1. A laminated coil component comprising:
a magnetic section including stacked magnetic layers; and
a conductor section having a plurality of conductor pattern layers arranged between the magnetic layers, and the conductor pattern layers being interconnected in a coiled shape to pass through the magnetic layers, the conductor section being buried in the magnetic section,
the conductor section including a conductor containing silver,
the magnetic section including a sintered ferrite material containing Fe, Ni, Zn, and Cu, and
a ratio of Cu content in CuO in a near-conductor section region of the magnetic section to Cu content in CuO in a central region of the magnetic section is 0.2 to 0.5.
2. The laminated coil component according to claim 1, wherein the ratio of Cu content in CuO in the near-conductor section region of the magnetic section to Cu content in CuO in the central region of the magnetic section is 0.2 to 0.3.
3. The laminated coil component according to claim 1, wherein the Cu content in CuO in the central region of the magnetic section is 0.2 to 3 weight %.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A method for producing a high frame rate, high resolution and high contrast image, comprising:
a) transmitting a group of signals of energy weighted by single spatial frequency but may be of different phases or linear time delay toward an object to be imaged;
b) weighting receive signals from the object with multiple spatial frequencies, or by performing a spatial Fourier transform;
c) reconstructing a two- or three-dimensional image data set from the group of the transmitted signals weighted by the single spatial frequency or linear time delay, and the receive signals weighted with the multiple spatial frequencies or processed by the spatial Fourier transform; and,
d) reconstructing the high frame rate, high resolution and high contrast image from the image data set of step c.
2. A method for producing a high frame rate, high resolution and high contrast velocity vector image of an object where at least a part of the object is moving, comprising:
a) transmitting two or more groups of signals of energy weighted by single spatial frequency but may be of different phases or linear time delay-toward the object,
b) weighting receive signals from the object with multiple spatial frequencies or by performing a spatial Fourier transform;
c) reconstructing two- or three-dimensional image data sets from the groups of the transmitted signals weighted by the single spatial frequency or linear time delay, and the receive signals weighted with the multiple spatial frequencies or processed by the spatial Fourier transform;
d) using the image data sets to reconstruct:
a first set of flow velocity component images in a first direction, and
a second set of flow velocity component images in a second direction that is different from the first direction; and,
e) reconstructing the velocity vector image from the two sets of velocity component images.
3. The method of claim 1, wherein step a) each group may contain one or more signals, each of which is produced with one transmission.
4. The method of claim 1, in which the transmit group comprises one or more limited diffraction beams.
5. The method of claim 1, in which the received signal for echoes returned from all random scatterers within the object f( r0) is a linear superposition of those echo signals from individual point scatterers as follows:
R
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
t
)
=
\ue89e
1
2
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
\xd7
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue89e
\uf74d
\uf74e
\ue8a0
(
k
x
+
k
x
T
)
\ue89e
x
0
+
\uf74e
\ue8a0
(
k
y
+
k
y
T
)
\ue89e
y
0
+
\uf74e
\ue8a0
(
k
z
+
k
z
T
)
\ue89e
z
0
\ue89e
\ue89e
\uf74c
r
\u21c0
0
\ue89e
\uf74d
–
i
\ue89e
\ue89e
\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
\ue89e
1
2
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
\ue89e
F
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
\ue89e
\uf74d
–
i
\ue89e
\ue89e
\u03c9
\ue89e
\ue89e
t
\ue89e
\ue89e
\uf74c
k
.
(
8
)
6. The method of claim 5, in which the temporal Fourier transform (spectrum) of the received signal obtained as follows:
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue89e
\uf74d
\uf74e
\ue8a0
(
k
x
+
k
x
T
)
\ue89e
x
0
+
\uf74e
\ue8a0
(
k
y
+
k
y
T
)
\ue89e
y
0
+
\uf74e
\ue8a0
(
k
z
+
k
z
T
)
\ue89e
z
0
\ue89e
\ue89e
\uf74c
r
\u21c0
0
\ue89e
\ue89e
or
\ue89e
\ue89e
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
x
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
F
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
\ue89e
\ue89e
or
\ue89e
\ue89e
F
BL
\ue8a0
(
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
\ue8a0
(
\u03c9
)
.
