1. A plant of soybean variety 01046668, wherein a sample of seed of said variety has been deposited under ATCC Accession No. ______.
2. A plant part of the plant of claim 1, wherein the plant part comprises at least one cell of said plant.
3. The plant part of claim 2, further defined as pollen, a meristem, a cell, or an ovule.
4. A seed of soybean variety 01046668, wherein a sample of seed of said variety has been deposited under ATCC Accession No. ______.
5. A method of producing soybean seed, wherein the method comprises crossing the plant of claim 1 with itself or a second soybean plant.
6. The method of claim 5, wherein the method is further defined as comprising crossing the plant of soybean variety 01046668 with a second, distinct soybean plant to produce an F1 hybrid soybean seed.
7. An F1 hybrid soybean seed produced by the method of claim 6.
8. An F1 hybrid soybean plant produced by growing the seed of claim 7.
9. A composition comprising the seed of claim 4 comprised in plant seed growth media, wherein a sample of seed of said variety has been deposited under ATCC Accession No. ______.
10. The composition of claim 9, wherein the growth media is soil or a synthetic cultivation medium.
11. A plant produced by introducing a single locus conversion into soybean variety 01046668, or a selfed progeny thereof comprising the single locus conversion, wherein the single locus conversion was introduced into soybean variety 01046668 by backcrossing or genetic transformation and wherein a sample of seed of soybean variety 01046668 has been deposited under ATCC Accession No. ______.
12. The plant of claim 11, wherein the single locus conversion comprises a transgene.
13. A seed that produces the plant of claim 11.
14. The seed of claim 13, wherein the single locus confers a trait selected from the group consisting of male sterility, herbicide tolerance, insect resistance, pest resistance, disease resistance, modified fatty acid metabolism, abiotic stress resistance, altered seed amino acid composition, site-specific genetic recombination, and modified carbohydrate metabolism.
15. The seed of claim 13, wherein the single locus confers tolerance to an herbicide selected from the group consisting of glyphosate, sulfonylurea, imidazalinone, dicamba, glufosinate, phenoxy propionic acid, cyclohexanedione, triazine, benzonitrile, PPO-inhibitor herbicides, and bromoxynil.
16. The seed of claim 13, wherein the single locus conversion comprises a transgene.
17. The method of claim 6, wherein the method further comprises:
(a) crossing a plant grown from said F1 hybrid soybean seed with itself or a different soybean plant to produce a seed of a progeny plant of a subsequent generation;
(b) growing a progeny plant of a subsequent generation from said seed of a progeny plant of a subsequent generation and crossing the progeny plant of a subsequent generation with itself or a second plant to produce a progeny plant of a further subsequent generation; and
(c) repeating steps (a) and (b) using said progeny plant of a further subsequent generation from step (b) in place of the plant grown from said F1 hybrid soybean seed in step (a), wherein steps (a) and (b) are repeated with sufficient inbreeding to produce an inbred soybean plant derived from the soybean variety 01046668.
18. The method of claim 17, comprising crossing said inbred soybean plant derived from the soybean variety 01046668 with a plant of a different genotype to produce a seed of a hybrid soybean plant derived from the soybean variety 01046668.
19. A method of producing a commodity plant product comprising collecting the commodity plant product from the plant of claim 1.
20. The method of claim 19, wherein the commodity plant product is protein concentrate, protein isolate, grain, soybean hulls, meal, flour, or oil.
21. A soybean commodity plant product produced by the method of claim 20, wherein the commodity plant product comprises at least one cell of soybean variety 01046668.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
What is claimed is:
1. A multi-wave-reflector antenna dish, comprising:
a reflector with a superquadric projected aperture, a minimal dish surface, simultaneously receiving signals from a plurality of satellites at fixed angles from each other, and producing a plurality of corresponding focusing waves sharing approximate radiation fields and having properties meeting requirements for satellite communication reception; and a
plurality of LNBF modules positioned on the focal plane of the said reflector to receive said focusing waves.
