WO1998033195A1 - Cantilevered microstructure - Google Patents

Cantilevered microstructure Download PDF

Info

Publication number
WO1998033195A1
WO1998033195A1 PCT/IB1998/000344 IB9800344W WO9833195A1 WO 1998033195 A1 WO1998033195 A1 WO 1998033195A1 IB 9800344 W IB9800344 W IB 9800344W WO 9833195 A1 WO9833195 A1 WO 9833195A1
Authority
WO
WIPO (PCT)
Prior art keywords
cantilever
layer
section
tce
cantilever arm
Prior art date
Application number
PCT/IB1998/000344
Other languages
French (fr)
Inventor
William N. Carr
Xi-Qing Sun
Original Assignee
Roxburgh Ltd.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Roxburgh Ltd. filed Critical Roxburgh Ltd.
Publication of WO1998033195A1 publication Critical patent/WO1998033195A1/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H1/00Contacts
    • H01H1/0036Switches making use of microelectromechanical systems [MEMS]
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H61/00Electrothermal relays
    • H01H61/02Electrothermal relays wherein the thermally-sensitive member is heated indirectly, e.g. resistively, inductively
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H1/00Contacts
    • H01H1/0036Switches making use of microelectromechanical systems [MEMS]
    • H01H2001/0042Bistable switches, i.e. having two stable positions requiring only actuating energy for switching between them, e.g. with snap membrane or by permanent magnet
    • H01H2001/0047Bistable switches, i.e. having two stable positions requiring only actuating energy for switching between them, e.g. with snap membrane or by permanent magnet operable only by mechanical latching
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H1/00Contacts
    • H01H1/0036Switches making use of microelectromechanical systems [MEMS]
    • H01H2001/0063Switches making use of microelectromechanical systems [MEMS] having electrostatic latches, i.e. the activated position is kept by electrostatic forces other than the activation force
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H61/00Electrothermal relays
    • H01H2061/006Micromechanical thermal relay

