US8345895B2 (en) | 2008-07-25 | 2013-01-01 | United Microelectronics Corp. | Diaphragm of MEMS electroacoustic transducer |
| JP2010081758A (en) | 2008-09-26 | 2010-04-08 | Hoya Corp | Electrostatic type actuator |
| TW201019453A (en) | 2008-11-05 | 2010-05-16 | Windtop Technology Corp | MEMS package |
| US8148031B2 (en) | 2008-11-13 | 2012-04-03 | College Of William And Mary | Solid oxide proton conductor system and method of operating same for enhanced proton transport |
| JP2010155306A (en) | 2008-12-26 | 2010-07-15 | Panasonic Corp | Microelectromechanical systems (mems) device and method of manufacturing the same |
| US8304274B2 (en) | 2009-02-13 | 2012-11-06 | Texas Instruments Incorporated | Micro-electro-mechanical system having movable element integrated into substrate-based package |
| JP2010203857A (en) * | 2009-03-02 | 2010-09-16 | Alps Electric Co Ltd | Package structure of pressure sensor |
| US8215176B2 (en) * | 2009-05-27 | 2012-07-10 | Continental Automotive Systems, Inc. | Pressure sensor for harsh media sensing and flexible packaging |
| WO2011031256A1 (en) | 2009-09-09 | 2011-03-17 | Hewlett-Packard Development Company, L.P. | Gyroscopic input systems and methods |
| US8436700B2 (en) | 2009-09-18 | 2013-05-07 | Easic Corporation | MEMS-based switching |
| TWI444052B (en) * | 2009-12-17 | 2014-07-01 | Ind Tech Res Inst | Capacitive transducer and fabrication method |
| JP2011218462A (en) | 2010-04-06 | 2011-11-04 | Seiko Epson Corp | Mems device |
| JP5321538B2 (en) | 2010-06-14 | 2013-10-23 | 株式会社デンソー | Method for manufacturing mechanical quantity sensor |
| US8685778B2 (en) | 2010-06-25 | 2014-04-01 | International Business Machines Corporation | Planar cavity MEMS and related structures, methods of manufacture and design structures |
| US20110316140A1 (en) | 2010-06-29 | 2011-12-29 | Nalla Ravi K | Microelectronic package and method of manufacturing same |
| CN103221331B (en) | 2010-09-18 | 2016-02-03 | 快捷半导体公司 | Hermetic Packages for MEMS |
| TWI434802B (en) | 2010-12-23 | 2014-04-21 | Ind Tech Res Inst | Microelectromechanical device with electric insulating structure and manufacturing method thereof |
| US8878335B2 (en) | 2010-12-23 | 2014-11-04 | Infineon Technologies Ag | Method and system for providing fusing after packaging of semiconductor devices |
| US20120161258A1 (en) | 2010-12-28 | 2012-06-28 | Loeppert Peter V | Package with a cmos die positioned underneath a mems die |
| US8714239B2 (en) | 2011-04-27 | 2014-05-06 | Luis Phillipe TOSI | Flow-induced electrostatic power generator for downhole use in oil and gas wells |
| US8824706B2 (en) * | 2011-08-30 | 2014-09-02 | Qualcomm Mems Technologies, Inc. | Piezoelectric microphone fabricated on glass |
| EP2565153B1 (en) | 2011-09-02 | 2015-11-11 | Nxp B.V. | Acoustic transducers with perforated membranes |
| WO2013089673A1 (en) | 2011-12-13 | 2013-06-20 | Intel Corporation | Through-silicon via resonators in chip packages and methods of assembling same |
| WO2013101156A1 (en) | 2011-12-30 | 2013-07-04 | Intel Corporation | Integration of laminate mems in bbul coreless package |
| EP2637007B1 (en) * | 2012-03-08 | 2020-01-22 | ams international AG | MEMS capacitive pressure sensor |
| EP2658288B1 (en) | 2012-04-27 | 2014-06-11 | Nxp B.V. | Acoustic transducers with perforated membranes |
| US9200973B2 (en) | 2012-06-28 | 2015-12-01 | Intel Corporation | Semiconductor package with air pressure sensor |
| US8633551B1 (en) | 2012-06-29 | 2014-01-21 | Intel Corporation | Semiconductor package with mechanical fuse |
| US20140001583A1 (en) | 2012-06-30 | 2014-01-02 | Intel Corporation | Method to inhibit metal-to-metal stiction issues in mems fabrication |
| US9297824B2 (en) | 2012-09-14 | 2016-03-29 | Intel Corporation | Techniques, systems and devices related to acceleration measurement |
| US9674945B2 (en) | 2012-09-21 | 2017-06-06 | Intel Corporation | Heterogeneous integration of microfluidic devices in package structures |
| JP5892027B2 (en) * | 2012-10-11 | 2016-03-23 | 株式会社デンソー | Pressure sensor device and manufacturing method thereof |
| US9429427B2 (en) | 2012-12-19 | 2016-08-30 | Intel Corporation | Inductive inertial sensor architecture and fabrication in packaging build-up layers |
| US8692340B1 (en) | 2013-03-13 | 2014-04-08 | Invensense, Inc. | MEMS acoustic sensor with integrated back cavity |