(
10
)
7. The method of claim 6, in which a 2D Fourier transform of the echo signals in terms of both x1 and y1 over a transducer surface is as follows:
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue89e
\uf74d
\uf74ek
x
\ue89e
x
0
+
\uf74ek
y
\ue89e
y
0
+
\uf74ek
z
\ue89e
z
0
\ue89e
\uf74d
\uf74ek
x
T
\ue89e
x
0
+
\uf74ek
y
T
\ue89e
y
0
+
\uf74ek
z
T
\ue89e
z
0
\ue89e
\ue89e
\uf74c
r
\u21c0
0
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue8a0
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
\ue89e
\uf74d
\uf74ek
x
\ue89e
x
0
+
\uf74ek
y
\ue89e
y
0
+
\uf74ek
z
\ue89e
z
0
\ue89e
\uf74d
\uf74ek
x
T
\ue89e
x
0
+
\uf74ek
y
T
\ue89e
y
0
+
\uf74ek
z
T
\ue89e
z
)
\ue89e
\ue89e
\uf74c
r
\u21c0
0
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue8a0
\u03a6
~
Array
R
\ue8a0
(
r
\u21c0
0
,
\u03c9
)
\ue89e
\uf74d
\uf74ek
x
T
\ue89e
x
0
+
\uf74ek
y
T
\ue89e
y
0
+
\uf74ek
z
T
\ue89e
z
)
\ue89e
\ue89e
\uf74c
r
\u21c0
0
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue8a0
\ue529
x
1
,
y
1
\ue89e
{
E
~
\ue8a0
(
x
1
,
y
1
;
r
\u21c0
0
;
\u03c9
)
}
\ue89e
\ue89e
\uf74d
\uf74ek
x
T
\ue89e
x
0
+
\uf74ek
y
T
\ue89e
y
0
+
\uf74ek
z
T
\ue89e
z
0
\ue89e
\uf74c
r
\u21c0
0
=
\ue529
x
1
,
y
1
\ue89e
{
\u222b
V
\ue89e
f
\ue8a0
(
r
\u21c0
0
)
\ue89e
A
\ue8a0
(
k
)
c
\ue89e
\uf74d
\uf74ek
x
T
\ue89e
x
0
+
\uf74ek
y
T
\ue89e
y
0
+
\uf74ek
z
T
\ue89e
z
0
\ue89e
\ue89e
E
~
\ue8a0
(
x
1
,
y
1
;
r
\u21c0
0
;
\u03c9
)
\ue89e
\uf74c
r
\u21c0
0
}
.
(
13
)
8. The method of claim 1, wherein four limited-diffraction array beams are transmitted (fix both kxT and kyT) in each group as follows:
\u03a6
Array
\ue8a0
(
1
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
cos
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
cos
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
26
)
\u03a6
Array
\ue8a0
(
2
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
cos
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
sin
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
27
)
\u03a6
Array
\ue8a0
(
3
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
sin
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
cos
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
\ue89e
and
(
28
)
\u03a6
Array
\ue8a0
(
4
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
sin
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
sin
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
29
)
wherein four coverage areas are obtained in a spatial Fourier space of f( r0) from combinations of the four echo signals, and wherein denoting the Fourier transform of the four echo signals as {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(1)(\u03c9), {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(2)(\u03c9), {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(3)(\u03c9), and {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(4)(\u03c9), corresponding to (26)-(29), respectively, provides:
F
BL
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
–
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
30
)
F
BL
\ue8a0
(
k
x
+
k
x
T
,
k
y
–
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
+
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
31
)
F
BL
\ue8a0
(
k
x
–
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
+
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
32
)
.
F
BL
\ue8a0
(
k
x
–
k
x
T
,
k
y
–
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
–
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
33
)
.
9. The method of claim 1, further comprising:
using (10) and (11) to directly give a relationship between the 3D Fourier transform of measured echo signals at a transducer surface and the 3D spatial Fourier transform of the object function for a steered plane wave transmission with a fixed Axicon angle (steering angle for plane waves), \u03b6T, of X wave and azimuthal angle, \u03b8T,
obtaining the spatial Fourier transform of the object function, and
using (17) to reconstruct images with an inverse 3D Fourier transform; wherein, for steered plane waves, the relationship of the parameters between the Fourier transform of the echoes and the object function is obtained:
{
k
x
\u2032
=
k
x
+
k
\ue89e
\ue89e
sin
\ue89e
\ue89e
\u03b6
T
\ue89e
cos
\ue89e
\ue89e
\u03b8
T
k
y
\u2032
=
k
y
+
k
\ue89e
\ue89e
sin
\ue89e
\ue89e
\u03b6
T
\ue89e
sin
\ue89e
\ue89e
\u03b8
T
k
z
\u2032
=
k
z
+
k
\ue89e
\ue89e
cos
\ue89e
\ue89e
\u03b6
T
=
k
2
–
k
x
2
–
k
y
2
+
k
\ue89e
\ue89e
cos
\ue89e
\ue89e
\u03b6
T
\u2265
0
.