Definitions

  • This invention relates to microstructures that are constructed utilizing semiconductor fabrication processes and, more particularly, to a cantilevered microstructure produced in accordance with such semiconductor processes .
  • Silicon "micromachining” has been developed as a means for accurately fabricating small structures . Such processing involves the selective etching of a silicon substrate and the deposition thereon of thin film layers of semiconductor materials. Various sacrificial layers are employed to enable the fabrication of relatively complex interactive structures .
  • Silicon micromachining has been applied to the fabrication of micromachines that include rotary and linear bearings. Such bearings have spawned further development of electrically-driven motors which exhibit a planar geometry and lateral dimensions on the order of 100 microns or so. In addition to micromotors, various microactuators have also been constructed utilizing micromachining concepts .
  • Figs . la and lb illustrate a prior art cantilever device wherein a polysilicon layer 10 is bonded to a layer 12 of different composition. Both layers are bonded, at one extremity, to a substrate 14.
  • the thermal coefficients of expansion of polysilicon layer 10 and layer 12 are chosen as to be sufficiently different that, without an applied potential to create a heating action, the structure exhibits an arcuate form as shown in Fig. la.
  • a voltage Vt is applied between layers 10 and 12 and current flow causes a heating of the layers, unequal expansion results in a clockwise rotation of the arm until contact is made with substrate contact region 16.
  • thermal actuator comprising a sandwich of polysilicon and gold
  • CMOS Electrothermal Microactuators Parameswaran et al . , Proceedings IEEE Microelectro-Mechanical Systems, 11-14 February 1990, pages 131.
  • cantilever arms have also been constructed using piezoelectric films which exhibit a large d 31 characteristic.
  • a piezoelectric film 20 has been sandwiched between a pair of electrodes 22 and 24 and coupled in a cantilever fashion to a contact 26.
  • Application of a voltage Vpz between electrodes 22 and 24 causes a flexure of piezoelectric film 20 (see Fig. 2b) , resulting in a counter-clockwise rotation of the cantilever arm and a disconnection of an electrical pathway between contacts 26 and 28.
  • Piezoelectrically actuated cantilever microdevices have been proposed for a variety of applications.
  • Such cantilever structures enable the redirection of an incident light beam to create an optical switching effect .
  • a cantilever arm 29 comprises a polysilicon layer 30 affixed to an insulating layer 32 and spans substrate contacts 34 and 36.
  • Vs voltage
  • an electrostatic force is created which provides a hold-down action between free end 37 of cantilever arm 29 and substrate contact 36.
  • Electrostatic actuation has also been employed to control the action of a microshutter, wherein a moving electrode of aluminum, chromium, gold or doped polysilicon and a fixed counter electrode is employed. The deflection of the moving electrode is controlled by electrostatic forces. The moving electrode rotates about an axis and employs a torsional-cantilever action. (See “Electrostatically Activated Micro-Shutter in (110) Silicon", DSC-Volume 40, Micromechanical Systems ASME, 1992, pages 13-22.
  • a cantilever microstructure includes a cantilever arm with a proximal end connected to a substrate and a freely movable distal end.
  • the cantilever arm comprises first and second sections and includes a continuous layer which exhibits a first thermal co-efficient of expansion (TCE) .
  • TCE thermal co-efficient of expansion
  • an electrical contact is positioned at the distal end of the cantilever arm.
  • a first layer is positioned on a surface of the continuous layer and along the first section thereof.
  • the first layer exhibits a second TCE which is different from the first TCE of the continuous layer.
  • a second layer is positioned on a surface of the continuous layer and along the second section thereof .
  • the second layer exhibits a third TCE which is different from the first TCE of the continuous layer.
  • Electrical control circuitry selectively applies signals to the first and second layers to cause a heating thereof and a flexure of the cantilever arm so as to bring the distal end thereof into contact with a conductive substrate .
  • Fig. la is a schematic view of a prior art, thermally actuated cantilever microstructure in an open position.
  • Fig. lb is a schematic view of the thermally actuated cantilever microstructure of Fig. la in the closed position.
  • Fig. 2a is a schematic view of a prior art, piezoelectrically actuated cantilever microstructure in the closed position.
  • Fig. 2b is a schematic view of the prior art cantilever microstructure of Fig. 2a in the open position .
  • Fig. 3 illustrates a prior art microcantilever which utilizes an electrostatic potential to provide a hold- down force .
  • Fig. 4 is a schematic illustration of a microcantilever structure incorporating the invention hereof .
  • Fig. 5 is a plan view of a microcantilever structure employing the invention.
  • Fig. 6 is a schematic side view of the microcantilever structure of Fig. 5.
  • Figs, la- le illustrate a sequence of schematic views useful in understanding the operation of the microcantilever structure of Figs. 5 and 6.
  • Fig. 8 illustrates application of a microcantilever structure, such as shown in Fig. 4, to the movement of a platform structure.
  • Figs. 9a and 9b illustrate application of a microcantilever incorporating the invention hereof to an optical shutter.
  • Fig. 10 is a schematic view of a piezoelectrically-controlled cantilever microstructure incorporating the invention hereof.
  • Fig. 4 is a schematic of a multi-segment microcantilever incorporating the invention hereof.
  • a silicon substrate 50 supports a multi-segment microcantilever 52 that is electrothermally actuated.
  • a continuous film 54 forms the central structure of microcantilever 52 and exhibits a first thermal coefficient of expansion (TCE) .
  • Microcantilever 52 is segmented into two sections 55 and 57. In section 55, a film 56, exhibiting a dissimilar TCE to that of continuous film 54 is bonded to continuous film 54.
  • Section 57 of microcantilever 52 includes a film 58 which is bonded to continuous film 54, but on an opposite surface thereof from film 56. Film 58 may be comprised of the same material as film 56, or may be a different film and can exhibit a still-different TCE from that of films 56 and 54.
  • a resistive layer 60 is positioned on film 56 and a resistive layer 62 is positioned on film 58.
  • the unheated position of sections 55 and 57 can be controlled to be either clockwise or counterclockwise, using known process technologies, i.e., annealing.
  • Application of voltage VI to resistive film 60 causes a heating of underlying films 56 and 54 and an expansion of both thereof. Their unequal TCE's cause, for example, a clockwise rotation of section 55 of microcantilever 52.
  • an application of a voltage V2 to resistive film 62 causes a thermal heating of films 58 and 54, an expansion of both thereof and, for example, a counter-clockwise rotation of section 57 of microcantilever 52.
  • a multiplicity of movements of microcantilever 52 can be achieved which enable a both physical latching action and an electrical contact to be accomplished at the distal end 64 of microcantilever 52.
  • the microcantilever of Fig. 4 is preferably produced using known micromachining/silicon processing procedures.
  • the structure of Fig. 4 can be produced using either a low temperature or high temperature process (i.e. 300°C or 850°C maximum temperatures, respectively) .
  • the low temperature process is compatible with CMOS VLSI processes.
  • aluminum is preferably utilized as a sacrificial layer;
  • continuous film 54 is P- doped amorphous silicon and films 56 and 58 are low temperature thermal oxides such as silicon dioxide.
  • Substrate 50 is a monocrystalline silicon substrate and supports continuous silicon film 54 in a cantilever fashion.
  • a low temperature thermal oxide is employed as the sacrificial layer (s)
  • films 56 and 58 are comprised of silicon nitride
  • film 54 comprises a P- doped polysilicon material.
  • Resistive heater layers 60 and 62 may also be comprised of P-doped polysilicon.
  • Films 56 and 58 may be semiconductive films to enable elimination of resistive films 60 and 62.
  • a further option is to utilize a high resistivity polysilicon film layer 54 (initially undoped) that is processed to include a diffused or implanted heater pattern.
  • a microcantilever structure 70 which performs an electrical switching function between a pair of contacts 71 and 72.
  • Microcantilever 70 accomplishes not only physical latching and electrical contact actions bu ⁇ also manifests an electrostatic hold-down capability. Note that the side view of Fig. 6 only illustrates some of the layers utilized in microcantilever 70 of Fig. 5, to avoid over-complication of the view.
  • microcantilever 70 which perform the same functions as schematic microcantilever 52 shown in Fig. 4 are numbered the same.
  • Microcantilever 70 comprises a central film 54 -(e.g. silicon) , with dielectric films 56 and 58 positioned on opposed surfaces thereof. Resistive layers 60 and 62 (see Fig. 6) are shown schematically in Fig. 5. A conductive layer 74 is continuous about the periphery of the upper surface of microcantilever 70 and is utilized for electrostatic hold-down purposes . The mid-portion of microcantilever 70 exhibits a pair of extended regions 80 to provide additional stability and position control during flexure of microcantilever 70.
  • a central film 54 -(e.g. silicon)
  • Resistive layers 60 and 62 are shown schematically in Fig. 5.
  • a conductive layer 74 is continuous about the periphery of the upper surface of microcantilever 70 and is utilized for electrostatic hold-down purposes .
  • the mid-portion of microcantilever 70 exhibits a pair of extended regions 80 to provide additional stability and position control during flexure of microcantilever 70.
  • a conductive bar 76 which, when in contact with contacts 71 and 72, creates a short circuit therebetween.
  • Contacts 71 and 72 may be insulated from silicon substrate 50 by intervening insulation regions or may be in contact with structures integrated into substrate 50.
  • the interface surfaces between contacts 71, 72 and conductive bar 76 exhibit a roughened condition so as to assure good electrical and physical contact therebetween. Such roughened surfaces assure that, when engaged, conductive bar 76 remains engaged with contacts 71 and 72 until proper voltages are applied to cause a disengagement thereof .
  • the roughened surfaces may exhibit roughness structures ranging from atomic dimensions to mask-defined dimensions of a few micrometers .
  • a controller 78 (which may, for instance, be a microprocessor) provides output voltages which control (i) the application of heater currents to resistive layers 60 and 62 and (ii) an electrostatic hcld-down voltage between conductor 74 and substrate 50. (Note that electrostatic hold-down conductor 74 is not shown in Figs , n? or (, ) .
  • Figs. 7a-7e schematically illustrate the operation of microcantilever 70, in transitioning from an unlatched state to a latched state, wherein conductor bar 76 creates a short circuit between contacts 71 and 72.
  • controller 78 has turned off energizing currents to resistive layers 60 and 62. Under these conditions, sections 55 and 57 of microcantilever 70 are unheated and conductive bar 76 remains out of contact with contacts 71 and 72.
  • controller 78 initially applies voltage V2 to resistive layer 62, causing a heating thereof and an expansion of films 54 and 58. Because of the differing TCE's between films 54 and 58, a counter-clockwise rotation occurs of section 57 of microcantilever 70 (Fig. 7b) .
  • controller 78 applies voltage VI to resistive layer 60 and continues application of voltage V2 to resistive layer 62.
  • the result is as shown in Fig. 7c wherein section 55 of microcantilever 70 is caused to rotate in a clockwise direction, causing a downward movement of conductor bar 76.
  • controller 78 removes voltage V2 from resistive layer 62, while continuing application of voltage VI to resistive layer 60.
  • layers 54 and 58 cool, the differential contraction therebetween causes a clockwise rotation of section 57 of microcantilever 70 until the roughened posterior edge of conductor bar 76 contacts the roughened frontal edge of contact 72.
  • microcantilever 70 enable a secure latching action to be achieved and assures excellent electrical connection between contact 71, 72 by conductor bar 76.
  • the multiple motions achievable from control of microcantilever 70 can also be utilized for a variety of other applications.
  • microcantilever 70 to perform a physical movement of a platform.
  • a plurality of microcantilevers 70 are fabricated on silicon substrate 80 in a reverse orientation to that shown in Figs.4-6.
  • a platform 82 which is movable in a lateral direction.
  • projections 84 which are adapted to interact with microcantilevers 70, when each thereof is actuated.
  • Platform 82 may be spring biased to the right, which spring bias is overcome by the action of microcantilevers 70.
  • protrusions 84 are not needed and friction between the cantilevers and the wafer permits positioning thereof.
  • Fig. 8 The action of the structure of Fig. 8 enables precise 3-D control of a "microplatform" .
  • the vertical height of platform 82 can be adjusted and maintained.
  • both x and y lateral movements of platform 82 are implemented as described above .
  • Figs. 9a and 9b illustrate the use of microcantilevers 70 as shutters in an optical gating structure 90.
  • light incident along direction 92 can either be passed through optical gating structure 90 or be blocked thereby.
  • the multi-section arrangement of each of microcantilevers 70 enables the movement thereof out of the respective light pathways, thereby enabling a maximum amount of light to pass therethrough. While each of microcantilevers 70 is shown in Fig. 9b as being simultaneously actuated, those skilled in the art will understand that individual microcantilevers 70 can be selectively controlled so as to either open a light pathway or not, in dependence upon the voltages supplied via a connected controller. Thus, one or more apertures can be caused to pass light and the remaining apertures can be in a shut state, in dependence upon a particularly desired control scheme.
  • a microcantilever 100 employs piezoelectric/electrostrictive layers to achieve a wide range of motions that are similar to those achieved by the electrothermally actuated microcantilevers described above.
  • a piezoelectric/electrostrictive film 102 includes a first section and a second section, the first section being sandwiched by a pair of electrodes 104, 106 and the second section by a pair of electrodes 108 and 110. Electrodes 104 and 106 are connected to a source of control voltage VI, and electrodes 108 and 110 are connected to a source of control voltage V2.
  • Electrodes 104, 106 and 108, 110 By reversing the respective potentials applied to electrodes 104, 106 and 108, 110, opposite directions of movement can be achieved. Additional electrode films can be added to the structure of Fig. 10 to add electrostatic pulldown action. Further, thermally heated films can be added to the structure of Fig. 10 to provide movement control. Other than the fact that actuator 100 is operated by piezoelectric/electrostrictive actions, its movements can be controlled in substantially the same manner as the electrothermally actuated microactuator described above.

