The invention relates generally to a method and apparatus for correcting optical aberrations. More specifically, the invention relates to a method and apparatus for correcting optical aberrations using a deformable mirror.
Many applications employing optical devices are limited by optical aberrations that result from the configuration of the optical device. The term “optical aberrations” includes deviations from the correct function of the optical device that result from disruptions and distortions of optical paths associated with the device. A source of optical aberrations that is particularly limiting in the use of optical devices is the object of the optical device. The object, or sample, refers to the element that the optical device is designed to perform a particular function on. Object-induced, or sample-induced, aberrations result from the refractive properties of the object or the optical path between the object and the optical device, and may include spherical aberrations that are symmetrical around the optical axis, as well as other types of aberrations.
Aberrations can be characterized by the shift in optical path experienced by a ray of light as it travels from a point source (i.e., a point at a given depth within a sample) through the sample. For many common configurations (i.e., for a system with a set sample refractive index and a set atmospheric or objective immersion refractive index separated by an interface plane perpendicular to the optical axis) the shift in optical path is only dependent upon the depth of the point source within the sample and the angle at which the ray of light travels through the sample relative to the optical axis.
The pupil plane in an optical device is the plane where the position of each ray depends solely on the angle of emergence from the sample alone. For any given optical device, it is possible to determine where at the pupil plane a ray with a particular angle of emergence will be positioned. Accordingly, at this plane, it is possible to identify the angle of emergence from the sample for each ray based upon the position of the ray at the pupil plane. Since in common configurations the shift in optical path depends on depth and angle alone, for each depth it is possible to correct the spherical aberrations at the pupil plane by introducing an optical element that can correct each ray of light according to its optical path shift.
Spherical aberrations are particularly problematic when analyzing moderately thick objects because they are depth dependent. A detailed discussion of optical aberrations, and a method and system for correcting optical aberrations, including spherical aberrations, is provided in U.S. patent application Ser. No. 11/419,070, which is incorporated herein by reference. The '070 application describes a method and system for correcting optical aberrations in applications such as wide-field microscopy, optical tweezers and optical media read/write devices. The '070 application teaches the use of adaptive optical elements of several types, such as a liquid lens (adjusted by pressure), a deformable membrane mirror (adjusted by piezoelectric or magnetic pistons), micro electro-mechanical (MEMS) mirrors, or various liquid crystal phase and amplitude modulators (with optical properties that are controlled pixel-by-pixel electrically via the patterned surfaces holding the liquid between them). Additionally, the '070 application provides that a mirror, such as a deformable mirror, may be used as an adaptive optical element for correcting optical aberrations.
Existing deformable mirror elements that use a force at the center of the rear surface of a mirror create a parabolic shape deformation on the mirror's surface. See, e.g., U.S. Pat. No. 7,229,178, which is incorporated herein by reference. Such mirrors can be made as small as required. The resulting wavefront after reflection in such mirrors can change the focus of the impinging wave, however, they introduce an additional large component of spherical aberrations. Other types of mirrors are deformed by introducing forces applied by multiple actuators at multiple locations on the mirror (typically on a rectangular or hexagonal array of points). These mirrors have more degrees of freedom for creating arbitrary functions of distortions for shaping a wavefront reflected from their surface. However, they are problematic in that they must be sufficiently large in order to provide space for the actuators, and they are associated with high-order aberrations introduced by the array of pistons. This problem is shared by both segmented mirrors (where each mirror segment is associated with one piston for displacement and maybe additional pistons for tilt) and “shape mirrors” (where multiple pistons push on a deformable membrane mirror). Both types of mirrors create deviations from the ideally required shape at the spatial frequency of the piston array; this is called piston “print through” or “waffle.” Another kind of adaptive optical element based on liquid crystals has small size and high spatial resolution.
However, a problem shared by most available adaptive elements is their limited range of creating phase shifts (e.g., a few wavelengths for typical devices). The maximum phase shift introduced by an adaptive optical element is called “throw”. Typical adaptive devices with throws of the order of two wavelengths can correct small aberrations, but have limited capability to change the focus of optical systems. They cannot correct aberrations in moderately thick objects, and cannot change focus in a useful scale. Other types of electric and magnetic actuators that can introduce more “throw” are large and transduce a very limited amount of force. These actuators are used with soft deformable membrane mirrors and have large “print-through” effects. The large size of the mirrors necessitates long optical distances that require large and bulky optical systems.