(
34
)
10. The method of claim 1, wherein, for a 2D image reconstruction, using a 2D imaging formula:
FBL(k\u2032x,k\u2032z)=c2H(k){tilde over (R)}k\u2032x,k\u2032z(\u03c9),\u2003\u2003(35)
where
{
k
x
\u2032
=
k
x
+
k
x
T
k
z
\u2032
=
k
z
+
k
z
T
=
k
2
–
k
x
2
+
k
2
–
k
x
T
2
\u2265
0
.
(
36
)
11. The method of claim 1, wherein step c) includes Fourier transforming along a time domain of one or more of: i) the weighted transmitted signal, or ii) the spatial Fourier transform, whereby a multi-dimensional k-space data set is formed.
12. The method of claim 1, wherein step c) includes:
i) interpolating a multi-dimensional k-space data set to produce rectilinear multi-dimensional k-space data sets; and,
ii) performing inverse Fourier transformations of the interpolated rectilinear multi-dimensional k-space data sets along each of its dimensions to produce the image data set.
13. The method of claim 12, wherein the k-space data sets have two- or three-dimensions, and the inverse Fourier transformation is performed along each of the two- or three-dimensions to produce a two- or three-dimensional image data set.
14. The method of claim 1, or wherein the image data set of step c) is reconstructed using the formula kz\u2032=k+kzT.
15. The method of claim 1, wherein the image data set of step c) is reconstructed using
{
k
x
\u2032
=
k
x
+
k
x
T
k
y
\u2032
=
k
y
+
k
y
T
k
z
\u2032
=
k
z
+
k
z
T
=
k
2
–
k
x
2
–
k
y
2
+
k
2
–
k
x
T
2
–
k
y
T
2
\u2265
0
.
16. The method of claim 1, wherein the image data set of step c) is reconstructed using
{
k
x
=
k
x
\u2032
–
k
x
T
k
=
(
k
z
\u20322
+
k
x
T
2
–
(
k
x
\u2032
–
k
x
T
)
2
)
2
+
4
\ue89e
\ue89e
k
z
\u20322
\ue8a0
(
k
x
\u2032
–
k
x
T
)
2
2
\ue89e
k
z
\u2032
,
for producing a two-dimensional image.
17. The method of claim 1, wherein steps a)-c) are performed a plurality of times.
18. The method of claim 1, wherein the spatial frequency is non-uniform.
19. The method of claim 1, further including combining a plurality of the single transmit spatial frequency signals and the multiple receive spatial frequency signals to increase signal-to-noise ratio, image resolution, image contrast, and reduce sidelobes for the image.
20. The method of claim 2, further including combining a plurality of the multiple transmit spatial frequency signals and the multiple receive spatial frequency signals to increase signal-to-noise ratio, image resolution, image contrast, and reduce sidelobes for the image.
21. The method of claim 1, in which the step a) and step b) are performed using the same transducer array.
22. The method of claim 1, in which the multiple receive signals are Fourier transformed over a single transducer aperture.
23. The method of claim 1, in which the multiple receive signals are superposed coherently with corresponding or other transmission weightings or steered angles to enhance resolutions and contrast, and to reduce sidelobes.
24. The method of claim 1, in which the multiple receive signals are superposed incoherently with corresponding or other transmission weightings or steered angles to reduce speckle formation.
25. The method of claim 1, in which one group of transmitted signals is used to reconstruct an image.
26. The method of claim 2, in which at least two groups of transmitted signals are used to reconstruct an image.
27. The method of claim 1, in which a single transmitter is used to produce weightings for different transducer elements.
28. The method of claim 1, in which more than one transmitter is used to produce weightings for different transducer elements.
29. The method of claim 1, in which harmonic andor elastic images are produced.
30. The method of claim 1, in which a physiological functional image is reproduced.
31. The method of claim 1, in which at least a part of the object to be imaged is moving.
32. The method of claim 2, in which the first direction is perpendicular with respect to a surface transmitting the signals.