Abstract

A cantilever microstructure includes a cantilever arm with a proximal end connected to a substrate and a freely movable distal end. The cantilever arm comprises first and second sections and includes a continuous layer which exhibits a first thermal co-efficient of expansion (TCE). In one embodiment, an electrical contact is positioned at the distal end of the cantilever arm. A first layer is positioned on a surface of the continuous layer and along the first section thereof. The first layer exhibits a second TCE which is different from the first TCE of the continuous layer. A second layer is positioned on a surface of the continuous layer and along the second section thereof. The second layer exhibits a third TCE which is different from the first TCE of the continuous layer. Electrical control circuitry selectively applies signals to the first and second layers to cause a heating thereof and a flexure of the cantilever arm so as to bring the distal end thereof into contact with a conductive substrate.

Description

Caritilevered Microstrueture
FIELD OF THE INVENTION
This invention relates to microstructures that are constructed utilizing semiconductor fabrication processes and, more particularly, to a cantilevered microstructure produced in accordance with such semiconductor processes .
BACKGROUND OF THE INVENTION
Silicon "micromachining" has been developed as a means for accurately fabricating small structures . Such processing involves the selective etching of a silicon substrate and the deposition thereon of thin film layers of semiconductor materials. Various sacrificial layers are employed to enable the fabrication of relatively complex interactive structures .
Silicon micromachining has been applied to the fabrication of micromachines that include rotary and linear bearings. Such bearings have spawned further development of electrically-driven motors which exhibit a planar geometry and lateral dimensions on the order of 100 microns or so. In addition to micromotors, various microactuators have also been constructed utilizing micromachining concepts .
Figs . la and lb illustrate a prior art cantilever device wherein a polysilicon layer 10 is bonded to a layer 12 of different composition. Both layers are bonded, at one extremity, to a substrate 14. The thermal coefficients of expansion of polysilicon layer 10 and layer 12 are chosen as to be sufficiently different that, without an applied potential to create a heating action, the structure exhibits an arcuate form as shown in Fig. la. When, as shown in Fig. lb, a voltage Vt is applied between layers 10 and 12 and current flow causes a heating of the layers, unequal expansion results in a clockwise rotation of the arm until contact is made with substrate contact region 16.
The action of the cantilever structure of Figs la and lb is much the same as a well known bi-metal thermal actuator widely used in thermostats. Further details of such structures can be found in "Thermally Excited Silicon Microactuators" , Riethmuller et al . , IEEE Transactions on Electron Devices, Volume 35, No. 6, June 1988, pages 758-763, and in "Design, Fabrication and Testing of a C-Shape Actuator", Lin et al . , Proceedings Eighth International Conference on Solid State Sensors and Actuators, Stockholm, Sweden, June 25-29, 1995, pages 418-420.
A further example of a thermal actuator comprising a sandwich of polysilicon and gold can be found described in "CMOS Electrothermal Microactuators", Parameswaran et al . , Proceedings IEEE Microelectro-Mechanical Systems, 11-14 February 1990, pages 131.
As shown in Figs. 2a and 2b, cantilever arms have also been constructed using piezoelectric films which exhibit a large d31 characteristic. Such a piezoelectric film 20 has been sandwiched between a pair of electrodes 22 and 24 and coupled in a cantilever fashion to a contact 26. Application of a voltage Vpz between electrodes 22 and 24 causes a flexure of piezoelectric film 20 (see Fig. 2b) , resulting in a counter-clockwise rotation of the cantilever arm and a disconnection of an electrical pathway between contacts 26 and 28.
In lieu of constructing a cantilever arm having an unattached free end, other prior art has employed a "tied-down" cantilever structure to provide a buckling action upon actuation by either a piezoelectric force or by a thermally actuated, differential expansion action. For instance, see "A Quantitative Analysis of Scratch Drive Actuator Buckling Motion", Akiyama et al . , Proceedings IEEE Micro-Electromechanical Systems, January 29-February 2, 1995, pages 310-315. A further version of such a buckling system is described in "Lateral In-plane Displacement Microactuators with Combined Thermal and Electrostatic Drive", Sun et al . , Solid-State Sensor and Actuator Workshop, Hilton Head, June 3-6, 1996, pages 31- 35.
Piezoelectrically actuated cantilever microdevices have been proposed for a variety of applications. Huang et al . in "Piezoelectrically Actuated Microcantilever for Actuated Mirror Array Application", Solid-State Sensor and Actuator Workshop, Hiltonhead Island, South Carolina, June 3-6, pages 191-195, have suggested the use of a piezoelectrically actuated cantilever structure for controlling the orientation of micro-mirrors. Such cantilever structures enable the redirection of an incident light beam to create an optical switching effect .
The application of electrostatic forces to provide both pull-down and repulsive forces in microactuators is known. Such a structure is shown in Fig. 3, wherein a cantilever arm 29 comprises a polysilicon layer 30 affixed to an insulating layer 32 and spans substrate contacts 34 and 36. When a voltage Vs is applied between contact 36 and across layers 30 and 32, an electrostatic force is created which provides a hold-down action between free end 37 of cantilever arm 29 and substrate contact 36.
Various electrostatically actuated devices can be found described in "Pull-in Dynamics of Electrostatically Actuated Beams", Gupta et al . , Poster Session Supplemental Digest, Solid-State Sensor and Actuator Workshop, Hiltonhead Island, South Carolina, June 3-6, 1996 , pages 1 , 2 .
Electrostatic actuation has also been employed to control the action of a microshutter, wherein a moving electrode of aluminum, chromium, gold or doped polysilicon and a fixed counter electrode is employed. The deflection of the moving electrode is controlled by electrostatic forces. The moving electrode rotates about an axis and employs a torsional-cantilever action. (See "Electrostatically Activated Micro-Shutter in (110) Silicon", DSC-Volume 40, Micromechanical Systems ASME, 1992, pages 13-22.
The prior art devices described above, while utilizing both thermal and piezoelectrically-controlled actuation, exhibit limited ranges of motion of the free ends of the cantilever arms. Such limitations restrict the application of the devices, notwithstanding their inherently low cost.
Accordingly, it is an object of this invention to provide an improved microactuator that exhibits extended ranges of movement of the actuating member.
It is another object of this invention to provide an improved microactuator which employs thermal actuation to accomplish movement of the actuating member.
It is another object of this invention to provide an improved microactuator that employs piezoelectric control to accomplish movement of the actuating member.
It is yet another object of this invention to provide a micromachined actuator which can be utilized for optical shuttering, control of a movable platform, and other applications. SUMMARY OF THE INVENTION
A cantilever microstructure includes a cantilever arm with a proximal end connected to a substrate and a freely movable distal end. The cantilever arm comprises first and second sections and includes a continuous layer which exhibits a first thermal co-efficient of expansion (TCE) . In one embodiment, an electrical contact is positioned at the distal end of the cantilever arm. A first layer is positioned on a surface of the continuous layer and along the first section thereof. The first layer exhibits a second TCE which is different from the first TCE of the continuous layer. A second layer is positioned on a surface of the continuous layer and along the second section thereof . The second layer exhibits a third TCE which is different from the first TCE of the continuous layer. Electrical control circuitry selectively applies signals to the first and second layers to cause a heating thereof and a flexure of the cantilever arm so as to bring the distal end thereof into contact with a conductive substrate .
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. la is a schematic view of a prior art, thermally actuated cantilever microstructure in an open position.
Fig. lb is a schematic view of the thermally actuated cantilever microstructure of Fig. la in the closed position.
Fig. 2a is a schematic view of a prior art, piezoelectrically actuated cantilever microstructure in the closed position.
Fig. 2b is a schematic view of the prior art cantilever microstructure of Fig. 2a in the open position .
Fig. 3 illustrates a prior art microcantilever which utilizes an electrostatic potential to provide a hold- down force .
Fig. 4 is a schematic illustration of a microcantilever structure incorporating the invention hereof .
Fig. 5 is a plan view of a microcantilever structure employing the invention.
Fig. 6 is a schematic side view of the microcantilever structure of Fig. 5.
Figs, la- le illustrate a sequence of schematic views useful in understanding the operation of the microcantilever structure of Figs. 5 and 6.
Fig. 8 illustrates application of a microcantilever structure, such as shown in Fig. 4, to the movement of a platform structure.
Figs. 9a and 9b illustrate application of a microcantilever incorporating the invention hereof to an optical shutter.
Fig. 10 is a schematic view of a piezoelectrically- controlled cantilever microstructure incorporating the invention hereof.
DETAILED DESCRIPTION OF THE INVENTION
Fig. 4 is a schematic of a multi-segment microcantilever incorporating the invention hereof. A silicon substrate 50 supports a multi-segment microcantilever 52 that is electrothermally actuated. A continuous film 54 forms the central structure of microcantilever 52 and exhibits a first thermal coefficient of expansion (TCE) . Microcantilever 52 is segmented into two sections 55 and 57. In section 55, a film 56, exhibiting a dissimilar TCE to that of continuous film 54 is bonded to continuous film 54. Section 57 of microcantilever 52 includes a film 58 which is bonded to continuous film 54, but on an opposite surface thereof from film 56. Film 58 may be comprised of the same material as film 56, or may be a different film and can exhibit a still-different TCE from that of films 56 and 54.