The present invention provides a method and apparatus that uses an improved deformable mirror in optical systems to change the focus and corrects optical aberrations, such as spherical aberrations, when analyzing objects, particularly moderately thick objects, without the disadvantages associated with existing approaches. Unlike existing optical systems with larger deformable mirrors, the present invention provides a method and apparatus that simply and precisely deforms a deformable mirror to a shape that provides a variable focal plane at varying depths within an object and corrects optical aberrations. In order to simply and precisely achieve the necessary shape function in the deformable mirror, the deformable mirror may have a variable thickness that provides the necessary deflective characteristics to create surface displacement functions for correcting optical aberrations and changing focus within an object, including moderately thick objects. Further, a simple and precise actuation system may be employed that deforms the variable thickness deformable mirror. The present invention may be implemented in many fields, including wide-field microscopy, optical tweezers and in optical media recording and reading devices. Moreover, the present invention may be incorporated into and implemented with the method and system taught by the '070 application.
According to an embodiment of the present invention, an apparatus for correcting optical aberrations in an optical device includes a deformable mirror having a variable thickness and an actuator configured to deform the deformable mirror. The deformable mirror may be anchored at its periphery and the actuator may be configured to apply a force to a central portion of the deformable mirror. The deformable mirror may be thinner at its periphery than at its center. The deformable mirror may also be thicker at its periphery than at its center. The deformable mirror may include a reflective surface that is configured to be shaped into a plane, a concave or a convex shape at equilibrium (without forces applied to it), leaving the thickness function free to be determined by the needed deformation from the equilibrium shape which is created by a single force actuator, e.g., pressing or pulling at a generally central portion of the deformable mirror. The actuator may be connected to a small pin emerging from the back of the mirror to closely approximate a point force. The pin may be located in a center or off-center position on the back of the mirror. Alternatively, the actuator may transduce the piston forces via a pressurized liquid that applies the forces homogeneously and uniformly to the deformable mirror such that the mirror deformation is a concave or a convex shape when higher or lower pressure is applied. Alternatively, a force may be applied circumferentially. The deformable mirror may be either a flat disk mirror with varying thickness or a stretched membrane mirror with variable elasticity, the flat disk or the stretched membrane mirror configured to produce the desired displacement function across its surfaces when forces or pressure act upon it.
According to another embodiment of the present invention, an apparatus for correcting optical aberrations in an optical device includes a deformable mirror having a variable thickness and an actuator configured to deform the deformable mirror where the actuator is configured to apply a compressive force along a circumferential portion of the deformable mirror where the deformable mirror is formed into a convex or concave shape under compression. The deformable mirror may be thinner at its periphery than at its center. The deformable mirror may also be thicker at its periphery than at its center. The apparatus may include a circumferential element positioned around a periphery of the deformable mirror. The actuator may actuate the circumferential element such that the circumferential element compresses the deformable mirror radially all around it. The actuator may be a single force actuator, such as a piezoelectrical device. The circumferential element may be a collet chuck, or a contracting ring. The deformable mirror may be a flat disk mirror made of metal, glass or plastics with variable thickness designed to deform upon introduction of the peripheral force according to a given displacement function. An advantage of this embodiment is that actuators that produce small displacements with large forces are placed to transform the mirror with much larger displacements. For example, if a piezoelectric piston introduces a 10 micrometer displacement at its tip, the circumferential device can translate it into a 30-fold displacement (about 0.3 min) at the mirror center.
According to another embodiment of the present invention, a method for correcting optical aberrations in an optical device includes the steps of: positioning an adaptive optical system in or close to a pupil plane, the adaptive optical system including at least one adaptive optical element, the adaptive optical element including a deformable mirror having a variable thickness and an actuator configured to deform the deformable mirror; configuring the adaptive optical element to correct optical aberrations at a first depth of focus within a sample; and reconfiguring the adaptive optical element to change focus and correct for optical aberrations at a second depth within the sample, the second depth being different from the first depth. The adaptive element may also include additional features of the apparatus for correcting optical aberrations discussed herein. If the optical device is a wide-field microscope, the method may also include the step of successively acquiring a plurality of images at different depths of focus within the sample over a predetermined period of time. If the optical device is a microscope, aberration-free three-dimensional images may be acquired. If the optical device is a three-dimensional recordable medium, data may be written or read from multiple layers.