33. The method of claim 2, in which a single image is used to construct the first and second sets of flow velocity component images by rotating the single image and interpolating data from the rotated image.
34. The method of claim 2, in which pulse Doppler or color flow Doppler method is used to reconstruct images.
35. The method of claim 1, in which the transmitted signals comprise sine and cosine spatially weighted signals.
36. An apparatus for producing a high frame rate, high resolution and high contrast image of an object, comprising:
a) a device configured to:
i) transmit one or more groups of signals of energy weighted by single spatial frequency but may be of different phases or linear time delay toward an object to be imaged; and
ii) receive by weighting receive signals from the object with multiple spatial frequencies, or by performing a spatial Fourier transform;
b) a device configured to reconstruct a two- or three-dimensional image data set from the group of the transmitted signals weighted by the single spatial frequency or linear time delay, and the receive signals weighted with the multiple spatial frequencies or processed by the spatial Fourier transform; and,
c) a device configured to reconstruct the high frame rate, high resolution and high contrast image from the image data set.
37. The apparatus of claim 36, wherein the transmitreceive device comprises a transducer array configured to form one or more limited diffraction transmitted beams.
38. The apparatus of claim 37, wherein the transmitreceive device comprises a transducer array configured to form one or more steered transmitted beams.
39. The apparatus of claim 36, wherein the device b) is configured to: i) Fourier transform the weighted echo signals to form at least a first multi-dimensional k-space data set.
40. The apparatus of claim 39 wherein device c) is further configured to: ii) interpolate one or more multi-dimensional k-space data sets to produce rectilinear multi-dimensional k-space data sets; and, iii) perform inverse Fourier transformations of the interpolated k-space data sets along each of its dimensions, whereby the image data set is produced.
41. The apparatus of claim 36, wherein the transmitreceive device comprising separate elements in a transducer array arranged in a one- or two-dimensional array.
42. The apparatus of claim 36, wherein the transmitreceive device is configured to steer one or more plane waves at one or more different angles.
43. The apparatus of claim 36, wherein a single transmitreceive device is configured to produce weightings for different transducer elements.
44. The apparatus of claim 36, wherein the transmitreceive device comprises a transducer having a single aperture, and wherein the receive signals are Fourier transformed over the single transducer aperture.
45. The apparatus of claim 36, wherein the transmitreceive device transmits more than one beam at the same spatial frequency or steering angle in order to obtain the velocity component image and to improve signal-to-noise ratio.
46. The method of claim 2, wherein step a) each group may contain one or more signals, each of which is produced with one transmission.
47. The method of claim 2, in which the transmit group comprises one or more limited diffraction beams.
48. The method of claim 2, in which the received signal for echoes returned from all random scatterers within the object f( r0) is a linear superposition of those echo signals from individual point scatterers as follows:
R
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
t
)
=
1
2
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue89e
(
k
)
c
\xd7
\u222b
V
\ue89e
f
\ue8a0
(
r
->
0
)
\ue89e
\uf74d
\uf74e
\ue8a0
(
k
x
+
k
x
T
)
\ue89e
x
0
+
\uf74e
\ue8a0
(
k
y
+
k
y
T
)
\ue89e
y
0
+
\uf74e
\ue8a0
(
k
z
+
k
z
T
)
\ue89e
z
0
\ue8a0
(
\uf74c
r
_
)
0
\ue89e
\uf74d
–
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
\ue89e
=
1
2
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue89e
(
k
)
c
\ue89e
F
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
\ue89e
\uf74d
–
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
(
8
)
49. The method of claim 48, in which the temporal Fourier transform (spectrum) of the received signal obtained as follows:
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
\u222b
V
\ue89e
f
(
r
->
0
)
\ue89e
\uf74d
\uf74e
\ue8a0
(
k
x
+
k
x
T
)
\ue89e
x
0
+
\uf74e
\ue8a0
(
k
y
+
k
y
T
)
\ue89e
y
0
+
\uf74e
\ue8a0
(
k
z
+
k
z
T
)
\ue89e
z
0
\ue89e
\uf74c
r
->
0
\ue89e
\ue89e
or
\ue89e
\ue89e
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
F
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
\ue89e
\ue89e
or
\ue89e
\ue89e
F
BL
\ue8a0
(
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
\ue8a0
(
\u03c9
)
.