A resistive layer 60 is positioned on film 56 and a resistive layer 62 is positioned on film 58. The unheated position of sections 55 and 57 can be controlled to be either clockwise or counterclockwise, using known process technologies, i.e., annealing. Application of voltage VI to resistive film 60 causes a heating of underlying films 56 and 54 and an expansion of both thereof. Their unequal TCE's cause, for example, a clockwise rotation of section 55 of microcantilever 52. In a similar vein, an application of a voltage V2 to resistive film 62 causes a thermal heating of films 58 and 54, an expansion of both thereof and, for example, a counter-clockwise rotation of section 57 of microcantilever 52. By selective application of voltages VI and V2 , a multiplicity of movements of microcantilever 52 can be achieved which enable a both physical latching action and an electrical contact to be accomplished at the distal end 64 of microcantilever 52.
The microcantilever of Fig. 4 is preferably produced using known micromachining/silicon processing procedures. The structure of Fig. 4 can be produced using either a low temperature or high temperature process (i.e. 300°C or 850°C maximum temperatures, respectively) . The low temperature process is compatible with CMOS VLSI processes. Under such conditions, aluminum is preferably utilized as a sacrificial layer; continuous film 54 is P- doped amorphous silicon and films 56 and 58 are low temperature thermal oxides such as silicon dioxide. Substrate 50 is a monocrystalline silicon substrate and supports continuous silicon film 54 in a cantilever fashion.
If it is desired to configure the microstructure of Fig. 4 for actuation by application of heat, utilizing the high temperature process (i.e. 850°C maximum temperature) , then a low temperature thermal oxide is employed as the sacrificial layer (s), films 56 and 58 are comprised of silicon nitride, and film 54 comprises a P- doped polysilicon material. Resistive heater layers 60 and 62 may also be comprised of P-doped polysilicon. Films 56 and 58 may be semiconductive films to enable elimination of resistive films 60 and 62. A further option is to utilize a high resistivity polysilicon film layer 54 (initially undoped) that is processed to include a diffused or implanted heater pattern.
In Fig. 5, a microcantilever structure 70 is illustrated which performs an electrical switching function between a pair of contacts 71 and 72. Microcantilever 70 accomplishes not only physical latching and electrical contact actions bu~ also manifests an electrostatic hold-down capability. Note that the side view of Fig. 6 only illustrates some of the layers utilized in microcantilever 70 of Fig. 5, to avoid over-complication of the view.
In Figs. 5 and 6, portions of microcantilever 70 which perform the same functions as schematic microcantilever 52 shown in Fig. 4 are numbered the same.
Microcantilever 70 comprises a central film 54 -(e.g. silicon) , with dielectric films 56 and 58 positioned on opposed surfaces thereof. Resistive layers 60 and 62 (see Fig. 6) are shown schematically in Fig. 5. A conductive layer 74 is continuous about the periphery of the upper surface of microcantilever 70 and is utilized for electrostatic hold-down purposes . The mid-portion of microcantilever 70 exhibits a pair of extended regions 80 to provide additional stability and position control during flexure of microcantilever 70.
At the distal end of microcantilever 70 is positioned a conductive bar 76 which, when in contact with contacts 71 and 72, creates a short circuit therebetween. Contacts 71 and 72 may be insulated from silicon substrate 50 by intervening insulation regions or may be in contact with structures integrated into substrate 50.
It is preferred that the interface surfaces between contacts 71, 72 and conductive bar 76 exhibit a roughened condition so as to assure good electrical and physical contact therebetween. Such roughened surfaces assure that, when engaged, conductive bar 76 remains engaged with contacts 71 and 72 until proper voltages are applied to cause a disengagement thereof . The roughened surfaces may exhibit roughness structures ranging from atomic dimensions to mask-defined dimensions of a few micrometers .
A controller 78 (which may, for instance, be a microprocessor) provides output voltages which control (i) the application of heater currents to resistive layers 60 and 62 and (ii) an electrostatic hcld-down voltage between conductor 74 and substrate 50. (Note that electrostatic hold-down conductor 74 is not shown in Figs, n? or (, ) .
Figs. 7a-7e schematically illustrate the operation of microcantilever 70, in transitioning from an unlatched state to a latched state, wherein conductor bar 76 creates a short circuit between contacts 71 and 72. Initially, in Fig. 7a, controller 78 has turned off energizing currents to resistive layers 60 and 62. Under these conditions, sections 55 and 57 of microcantilever 70 are unheated and conductive bar 76 remains out of contact with contacts 71 and 72. To create a latching action, controller 78 initially applies voltage V2 to resistive layer 62, causing a heating thereof and an expansion of films 54 and 58. Because of the differing TCE's between films 54 and 58, a counter-clockwise rotation occurs of section 57 of microcantilever 70 (Fig. 7b) .
Next, controller 78 applies voltage VI to resistive layer 60 and continues application of voltage V2 to resistive layer 62. The result is as shown in Fig. 7c wherein section 55 of microcantilever 70 is caused to rotate in a clockwise direction, causing a downward movement of conductor bar 76. Thereafter (Fig 7d) , controller 78 removes voltage V2 from resistive layer 62, while continuing application of voltage VI to resistive layer 60. As layers 54 and 58 cool, the differential contraction therebetween causes a clockwise rotation of section 57 of microcantilever 70 until the roughened posterior edge of conductor bar 76 contacts the roughened frontal edge of contact 72.
Thereafter (Fig. 7e) , power is removed from the section 55 of microcantilever 70 and the resulting clockwise movement thereof causes conductor bar 76 to be drawn against contacts 71 and 72 into a "latched" condition. To unlatch microcantilever 70 from contacts 71 and 72, the procedure is reversed, as shown in Figs. 7e- 7a.
From the above description, it can be seen that the individually controllable movements of sections 55 and 57 of microcantilever 70 enable a secure latching action to be achieved and assures excellent electrical connection between contact 71, 72 by conductor bar 76. The multiple motions achievable from control of microcantilever 70 can also be utilized for a variety of other applications.
In Fig. 8, the use of microcantilever 70 to perform a physical movement of a platform is illustrated. ' A plurality of microcantilevers 70 are fabricated on silicon substrate 80 in a reverse orientation to that shown in Figs.4-6. Immediately above silicon substrate 80 is a platform 82 which is movable in a lateral direction. In one embodiment, jutting down from the underside of platform 82 are a plurality of projections 84 which are adapted to interact with microcantilevers 70, when each thereof is actuated. By applying appropriate heater voltages to the sections of each of microcantilevers 70, they are collectively caused to rotate in a counterclockwise direction and to engage protrusions 84. Such engagement causes a movement to the left of platform 82 by an amount that is dependent upon the amount of movement of each of microcantilevers 70. Platform 82 may be spring biased to the right, which spring bias is overcome by the action of microcantilevers 70. In other applications, such as for the positioning of silicon wafer disks, protrusions 84 are not needed and friction between the cantilevers and the wafer permits positioning thereof.
The action of the structure of Fig. 8 enables precise 3-D control of a "microplatform" . In accordance with the level of energy applied, respectively, to the sections of each of microcantilevers 70, the vertical height of platform 82 can be adjusted and maintained. In addition, both x and y lateral movements of platform 82 are implemented as described above .
Figs. 9a and 9b illustrate the use of microcantilevers 70 as shutters in an optical gating structure 90. By appropriate control of each of microcantilevers 70, light incident along direction 92 can either be passed through optical gating structure 90 or be blocked thereby. The multi-section arrangement of each of microcantilevers 70 enables the movement thereof out of the respective light pathways, thereby enabling a maximum amount of light to pass therethrough. While each of microcantilevers 70 is shown in Fig. 9b as being simultaneously actuated, those skilled in the art will understand that individual microcantilevers 70 can be selectively controlled so as to either open a light pathway or not, in dependence upon the voltages supplied via a connected controller. Thus, one or more apertures can be caused to pass light and the remaining apertures can be in a shut state, in dependence upon a particularly desired control scheme.
Each of the embodiments described above has employed electrothermal actuation of a microcantilever to achieve a movement thereof about an anchor point. In Fig. 10, a microcantilever 100 employs piezoelectric/electrostrictive layers to achieve a wide range of motions that are similar to those achieved by the electrothermally actuated microcantilevers described above. A piezoelectric/electrostrictive film 102 includes a first section and a second section, the first section being sandwiched by a pair of electrodes 104, 106 and the second section by a pair of electrodes 108 and 110. Electrodes 104 and 106 are connected to a source of control voltage VI, and electrodes 108 and 110 are connected to a source of control voltage V2. By reversing the respective potentials applied to electrodes 104, 106 and 108, 110, opposite directions of movement can be achieved. Additional electrode films can be added to the structure of Fig. 10 to add electrostatic pulldown action. Further, thermally heated films can be added to the structure of Fig. 10 to provide movement control. Other than the fact that actuator 100 is operated by piezoelectric/electrostrictive actions, its movements can be controlled in substantially the same manner as the electrothermally actuated microactuator described above.
It should be understood that the foregoing description is only illustrative of the invention. Various alternatives and modifications can be devised by those skilled in the art without departing from the invention. Accordingly, the present invention is intended to embrace all such alternatives, modifications and variances which fall within the scope of the appended claims .