Further details and aspects of example embodiments of the present invention are described in more detail with reference to the Figures, in which:
FIGS. 1 and 2A-2F illustrate a deformable mirror 10 having a variable thickness. In some embodiments, as depicted in
The relative thickness of the periphery and center of the deformable mirror 10 can be chosen based on the angular dependence function of the aberrations to be corrected. In the embodiments in which the deformable mirror 10 is thinner at its periphery than at its center, the application of a deforming force causes the deformable mirror 10 to deform by a relatively large amount along its periphery. This results in a relatively large change in the phase of the reflected wavefront at large angles. By contrast, in the embodiments in which the deformable mirror 10 is thicker at its periphery than at its center, the application of a deforming force causes the deformable mirror 10 to deform by a relatively large amount away from its periphery. This results in a relatively large change in the phase of the reflected wavefront at small angles. Therefore, a deformable mirror 10 that is thinner at its periphery than at its center can be used when relatively large phase changes are desired at large angles, while a deformable mirror 10 that is thicker at its periphery than at its center can be used when relatively large phase changes are desired at small angles.
Deformable mirror 10 is not limited to the specific profiles illustrated. It may have alternate profiles of varying thicknesses that provide desired surface displacements from equilibrium when forces act to distort the mirror and therefore, shift the phase of a reflected wavefront as a function of position on the mirror (e.g., as a function of radius for spherical aberration corrections). Deformable mirror 10 may be a flat disk mirror with variable thickness, e.g., as shown in
As discussed above, deformable mirror 10 need not have a circular shape. It may, for example, have an elliptical shape. Further, the retaining ring or collet around the edge of the mirror may be elliptical in shape. Still further, the mirror may have an elliptical profile. It is possible to provide an elliptical correction function to account for off-axis corrections.
Alternatively, in
A system for correcting optical aberrations in an optical device may include an adaptive optical system. The adaptive optical system includes at least one adaptive optical element positioned for example in a pupil plane and is capable of correcting optical aberrations at a first depth of focus within a sample. The adaptive optical element is capable of being reconfigured to correct for optical aberrations at a second depth within the sample, the second depth being different from the first depth. The adaptive element includes a deformable mirror having a variable thickness and an actuator configured to deform the deformable mirror. The adaptive element may also include the features of the apparatus for correcting optical aberrations discussed herein. The optical device may include a wide-field microscope, optical tweezers or an optical read/write media drive.
A method for correcting optical aberrations in an optical device includes the following steps: positioning an adaptive optical system for example in a pupil plane, where the adaptive optical system includes at least one adaptive optical element, the adaptive optical element includes a deformable mirror having a variable thickness and an actuator configured to deform the deformable mirror; configuring the adaptive optical element to correct optical aberrations at a first depth of focus within a sample; and reconfiguring the adaptive optical element to correct for optical aberrations at a second depth within the sample, the second depth being different from the first depth. If the optical device is a wide-field microscope, the method may also include the step of acquiring a plurality of images at different depths of focus within the sample successively over a predetermined period of time.
The aforementioned methods and apparatuses are advantageous in that they can generate larger vertical surface displacements of a deformable mirror by small displacements of an actuator, such as a piezoelectric actuator and can be made with a small optical diameter allowing their incorporation into compact optical systems, see, e.g.,
The aforementioned methods and apparatuses are also advantageous in that the profile or thickness of deformable mirrors/membranes may be provided such that a desired deflection takes place in the deformable mirrors/membranes. For example, an optical system configured to image different focal planes (or sample depths) may image different focal planes by moving the optics (and camera) with respect to a sample, by adjusting one or several optical elements within the optical system without changing the distance between a front element and the sample or the back element and the camera, or by adding a spherical phase-shift to the wavefront, e.g., using a mirror with variable curvature determined by the focal plane shift. However, high-magnification optical systems, such as microscopes and optical recorders, are typically designed with rays that traverse optics far away from the optical axis at large angles, and are optimized for minimal aberrations in a very stringent configuration. The optimal focal plane for an optical system is designed by minimizing the aberrations. Focusing to other planes can be achieved by adding a phase-shift to the wavefront. The added phase function that defocuses and corrects aberrations is concave with steep sides (steeper than spherical) for negative refractive index mismatch (e.g., live specimens microscopy using an oil-immersion objective into a water-embedded sample), and convex for optical recording devices, (focusing with an air lens into plastics). As shown in
As set forth below in calculation section I, with reference to
Thus, according to the mathematical relations presented below in calculation section II, the displacements of the surface (used as a mirror) for a disk with any given shape, (such as varying thickness) can be calculated numerically as a function of the forces applied to it. These calculations may be carried out by “finite element analysis” software packages. To determine the thickness profile that will create any desired surface function the finite element analysis is carried out for the initial thickness profile, the resulted displacement function is determined, compared to the desired function, and iteratively repeated with the corrected thickness profile, where a larger displacement required implies reducing the thickness and vice versa. For example, if the periphery of the disk deformable mirror is made thinner, when there is compression, the edge displacements are steeper then the parabolic profile of a uniform thickness disk. Arbitrary (possibly aspherical) surfaces could also be created to form any mirror shape without stress. A force may then be applied to displace the surfaces. Special properties of the plate material (glass, metals, carbon fiber, stretched membrane, etc.) may be used in order to achieve various ranges of displacements when responding to forces. For example, a dynamic concave or convex plate mirror may be provided with large displacements, by compression around the periphery of the plate, by homogeneously compression via a pressurized liquid or by applying a force at a center portion of the mirror.