| US9147663B2 (en) * | 2013-05-28 | 2015-09-29 | Intel Corporation | Bridge interconnection with layered interconnect structures |
| US10006823B2 (en) * | 2013-06-20 | 2018-06-26 | The Regents Of The University Of Michigan | Microdischarge-based transducer |
| US20150048515A1 (en) * | 2013-08-15 | 2015-02-19 | Chong Zhang | Fabrication of a substrate with an embedded die using projection patterning and associated package configurations |
| US9260294B2 (en) * | 2013-12-27 | 2016-02-16 | Intel Corporation | Integration of pressure or inertial sensors into integrated circuit fabrication and packaging |
-
2012
- 2012-06-28 US US13/536,210 patent/US9200973B2/en not_active Expired - Fee Related
-
2013
- 2013-06-10 WO PCT/US2013/045026 patent/WO2014004067A1/en not_active Ceased
- 2013-06-10 CN CN201380028085.8A patent/CN104321868B/en not_active Expired - Fee Related
- 2013-06-10 DE DE112013003193.0T patent/DE112013003193B4/en active Active
- 2013-06-10 JP JP2015515288A patent/JP5869183B2/en not_active Expired - Fee Related
- 2013-06-10 KR KR1020147033154A patent/KR101693171B1/en not_active Expired - Fee Related
- 2013-06-20 TW TW102121931A patent/TWI523191B/en not_active IP Right Cessation
-
2015
- 2015-11-24 US US14/951,422 patent/US10508961B2/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5883779A (en) * | 1994-11-24 | 1999-03-16 | Siemens Aktiengesellschaft | Pressure sensor |
| US20050132814A1 (en) * | 1999-08-20 | 2005-06-23 | Hitachi, Ltd. | Semiconductor pressure sensor and pressure sensing device |
| JP2006170785A (en) * | 2004-12-15 | 2006-06-29 | Kyocera Corp | Pressure detection device package, pressure detection device, and pressure sensitive element |
| KR20080101010A (en) * | 2007-05-15 | 2008-11-21 | (주)미코엠에스티 | Capacitive pressure sensor and its manufacturing method |
| US20090127590A1 (en) * | 2007-11-16 | 2009-05-21 | Seiko Epson Corporation | Micro electro mechanical device, method for manufacturing the same, semiconductor device, and method for manufacturing the same |
Also Published As
| Publication number | Publication date |
|---|---|
| US20140000377A1 (en) | 2014-01-02 |
| KR20150006862A (en) | 2015-01-19 |
| KR101693171B1 (en) | 2017-01-06 |
| JP5869183B2 (en) | 2016-02-24 |
| JP2015525344A (en) | 2015-09-03 |
| US10508961B2 (en) | 2019-12-17 |
| US9200973B2 (en) | 2015-12-01 |
| CN104321868A (en) | 2015-01-28 |
| TWI523191B (en) | 2016-02-21 |
| CN104321868B (en) | 2017-05-17 |
| DE112013003193B4 (en) | 2022-02-10 |
| TW201413914A (en) | 2014-04-01 |
| US20160076961A1 (en) | 2016-03-17 |
| DE112013003193T5 (en) | 2015-03-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10508961B2 (en) | Semiconductor package with air pressure sensor | |
| US8633551B1 (en) | Semiconductor package with mechanical fuse | |
| US9345184B2 (en) | Magnetic field shielding for packaging build-up architectures | |
| JP6199322B2 (en) | Method for embedding a controlled cavity MEMS package in an integrated board | |
| US9501068B2 (en) | Integration of pressure sensors into integrated circuit fabrication and packaging | |
| US10179729B2 (en) | Hermetic encapsulation for microelectromechanical systems (MEMS) devices | |
| CN104995130B (en) | The structure for forming the method for the microelectromechanical structure buried coupled with device substrate and being consequently formed | |
| TW201307183A (en) | Thin metal shield on electronic devices | |
| US9505610B2 (en) | Device, system and method for providing MEMS structures of a semiconductor package | |
| KR20170131373A (en) | METHOD FOR MANUFACTURING SENSOR INTEGRATED PACKAGE | |
| CN102234098B (en) | Manufacturing method of micro electromechanical structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 13809474 Country of ref document: EP Kind code of ref document: A1 |
|
| ENP | Entry into the national phase |
Ref document number: 20147033154 Country of ref document: KR Kind code of ref document: A |
|
| ENP | Entry into the national phase |
Ref document number: 2015515288 Country of ref document: JP Kind code of ref document: A |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 1120130031930 Country of ref document: DE Ref document number: 112013003193 Country of ref document: DE |
|
| 122 | Ep: pct application non-entry in european phase |
Ref document number: 13809474 Country of ref document: EP Kind code of ref document: A1 |