Claims

1. A cantilever microstructure comprising:
a substrate;
a cantilever arm having a proximal end connected to said substrate and a free distal end, said cantilever arm including at least a first section and a second section and comprised of a material exhibiting a first thermal coefficient of expansion (TCE) ;
contact means positioned near said distal end;
first layer means positioned on a surface of said cantilever arm in said first section, said first layer means exhibiting a second TCE which is different from the first TCE;
second layer means positioned on a surface of said cantilever arm in said second section, said first layer means exhibiting a third TCE which is different from the first TCE;
control means for selectively applying signals to said first layer means and/or said second layer means to cause a flexure of said cantilever arm so as to bring said distal end into or out of contact with said contact means .
2. The cantilever microstructure as recited in claim 1, wherein said first layer means comprises a first dielectric layer and a first resistive layer, and said second layer means comprises a second dielectric layer and a second resistive layer, said control means applying said signals to said first resistive layer and second resistive layer to cause a heating of said first resistive layer and second resistive layer and said cantilever arm, whereby differential expansion/contraction causes movement of said first section and second section of said cantilever arm.
3. The cantilever microstructure as recited in claim 2, wherein said first dielectric layer and second dielectric layer exhibit identical TCE's.
4. The cantilever microstructure as recited in claim 2, wherein said first dielectric layer is positioned on one surface of said cantilever arm and said second dielectric layer is positioned on a surface of said cantilever arm that is opposed to said one surface.
5. The cantilever microstructure as recited in claim 1, wherein said contact means is positioned on said substrate and comprises at least a pair of electrical contacts and said distal end comprises a conductor which provides a circuit path between said contact means when in contact therewith.
6. The cantilever microstructure as recited in claim 5, wherein said pair of electrical contacts and said conductor manifest irregular surfaces at points of contact therebetween to assure frictional contact therebetween.
7. The cantilever microstructure as recited in claim 5, wherein said pair of electrical contacts and said conductor manifest irregular surfaces at points of contact therebetween to assure a minimum electrical contact resistance therebetween.
8. The cantilever microstructure as recited in claim 2, wherein said first dielectric layer and said second dielectric layer are comprised of silicon nitride and said cantilever arm is comprised of polysilicon.
9. The cantilever microstructure as recited in claim 2, wherein said first dielectric layer and said second dielectric layer are comprised of an oxide of silicon and said cantilever arm is comprised of amorphous silicon.
10. The cantilever microstructure as recited in claim 1, further comprising:
conductive means positioned on and insulated from said cantilever arm at least in a region of said free distal end; and
means for applying a potential between said conductive means and said contact means which induces an electrostatic hold-down force on said distal end when said distal end is in contact with said contact means .
11. An actuator comprising:
a movable structure;
a substrate positioned adjacent said movable structure;
plural cantilever actuators mounted on said substrate, each comprising-. a cantilever arm having a proximal end connected to said substrate and a distal end, said cantilever arm comprising at least a first section and a second section and comprised of a material exhibiting a first thermal coefficient of expansion (TCE) ;
first layer means positioned on a surface of said cantilever arm and along said first section, said first layer means exhibiting a second TCE which is different from the first TCE;
second layer means positioned on a surface of said cantilever arm and along said second section, said first layer means exhibiting a third TCE which is different from the first TCE; and
control means for selectively applying signals to said first layer means and/or said second layer means to cause a flexure of said cantilever arm so as to bring said distal end into contact with said movable structure to cause movement thereof .
12. An optical shutter comprising:
an apertured structure including plural apertures ;
plural cantilever shutters mounted on said apertured structure, each shutter comprising:
a cantilever shutter having a proximal end connected to said apertured structure and an extending portion for closing an adjacent aperture, said extending portion comprising a first section and a second section and exhibiting a first thermal coefficient of expansion (TCE) ;
first layer means positioned on a surface of said cantilever shutter and along said first section, said first layer means exhibiting a second TCE which is different from the first TCE;
second layer means positioned on a surface of said cantilever shutter and along said second section, said first layer means exhibiting a third TCE which is different from the first TCE; and
control means for selectively applying signals to said first layer means and/or said second layer means to cause a flexure of said cantilever shutter so as to move said extending portion to optically block said adjacent aperture or unblock said adjacent aperture .
13. A cantilever microstructure comprising:
a substrate;
a cantilever arm having a proximal end connected to said substrate and a distal end, said arm comprising a first section and a second section and comprised of a material exhibiting a piezoelectric/electrostrictive characteristic,- contact means positioned near said distal end;
first electrode means positioned about said cantilever arm and along said first section, for causing, upon energization, movement of said first section;
second electrode means positioned about said cantilever arm and along said second section, for causing, upon energization, movement of said second section; and
control means for selectively applying signals to said first electrode means and/or said second electrode means to cause a flexure of said cantilever arm so as to bring said distal end into or out of contact with said contact means .
14. The cantilever microstructure as recited in claim 13, further comprising:
thermally actuated means positioned on said cantilever arm which, when energized, act to cause further movement of said cantilever arm.
15. The cantilever microstructure as recited in claim 13, further comprising:
conductive means positioned on and insulated from said cantilever arm at least in a region of said distal end; and
means for applying a potential between said conductive means and said contact means which induces an electrostatic hold-down force on said distal end when said distal end is in contact with said contact means .
PCT/IB1998/000344 1997-01-24 1998-01-20 Cantilevered microstructure WO1998033195A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/787,281 US5796152A (en) 1997-01-24 1997-01-24 Cantilevered microstructure
US08/787,281 1997-01-24