I. Estimation of the Forces and Displacements Generated by Disks
Analytical equations may be used to estimate the forces and displacements that can be expected in various mirror configurations (e.g., the force at center, circumferential force and pressure configurations described herein.) Piezoelectric devices may produce the force and expansion parameter needed to generate sufficiently large mirror deformation for both focusing and correction of aberration.
In
In
1/cos α=√{1+tan2 α}=√{1+(dz/dr)2}˜(1+2a2r2) (1)
Compressing the radius, R, by ΔR, and preserving the length of the bent beam/disk results in:
R+ΔR=integral from 0 to R on{dr/cos α}=R+2/3a2R3 (2)
R+ΔR=0∫R{dr/cos α}=R+2/3a2R3 (3)
α=√{3ΔR/2R3} (4)
dz =aR2=√{3RΔR/2} (5)
where a is defined above: dz(r)=ar2.
For example, in the case of a 10 mm long beam, R=5 mm, ΔR=10 micrometer the bulging at its center dz is:
dz =√{3*5000*10/2}=274 micrometers (6)
For a disk, area preservation implies:
π(R+ΔR)2=integral from 0 to R on {2πRdR/cos α}=2π((R2/2+2/4a2R4) (7)
π(R+ΔR)2=0∫R{2πRdR/coso α}=2π(R2/2+2/4a2R4) (8)
dz =aR2=√{2RΔR} (9)
Bulging is similar in magnitude to the above: for R=5 mm, ΔR=10 micrometer
dz =√{2*5000*10}=316 micrometers (10)
As set forth in L. D. Landau & E. M. Lifshitz, Theory of Elasticity, Butterworth Heinemann, 1986, which is incorporated herein by reference, the rigorous solution for a disk of uniform thickness, h, pressed vertically at its center by force fz and supported on its periphery is as follows:
dz =fz/(16πD)*[(3+ν)/(1+ν)*(R2−r2)−2r2log(R/r)] (11)
D=E h3/[12(1−ν2)] (12)
Substituting for Young's modulus, E=60×103N/mm2; Poisson ratio,ν=0.2 (glass); R=5 mm; h=0.2 mm; for dz=0.3 mm at r=0 results in:
f =30 Newton [approximately 3 Kgm force]. (13)
The peripheral force can be estimated from the bulging angle at R, cos2 α=1−6ΔR/R
sin α=√{6ΔR/R}˜0.11 fz/sin α=9f˜270 Newton [approximately 27 Kgm force] (14)
The solution for a pressure P, applied to a disk of uniform thickness is:
dz =3P(1−ν2)/(16E h3)*(R2−r2)*[(5+ν)/(1+ν)*R2−r2]*(R2−r2). (15)
II. The Differential Equations of Elasticity used to Solve Numerically the Distortions of an Arbitrary Shaped Material when a Set of Forces are Applied to it
Differential equations of forces and distortions in elastic medium are provided for use by “finite element analysis” to solve deformations of arbitrarily shaped solid bodies such that, given the deformations need for focusing and correction of aberrations for a particular optical system, a thickness function (or for membranes a stiffness function) for deformable mirrors, as described herein, may be determined. Thus, as described below, a design of the thickness function of a disk mirror may be determined so as to obtain a desired deformation function on its reflecting surface.