(
10
)
50. The method of claim 49, in which a 2D Fourier transform of the echo signals in terms of both x1 and y1 over a transducer surface is as follows:
R
~
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
\ue8a0
(
\u03c9
)
=
A
\ue8a0
(
k
)
\ue89e
T
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
c
2
\xd7
\u222b
V
\ue89e
f
(
r
->
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
\ue89e
z
0
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
T
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
T
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74c
r
->
0
\ue89e
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
(
r
->
0
)
\ue8a0
T
\ue8a0
(
k
)
\ue89e
H
\ue89e
(
k
)
c
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
\ue89e
z
0
\ue89e
\uf74c
\uf74d
\uf74e
\ue89e
\ue89e
k
x
T
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
T
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74c
r
->
0
\ue89e
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
(
r
->
0
)
\u03a6
~
Array
R
\ue8a0
(
r
->
0
,
\u03c9
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
\ue89e
z
0
\ue89e
\uf74c
r
->
0
\ue89e
=
A
\ue8a0
(
k
)
c
\ue89e
\u222b
V
\ue89e
f
(
r
->
0
)
\ue569
x
1
,
y
1
\ue89e
{
E
~
\ue8a0
(
x
1
,
y
1
;
r
->
0
;
\u03c9
)
}
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
T
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
T
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74c
r
->
0
\ue89e
=
\ue569
x
1
,
y
1
\ue89e
{
\u222b
V
\ue89e
f
\ue8a0
(
r
->
0
)
\ue89e
A
\ue8a0
(
k
)
c
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
x
T
\ue89e
x
0
+
\uf74e
\ue89e
\ue89e
k
y
T
\ue89e
y
0
+
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
E
~
\ue8a0
(
x
1
,
y
1
;
r
_
0
;
\u03c9
)
\ue89e
\uf74c
r
->
0
}
.
(
13
)
51. The method of claim 2, wherein four limited-diffraction array beams are transmitted (fix both kxT and kyT) in each group as follows:
\u03a6
Array
\ue8a0
(
1
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
cos
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
cos
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
26
)
\u03a6
Array
\ue8a0
(
2
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
cos
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
sin
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
27
)
\u03a6
Array
\ue8a0
(
3
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
sin
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
cos
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
\ue89e
and
(
28
)
\u03a6
Array
\ue8a0
(
4
)
T
(
r
->
0
,
t
)
=
1
2
\ue89e
\ue89e
\u03c0
\ue89e
\u222b
–
\u221e
\u221e
\ue89e
A
\ue8a0
(
k
)
\ue89e
H
\ue8a0
(
k
)
\ue89e
sin
\ue8a0
(
k
x
T
\ue89e
x
0
)
\ue89e
sin
\ue8a0
(
k
y
T
\ue89e
y
0
)
\ue89e
\uf74d
\uf74e
\ue89e
\ue89e
k
z
T
\ue89e
z
0
\ue89e
\uf74d
\uf74e\u03c9
\ue89e
\ue89e
t
\ue89e
\uf74c
k
,
(
29
)
wherein four coverage areas are obtained in a spatial Fourier space of f( r0) from combinations of the four echo signals, and wherein denoting the Fourier transform of the four echo signals as {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(1)(\u03c9), {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(2)(\u03c9), {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(3)(\u03c9), and {tilde over (R)}k\u2032x,k\u2032y,k\u2032z(4)(\u03c9), and corresponding to (26)-(29), respectively, provides:
F
BL
\ue8a0
(
k
x
+
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
–
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
30
)
F
BL
\ue8a0
(
k
x
+
k
x
T
,
k
y
–
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
+
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
31
)
F
BL
\ue8a0
(
k
x
–
k
x
T
,
k
y
+
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
+
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
+
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
32
)
.
F
BL
\ue8a0
(
k
x
–
k
x
T
,
k
y
–
k
y
T
,
k
z
+
k
z
T
)
=
c
2
\ue89e
H
\ue8a0
(
k
)
\ue89e
(
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
1
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
2
)
\ue8a0
(
\u03c9
)
–
\uf74e
\ue89e
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
3
)
\ue8a0
(
\u03c9
)
–
R
~
k
x
\u2032
,
k
y
\u2032
,
k
z
\u2032
(
4
)
\ue8a0
(
\u03c9
)
)
,
(
33
)
.