Publications (1)

Publication Number Publication Date
WO1998033195A1 true WO1998033195A1 (en) 1998-07-30

Family

ID=25140976

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB1998/000344 WO1998033195A1 (en) 1997-01-24 1998-01-20 Cantilevered microstructure

Country Status (2)

Country Link
US (1) US5796152A (en)
WO (1) WO1998033195A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000058980A1 (en) * 1999-03-26 2000-10-05 Minners R Sjhon Bistable micro-switch and method of manufacturing the same
US6236300B1 (en) 1999-03-26 2001-05-22 R. Sjhon Minners Bistable micro-switch and method of manufacturing the same
WO2001073805A1 (en) * 2000-03-29 2001-10-04 Fraunhofer Gesellschaft zur Förderung der angewandten Forschung e.V. Microactuator arrangement
WO2002017339A1 (en) * 2000-08-21 2002-02-28 Jds Uniphase Corporation Switches and switching arrays that use microelectromechanical devices having one or more beam members that are responsive to temperature
FR2871790A1 (en) * 2004-06-22 2005-12-23 Commissariat Energie Atomique Microspring for micropoint card system, has free end, and sections with layer of one material and two stacks of layers of another two materials, where layer of each stack is set in predetermined state of stress

Families Citing this family (95)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE9500849D0 (en) * 1995-03-10 1995-03-10 Pharmacia Ab Methods for the manufacture of micromachined structures and micromachined structures manufactured using such methods
US5962949A (en) * 1996-12-16 1999-10-05 Mcnc Microelectromechanical positioning apparatus
US5994816A (en) * 1996-12-16 1999-11-30 Mcnc Thermal arched beam microelectromechanical devices and associated fabrication methods
WO1998045677A2 (en) * 1997-02-28 1998-10-15 The Penn State Research Foundation Transducer structure with differing coupling coefficients feature
SE9703969L (en) * 1997-10-29 1999-04-30 Gert Andersson Device for mechanical switching of signals
US6091050A (en) * 1997-11-17 2000-07-18 Roxburgh Limited Thermal microplatform
FR2772512B1 (en) * 1997-12-16 2004-04-16 Commissariat Energie Atomique MICROSYSTEM WITH DEFORMABLE ELEMENT UNDER THE EFFECT OF A THERMAL ACTUATOR
US6017770A (en) * 1998-09-30 2000-01-25 Eastman Kodak Company Method of making a hybrid micro-electromagnetic article of manufacture
US6253011B1 (en) 1998-12-30 2001-06-26 Mcdonnell Douglas Corporation Micro-aligner for precisely aligning an optical fiber and an associated fabrication method
US6792754B2 (en) * 1999-02-15 2004-09-21 Silverbrook Research Pty Ltd Integrated circuit device for fluid ejection
AUPP868999A0 (en) * 1999-02-15 1999-03-11 Silverbrook Research Pty Ltd A method and apparatus(IJ46P1D)
US6590313B2 (en) 1999-02-26 2003-07-08 Memscap S.A. MEMS microactuators located in interior regions of frames having openings therein and methods of operating same
US6236139B1 (en) 1999-02-26 2001-05-22 Jds Uniphase Inc. Temperature compensated microelectromechanical structures and related methods
US6160230A (en) * 1999-03-01 2000-12-12 Raytheon Company Method and apparatus for an improved single pole double throw micro-electrical mechanical switch
US6137206A (en) * 1999-03-23 2000-10-24 Cronos Integrated Microsystems, Inc. Microelectromechanical rotary structures
US6430333B1 (en) * 1999-04-15 2002-08-06 Solus Micro Technologies, Inc. Monolithic 2D optical switch and method of fabrication
US6218762B1 (en) * 1999-05-03 2001-04-17 Mcnc Multi-dimensional scalable displacement enabled microelectromechanical actuator structures and arrays
AU2005203482B2 (en) * 1999-06-30 2006-09-14 Zamtec Limited Inkjet Printhead with Excess Actuator Movement Detection
AU2004200135B2 (en) * 1999-06-30 2005-05-26 Zamtec Limited Movement sensor in a micro electro-mechanical device
AU766416B2 (en) * 1999-06-30 2003-10-16 Silverbrook Research Pty Ltd Movement sensor in a micro electro-mechanical device
AUPQ130999A0 (en) * 1999-06-30 1999-07-22 Silverbrook Research Pty Ltd A method and apparatus (IJ47V11)
US6382779B1 (en) * 1999-06-30 2002-05-07 Silverbrook Research Pty Ltd Testing a micro electro- mechanical device
US6229683B1 (en) 1999-06-30 2001-05-08 Mcnc High voltage micromachined electrostatic switch
US6057520A (en) * 1999-06-30 2000-05-02 Mcnc Arc resistant high voltage micromachined electrostatic switch
DE19936112A1 (en) * 1999-07-31 2001-02-01 Mannesmann Vdo Ag Semiconductor switch
GB2353410B (en) * 1999-08-18 2002-04-17 Marconi Electronic Syst Ltd Electrical switches
US6291922B1 (en) 1999-08-25 2001-09-18 Jds Uniphase, Inc. Microelectromechanical device having single crystalline components and metallic components
US6268908B1 (en) * 1999-08-30 2001-07-31 International Business Machines Corporation Micro adjustable illumination aperture
US6255757B1 (en) 1999-09-01 2001-07-03 Jds Uniphase Inc. Microactuators including a metal layer on distal portions of an arched beam
US6211598B1 (en) * 1999-09-13 2001-04-03 Jds Uniphase Inc. In-plane MEMS thermal actuator and associated fabrication methods
US6275320B1 (en) 1999-09-27 2001-08-14 Jds Uniphase, Inc. MEMS variable optical attenuator
US6239685B1 (en) 1999-10-14 2001-05-29 International Business Machines Corporation Bistable micromechanical switches
US6359374B1 (en) 1999-11-23 2002-03-19 Mcnc Miniature electrical relays using a piezoelectric thin film as an actuating element
US6333583B1 (en) * 2000-03-28 2001-12-25 Jds Uniphase Corporation Microelectromechanical systems including thermally actuated beams on heaters that move with the thermally actuated beams
US6624730B2 (en) * 2000-03-28 2003-09-23 Tini Alloy Company Thin film shape memory alloy actuated microrelay
US6698295B1 (en) * 2000-03-31 2004-03-02 Shipley Company, L.L.C. Microstructures comprising silicon nitride layer and thin conductive polysilicon layer
US7026697B2 (en) * 2000-03-31 2006-04-11 Shipley Company, L.L.C. Microstructures comprising a dielectric layer and a thin conductive layer
AU6851101A (en) * 2000-06-19 2002-01-02 Univ Brigham Young Thermomechanical in-plane microactuator
WO2002002328A1 (en) * 2000-06-30 2002-01-10 Silverbrook Research Pty Ltd Buckle resistant thermal bend actuators
US6775048B1 (en) * 2000-10-31 2004-08-10 Microsoft Corporation Microelectrical mechanical structure (MEMS) optical modulator and optical display system
US6473361B1 (en) 2000-11-10 2002-10-29 Xerox Corporation Electromechanical memory cell