The shape of a piece of material with known elastic properties, such as a disk with an uneven thickness, can be calculated given the forces acting on it. For example, the shape of the disk can be determined when pushed or pulled at its center. These calculations may be used to find the thickness as a function of radius (or more generally, position) that will result in a desired deformation function such that a deformable mirror (e.g., the deformable mirrors discussed in the example embodiments of the present invention presented herein) will create a desired phase shift function for a wavefront reflected from its surface.
fj=?Φij/?xi (16)
Generalized Hooke's law is:
Φij=Cijklεkl (17)
where the indices i, j, k and 1 run on the coordinates x,y,z (reference is made to L. D. Landau & E. M. Lifshitz, Theory of Elasticity, Butterworth Heinemann, 1986, for details regarding vector and matrix annotation, which is incorporated by reference herein), and where the displacements, ul, and the strain tensor εkl are related by the following equation:
εkl=?ul/?xk (18)
Therefore the equilibrium displacements of an object under forces obey the following equation:
fj=?Cijkl εkl/?xi=?i(Cijkl?k ul) (19)
The strain tensor can be expressed in cylindrical coordinates, (rφz) as follows:
εrr=?ur/?r; εφφ=1/r?uφ/?φ+ur/r; εzz=?uz/?z (20)
2 εφz=1/r ?uz/?φ+?uφ/?z; 2εrz=?ur/?z+?uz/? r; 2εrφ=?uφ/?r−u100/r+1/r?ur/?φ (21)
For cylindrically symmetric cases: u100=?uz/?φ=?ur/?φ=0, therefore:
εφz=εrφ=0; 2εrz=?ur/?z+?uz/? r (22)
εrr=?ur/?r; εφφ=ur/,r; εzz=?uz/?z (23)
For a thin plate with “flexural rigidity” D(r)=Eh3(r)/12(1−ν2), the displacements perpendicular to its surface, ζ=uz, as a result of force f(r) in the z direction:
Δζ2=?2ζ/?r2+ν/r ?ζ/? r=f(r)/D(r) (24)
D=E h3(r)/12(1−ν2) (25)
where: E=Young modulus, ν=Poisson ratio, h(r)=disk thickness.
For force along r, the full differential equation fj=?i(Cijkl ?k ui) must be integrated, but for cylindrical symmetry only the two dimensional problem in r, z coordinates should be solved. This much faster two-dimensional numerical solution for the radially symmetric problem allows iterative optimization of the disk thickness function given the desired distortion function which is dictated by the needed phase-shifts to focus and correct aberrations in an optical system.
The equations for the cylindrically-symmetric case are therefore:
Σi∂2uk/∂xi2+1/(1−2ν)∂/∂xk{Σi[∂ui/∂xi]}=−[2 (1+ν)/E] fk (26)
fk=body forces that are zero inside the volume.
where ui are the displacements along x,y and z for i=1,2 and 3 respectively; xi are x,y and z for i=1,2 and 3.
v and w are defined below after their first use in Equations 27,28.
On all free boundaries, the stress tensor is zero: σij==∂ui/∂xk=0 i,j=1,2 for (r,z)
and where forces are applied: ∂σik/∂xk=−fi
Rewriting for the radial and vertical displacements v and w:
∂/∂r[(1+A)r∂v/∂r]+A ∂/∂r[∂w/∂z]+∂/∂z[r∂v/∂z]+2(1+A)∂v/∂r+v/r=Bfr (27)
∂/∂r[∂w/∂r]+∂/∂z[(1+A)∂w/∂z]+∂/∂z[Ar∂v/∂r]+2A∂v/∂z+1/r∂w/∂r=Bfz (28)
where v(r,z)=ur(r,z)/r and w(r,z)=uz(r,z) are the radial and vertical displacements.