52. The method of claim 2, further comprising:
using (10) and (11) to directly give a relationship between the 3D Fourier transform of measured echo signals at a transducer surface and the 3D spatial Fourier transform of the object function for a steered plane wave transmission with a fixed Axicon angle (steering angle for plane waves), \u03b6T, of X wave and azimuthal angle, \u03b8T,
obtaining the spatial Fourier transform of the object function, and
using (17) to reconstruct images with an inverse 3D Fourier transform; wherein, for steered plane waves, the relationship of the parameters between the Fourier transform of the echoes and the object function is obtained:
{
k
x
\u2032
=
k
x
+
k
\ue89e
\ue89e
sin
\ue89e
\ue89e
\u03b6
T
\ue89e
cos
\ue89e
\ue89e
\u03b8
T
k
y
\u2032
=
k
y
+
k
\ue89e
\ue89e
sin
\ue89e
\ue89e
\u03b6
T
\ue89e
sin
\ue89e
\ue89e
\u03b8
T
k
z
\u2032
=
k
z
+
k
\ue89e
\ue89e
cos
\ue89e
\ue89e
\u03b6
T
=
k
2
–
k
x
2
–
k
y
2
+
k
\ue89e
\ue89e
cos
\ue89e
\ue89e
\u03b6
T
\u2265
0
.
(
34
)
53. The method of claim 2, wherein, for a 2D image reconstruction, using a 2D imaging formula:
FBL(k\u2032x,k\u2032z)=c2H(k){tilde over (R)}k\u2032x,k\u2032z(\u03c9),\u2003\u2003(35)
where
{
k
x
\u2032
=
k
x
+
k
x
T
k
z
\u2032
=
k
z
+
k
z
T
=
k
2
–
k
x
2
+
k
2
–
k
x
T
2
\u2265
0
.
(
36
)
54. The method of claim 2, wherein step c) includes Fourier transforming along a time domain of one or more of: i) the weighted transmitted signal, or ii) the spatial Fourier transform, whereby a multi-dimensional k-space data set is formed.
55. The method of claim 2, wherein step c) includes:
i) interpolating a multi-dimensional k-space data set to produce rectilinear multi-dimensional k-space data sets; and,
ii) performing inverse Fourier transformations of the interpolated rectilinear multi-dimensional k-space data sets along each of its dimensions to produce the image data set.
56. The method of claim 55, wherein the k-space data sets have two- or three-dimensions, and the inverse Fourier transformation is performed along each of the two- or three-dimensions to produce a two- or three-dimensional image data set.
57. The method of claim 2, wherein the image data set of step c) is reconstructed using the formula kz\u2032=k+kzT.
58. The method of claim 2, wherein the image data set of step c) is reconstructed using
{
k
x
\u2032
=
k
x
+
k
x
T
k
y
\u2032
=
k
y
+
k
y
T
k
z
\u2032
=
k
z
+
k
z
T
=
k
2
–
k
x
2
–
k
y
2
+
k
2
–
k
x
T
2
–
k
y
T
2
\u2265
0
.
59. The method of claim 2, wherein the image data set of step c) is reconstructed using
{
k
x
=
k
x
\u2032
–
k
x
T
k
=
(
k
z
\u20322
+
k
x
T
2
–
(
k
x
\u2032
–
k
x
T
)
2
)
2
+
4
\ue89e
\ue89e
k
z
\u20322
\ue8a0
(
k
x
\u2032
–
k
x
T
)
2
2
\ue89e
k
z
\u2032
,
for producing a two-dimensional image.
60. The method of claim 2, wherein steps a)-c) are performed a plurality of times.
61. The method of claim 2, wherein the spatial frequency is non-uniform.
62. The method of claim 2, in which the step a) and step b) are performed using the same transducer array.
63. The method of claim 2, in which the multiple receive signals are Fourier transformed over a single transducer aperture.
64. The method of claim 2, in which the multiple receive signals are superposed coherently with corresponding or other transmission weightings or steered angles to enhance resolutions and contrast, and to reduce sidelobes.
65. The method of claim 2, in which the multiple receive signals are superposed incoherently with corresponding or other transmission weightings or steered angles to reduce speckle formation.
66. The method of claim 2, in which a single transmitter is used to produce weightings for different transducer elements.
67. The method of claim 2, in which more than one transmitter is used to produce weightings for different transducer elements.
68. The method of claim 2, in which harmonic andor elastic images are produced.
69. The method of claim 2, in which a physiological functional image is reproduced.
70. The method of claim 2, in which at least a part of the object to be imaged is moving.
71. The method of claim 2, in which the transmitted signals comprise sine and cosine spatially weighted signals.