FR2818795B1 (en) * 2000-12-27 2003-12-05 Commissariat Energie Atomique MICRO-DEVICE WITH THERMAL ACTUATOR
US6626417B2 (en) 2001-02-23 2003-09-30 Becton, Dickinson And Company Microfluidic valve and microactuator for a microvalve
DE10122363B4 (en) * 2001-05-09 2007-11-29 Infineon Technologies Ag Semiconductor module
JP2003062798A (en) * 2001-08-21 2003-03-05 Advantest Corp Actuator and switch
DE60222468T2 (en) * 2001-11-09 2008-06-12 Wispry, Inc. MEMS DEVICE WITH THREE-LINE BENDING BAR AND METHOD THEREFOR
US6770882B2 (en) * 2002-01-14 2004-08-03 Multispectral Imaging, Inc. Micromachined pyro-optical structure
US6631979B2 (en) 2002-01-17 2003-10-14 Eastman Kodak Company Thermal actuator with optimized heater length
US6838640B2 (en) * 2002-05-13 2005-01-04 The Regents Of The University Of Michigan Separation microcolumn assembly for a microgas chromatograph and the like
AU2002368165A1 (en) * 2002-08-08 2004-02-25 Xcom Wireless, Inc. Microfabricated double-throw relay with multimorph actuator and electrostatic latch mechanism
WO2004015729A1 (en) * 2002-08-08 2004-02-19 Xcom Wireless, Inc. Microfabricated relay with multimorph actuator and electrostatic latch mechanism
US7019434B2 (en) * 2002-11-08 2006-03-28 Iris Ao, Inc. Deformable mirror method and apparatus including bimorph flexures and integrated drive
US7034375B2 (en) * 2003-02-21 2006-04-25 Honeywell International Inc. Micro electromechanical systems thermal switch
US7038355B2 (en) * 2003-04-03 2006-05-02 Stmicroelectronics Sa Tunable microresonator on an insulating beam deformable by the difference in thermal expansion coefficients
US20040255643A1 (en) * 2003-05-13 2004-12-23 Wise Kensall D. High-performance separation microcolumn assembly and method of making same
US7422403B1 (en) 2003-10-23 2008-09-09 Tini Alloy Company Non-explosive releasable coupling device
US6877316B1 (en) * 2003-11-21 2005-04-12 Zyvex Corporation Electro-thermal scratch drive actuator
FR2868591B1 (en) * 2004-04-06 2006-06-09 Commissariat Energie Atomique MICROCOMMUTER WITH LOW ACTUATION VOLTAGE AND LOW CONSUMPTION
US7632361B2 (en) * 2004-05-06 2009-12-15 Tini Alloy Company Single crystal shape memory alloy devices and methods
US7623142B2 (en) * 2004-09-14 2009-11-24 Hewlett-Packard Development Company, L.P. Flexure
US7665300B2 (en) * 2005-03-11 2010-02-23 Massachusetts Institute Of Technology Thin, flexible actuator array to produce complex shapes and force distributions
US7763342B2 (en) 2005-03-31 2010-07-27 Tini Alloy Company Tear-resistant thin film methods of fabrication
US7441888B1 (en) 2005-05-09 2008-10-28 Tini Alloy Company Eyeglass frame
US7540899B1 (en) 2005-05-25 2009-06-02 Tini Alloy Company Shape memory alloy thin film, method of fabrication, and articles of manufacture
US7683429B2 (en) * 2005-05-31 2010-03-23 Semiconductor Energy Laboratory Co., Ltd. Microstructure and manufacturing method of the same
US7349236B2 (en) * 2005-06-24 2008-03-25 Xerox Corporation Electromechanical memory cell with torsional movement
US20070096860A1 (en) * 2005-11-02 2007-05-03 Innovative Micro Technology Compact MEMS thermal device and method of manufacture
US7548145B2 (en) * 2006-01-19 2009-06-16 Innovative Micro Technology Hysteretic MEMS thermal device and method of manufacture
WO2008052306A1 (en) * 2006-09-28 2008-05-08 Simon Fraser University Three-dimensional microstructures and methods for making same
US8349099B1 (en) 2006-12-01 2013-01-08 Ormco Corporation Method of alloying reactive components
US8584767B2 (en) 2007-01-25 2013-11-19 Tini Alloy Company Sprinkler valve with active actuation
WO2008092028A1 (en) 2007-01-25 2008-07-31 Tini Alloy Company Frangible shape memory alloy fire sprinkler valve actuator
US8168120B1 (en) 2007-03-06 2012-05-01 The Research Foundation Of State University Of New York Reliable switch that is triggered by the detection of a specific gas or substance
US7602266B2 (en) * 2007-03-16 2009-10-13 Réseaux MEMS, Société en commandite MEMS actuators and switches
US8007674B2 (en) 2007-07-30 2011-08-30 Tini Alloy Company Method and devices for preventing restenosis in cardiovascular stents
US8154378B2 (en) * 2007-08-10 2012-04-10 Alcatel Lucent Thermal actuator for a MEMS-based relay switch
JP5391395B2 (en) * 2007-10-15 2014-01-15 日立金属株式会社 Substrate with piezoelectric thin film and piezoelectric element
US8556969B2 (en) 2007-11-30 2013-10-15 Ormco Corporation Biocompatible copper-based single-crystal shape memory alloys
US8382917B2 (en) 2007-12-03 2013-02-26 Ormco Corporation Hyperelastic shape setting devices and fabrication methods
US7842143B2 (en) 2007-12-03 2010-11-30 Tini Alloy Company Hyperelastic shape setting devices and fabrication methods
JP5605952B2 (en) * 2008-11-26 2014-10-15 フリースケール セミコンダクター インコーポレイテッド Electromechanical transducer device and manufacturing method thereof
US8513042B2 (en) 2009-06-29 2013-08-20 Freescale Semiconductor, Inc. Method of forming an electromechanical transducer device
US8314983B2 (en) * 2009-11-10 2012-11-20 International Business Machines Corporation Nonvolatile nano-electromechanical system device
GB2516801A (en) 2012-05-24 2015-02-04 Douglas H Lundy Threat detection system and method
US11040230B2 (en) 2012-08-31 2021-06-22 Tini Alloy Company Fire sprinkler valve actuator
US10124197B2 (en) 2012-08-31 2018-11-13 TiNi Allot Company Fire sprinkler valve actuator
EP2868853B1 (en) * 2013-10-31 2018-12-26 Electrolux Appliances Aktiebolag Household appliance comprising an actuation system
FR3042789B1 (en) * 2015-10-21 2019-07-12 Commissariat A L'energie Atomique Et Aux Energies Alternatives MICROELECTROMECHANICAL AND / OR NANOELECTROMECHANICAL STRUCTURE WITH ELECTROTHERMIC ACTUATION COMPRISING AT LEAST TWO DIFFERENTLY POLARIZABLE ACTUATION BEAMS
WO2017130738A1 (en) * 2016-01-29 2017-08-03 株式会社村田製作所 Vibration device
US11456234B2 (en) 2018-08-10 2022-09-27 Frore Systems Inc. Chamber architecture for cooling devices
US11464140B2 (en) 2019-12-06 2022-10-04 Frore Systems Inc. Centrally anchored MEMS-based active cooling systems
KR20220082053A (en) 2019-10-30 2022-06-16 프로리 시스템스 인코포레이티드 MEMS based airflow system
US11510341B2 (en) * 2019-12-06 2022-11-22 Frore Systems Inc. Engineered actuators usable in MEMs active cooling devices
US11796262B2 (en) 2019-12-06 2023-10-24 Frore Systems Inc. Top chamber cavities for center-pinned actuators
KR20230075503A (en) 2020-10-02 2023-05-31 프로리 시스템스 인코포레이티드 active heatsink