A=1/(1−2v) Poisson ratio typical value: ν0.2 (29)
B=−2 (1+ν)/E Young's modulus typical value: E=60×103N/mm2 (30)
Rewriting these equations for the explicit finite element analysis formulation:
∂/∂r[C11∂/∂r[v]]+∂/∂r[D11∂/∂r[w]]++∂/∂r[C12∂/∂z[v]]+∂/∂r[D12∂/∂z[w]]++∂/∂z[C12∂/∂r[v]]+∂/∂z[D21∂/∂r[w]]++∂/∂z[C22∂/∂z[v]]+∂/∂z[D22∂/∂z[w]]++∂/∂r[A1v]+∂/∂r[B1w]++∂/∂z[A2v]+∂/∂z[B2w]++E0=B fr (31)
∂/∂r[C11∂/∂r[v]]+∂/∂r[D11∂/∂r[w]]++∂/∂r[C12∂/∂z[v]]+∂/∂r[D12∂/∂z[w]]++∂/∂z[C21∂/∂r[v]]+∂/∂z[D21∂/∂r[w]]++∂/∂z[C22∂/∂z[v]]+∂/∂z[D22∂/∂z[w]]++∂/∂r[A1v]+∂/∂r[B1w]++∂/∂z[A2v]+∂/∂z[B2w]++E0=B fz (32)
Boundary Conditions:
w(R,0)=0 Disk supported at radius R.
v(0,z)=∂v(0,z)/∂r=∂w/∂r=0 From symmetry—center not radially distorted.
B fr(r,z)=0
B fz(r,0)=P constant pressure or B fz(0,0)=F force at center.
These equations may be solved for several cases using Finite Element Analysis software, and representative results are displayed in
III. Deformation Function for Correcting Index Mismatch Aberrations and, Change Focus
Equations may be used to determine the deformation function needed by a deformable mirror. For example, equations for wavefront correction required for a particular case of live sample microscopy and focusing into optical recording media may be provided. A phase-shift function responsible for spherical aberrations induced by mismatched index of refraction, such as between oil-immersion objective in a microscope and water-embedded live biological sample or between air lens and plastic recording media, may be provided. The phase-shift as a function of emergence angle from a point within the sample at a given depth determines the deformation function of a mirror located in the microscope pupil plane (or any other plane conjugated to it).
The following is a specific example for the generation by a deformable mirror of the above described phase shifts for wavefronts in microscopy, where the thickness of the disk mirror is fitted to create correction for aberrations induced by sample depth inside a refractive medium different then the cover glass and objective immersion medium. In the pupil plane, where the mirror is placed, the angle of emergence from the specimen, θ is proportional to the radial coordinate of the mirror, r.
Phase(θ)=Dn cos θ′ (33)
With the values: D=5 m n=1.518 n′=1.38 and n sin θ=n′sin θ′ for
The second curves 2 and 4 plot the phases added to a wavefront focused into depth D=10 micrometers, that will only correct the aberrations due to index mismatch according to:
Phase(θ)=D(n′cos θ′-n cos θ) (34)
As observed, correction for aberration and changing focus requires about twice the phase shift as just for correcting aberrations.
These equations are derived from the '070 application as well as a paper entitled “Modeling the Application of Adaptive Optics to Wide-Field Microscope Live Imaging”, J. Microscopy 226:33-42 (2007), Z. Kam, P. Kner, D. Agard, and J. W. Sedat, which is incorporated herein by reference.
The present application claims the benefit of U.S. Provisional Patent Application Ser. No. 61/024,726, filed Jan. 30, 2008, the contents of which are hereby incorporated by reference in their entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US2009/032592 | 1/30/2009 | WO | 00 | 2/23/2011 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2009/097503 | 8/6/2009 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3972600 | Cobarg | Aug 1976 | A |
5986795 | Chapman et al. | Nov 1999 | A |
6108121 | Mansell et al. | Aug 2000 | A |
6843572 | Shiraishi | Jan 2005 | B2 |
7229178 | Headley et al. | Jun 2007 | B1 |
20030214734 | Nishioka et al. | Nov 2003 | A1 |
20040223212 | Sakuma | Nov 2004 | A1 |
20040233553 | Shibata et al. | Nov 2004 | A1 |
20060103956 | Griffith et al. | May 2006 | A1 |
20070165312 | Aoki et al. | Jul 2007 | A1 |
20070258158 | Aoki et al. | Nov 2007 | A1 |
20070268592 | Kam et al. | Nov 2007 | A1 |
Number | Date | Country |
---|---|---|
9 293915 | Nov 1997 | JP |
2006 012286 | Jan 2006 | JP |
Entry |
---|
International Preliminary Report on Patentability dated Aug. 12, 2010 in PCT/US2009/032592. |
Extended European Search Report dated Oct. 17, 2011 issued in EP09705470.4. |
Number | Date | Country | |
---|---|---|---|
20110134552 A1 | Jun 2011 | US |
Number | Date | Country | |
---|---|---|---|
61024726 | Jan 2008 | US |