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2717759A1 (en) * 1976-04-22 1977-11-24 Hitachi Ltd THERMAL DELAY SWITCH
US5258591A (en) * 1991-10-18 1993-11-02 Westinghouse Electric Corp. Low inductance cantilever switch
US5463233A (en) * 1993-06-23 1995-10-31 Alliedsignal Inc. Micromachined thermal switch
WO1996008701A1 (en) * 1994-09-12 1996-03-21 International Business Machines Corporation Electromechanical transducer
WO1996034417A1 (en) * 1995-04-27 1996-10-31 Elisabeth Smela A micromachined structure and use thereof, and a micromachined device and a method for the manufacture thereof

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5058856A (en) * 1991-05-08 1991-10-22 Hewlett-Packard Company Thermally-actuated microminiature valve
JP3148946B2 (en) * 1991-05-30 2001-03-26 キヤノン株式会社 Probe driving mechanism, tunnel current detecting device using the mechanism, information processing device, piezoelectric actuator
US5536963A (en) * 1994-05-11 1996-07-16 Regents Of The University Of Minnesota Microdevice with ferroelectric for sensing or applying a force
DE4437260C1 (en) * 1994-10-18 1995-10-19 Siemens Ag Micro-mechanical electrostatic relay with slotted spring tongue surface
US5659195A (en) * 1995-06-08 1997-08-19 The Regents Of The University Of California CMOS integrated microsensor with a precision measurement circuit

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2717759A1 (en) * 1976-04-22 1977-11-24 Hitachi Ltd THERMAL DELAY SWITCH
US5258591A (en) * 1991-10-18 1993-11-02 Westinghouse Electric Corp. Low inductance cantilever switch
US5463233A (en) * 1993-06-23 1995-10-31 Alliedsignal Inc. Micromachined thermal switch
WO1996008701A1 (en) * 1994-09-12 1996-03-21 International Business Machines Corporation Electromechanical transducer
WO1996034417A1 (en) * 1995-04-27 1996-10-31 Elisabeth Smela A micromachined structure and use thereof, and a micromachined device and a method for the manufacture thereof

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000058980A1 (en) * 1999-03-26 2000-10-05 Minners R Sjhon Bistable micro-switch and method of manufacturing the same
US6236300B1 (en) 1999-03-26 2001-05-22 R. Sjhon Minners Bistable micro-switch and method of manufacturing the same
WO2001073805A1 (en) * 2000-03-29 2001-10-04 Fraunhofer Gesellschaft zur Förderung der angewandten Forschung e.V. Microactuator arrangement
US6684638B2 (en) 2000-03-29 2004-02-03 Fraunhofer Gesellschaft Zur Angewandten Forderung Der Forschung E.V. Microactuator arrangement
WO2002017339A1 (en) * 2000-08-21 2002-02-28 Jds Uniphase Corporation Switches and switching arrays that use microelectromechanical devices having one or more beam members that are responsive to temperature
FR2871790A1 (en) * 2004-06-22 2005-12-23 Commissariat Energie Atomique Microspring for micropoint card system, has free end, and sections with layer of one material and two stacks of layers of another two materials, where layer of each stack is set in predetermined state of stress

Also Published As

Publication number Publication date
US5796152A (en) 1998-08-18

Similar Documents

Publication Publication Date Title
US5796152A (en) Cantilevered microstructure
US6351580B1 (en) Microelectromechanical devices having brake assemblies therein to control movement of optical shutters and other movable elements
US5870007A (en) Multi-dimensional physical actuation of microstructures
US6819822B2 (en) Two-dimensional gimbaled scanning actuator with vertical electrostatic comb-drive for actuation and/or sensing
US7928632B2 (en) Method and structure for an out-of-plane compliant micro actuator
US6275325B1 (en) Thermally activated microelectromechanical systems actuator
US6211598B1 (en) In-plane MEMS thermal actuator and associated fabrication methods
US6327855B1 (en) Actuators including serpentine arrangements of alternating actuating and opposing segments and related methods
US6428173B1 (en) Moveable microelectromechanical mirror structures and associated methods
KR101081759B1 (en) Micro electromechanical system switch
CA2320458C (en) Mems variable optical attenuator
US6804959B2 (en) Unilateral thermal buckle-beam actuator
US5214727A (en) Electrostatic microactuator
US6367252B1 (en) Microelectromechanical actuators including sinuous beam structures
US6675578B1 (en) Thermal buckle-beam actuator
JP2001117027A (en) Micro electromechanical optical device
JP4115116B2 (en) Thermal microelectrical mechanical actuator
US6739132B2 (en) Thermal micro-actuator based on selective electrical excitation
WO2001073937A2 (en) Two-dimensional gimbaled scanning actuator with vertical electrostatic comb-drive for actuation and/or sensing
JP4544823B2 (en) Out-of-plane operation method of thermal MEMS actuator and thermal MEMS actuator
US6338249B1 (en) Electrothermally actuated vibromotor
US20020172452A1 (en) Latching apparatus for a mems optical switch
US7893799B1 (en) MEMS latching high power switch
Lee Novel H-beam electrothermal actuators with capability of generating bi-directional static displacement
WO2004017509A2 (en) System and method for providing a micro-electro-mechanical microengine assembly

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): JP

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 1998531780

Format of ref document f/p: F

122 Ep: pct application non-entry in european phase