2. An antenna dish of claim 1, wherein said reflector with a superquadric projected aperture is formed from projected aperture cutting on a paraboloid that satisfies an equation of X 2Y 24fz with focus f.
3. An antenna dish of claim 2, wherein the boundary of said superquadric used for projected aperture cutting satisfies an equation, XA n(YB)B n1, where A is the mapping horizontal radius of the said superquadric aperture onto the XY plane, B is the mapping vertical radius of the superquadric aperture onto the XY plane, and n the coefficient of the equation with range from 2 to 3.
4. An antenna dish of claim 3, wherein said superquadric is an ellipse when n2.
5. An antenna dish of claim 3, wherein said superquadric is a super ellipse when n>2.
6. An antenna dish of claim 3, wherein the said plurality of LNBF modules, have angles of elevation ranging from 35.73 to 43.2 degrees and are arranged in a line within a distance of 2.6 inches from the dish center on the focal plane of said paraboloid with an f of 12 inches.
7. An antenna dish of claim 1, wherein said requirements for satellite communication reception include (a) each focusing wave has gain higher than 34.0 dB and a sidelobe level lower than 25 dB, and (b) gain differential between the focusing waves is less than 3%.
8. An antenna dish of claim 3, wherein said requirements for satellite communication reception are met when said superquadric is with an n2.1, the mapping horizontal radius onto XY plane is 11.25 inches and the mapping vertical radius onto XY plane is 8.75 inches.
9. An antenna dish of claim 8, wherein the said antenna dish simultaneously receives signals transmitted from three satellites positioned within a range of 18 degrees longitude (w101, w110, w119).
10. An antenna dish of claim 1, wherein said reflector with a superquadric projected aperture is formed by process including, projecting said superquadric on the paraboloid, projected aperture cutting and surface distortion of the aperture.
11. An antenna dish of claim 10, further including the generalized diffraction synthesis technique to complete said surface distortion.
12. A shaping method for an antenna dish having a reflector with super ellipse projected aperture, employed for receiving signals from at least three satellites; and under the condition of a minimal dish area, simultaneously receiving signals transmitted from satellites positioned within a certain range of angles thus producing a plurality of focusing waves respectively with properties that meet the requirements for satellite communication reception, comprising the steps:
(1) setting up requirements for radiation pattern;
(2) setting up initial configuration of the reflector shape;
(3) analyzing a radiation pattern;
(4) verifying whether pattern requirements established in step (1) are met; and
(5) if not, adjusting aperture coefficients and repeating step (4).
13. A shaping method for an antenna dish of claim 12, wherein said reflector with a super ellipse projected aperture is formed from a projected aperture cutting on a paraboloid that satisfies an equation of X 2Y 24fz with focus f.
14. A shaping method for an antenna dish of claim 13, wherein the boundary of superquadric used for projected aperture cutting satisfies an equation, XA n(YB)B n1, where A is the mapping horizontal radius of the said superquadric aperture onto the XY plane, B is the mapping vertical radius of the superquadric aperture onto the XY plane, and n the coefficient of the equation with range from 2 to 3.
15. A shaping method for an antenna dish of claim 12, wherein the requirements of radiation pattern in step (1) include (a) each focusing wave has gain higher than 34.0 dB and a sidelobe level lower than 25 dB, and (b) gain differential between the focusing waves is less than 3%.
16. A construction method for an antenna dish of claim 12, wherein the initial configuration for the reflector shape in step (2) is a plurality of LNBF modules, with angles of elevation ranging from 35.73 to 43.2 degrees, arranged in a line, within a distance of 2.6 inches from the dish center on the focal plane of said paraboloid, with an f of 12 inches.
17. A construction method for an antenna dish of claim 14, wherein the n of the said equation is 2.1, the horizontal radius mapped onto XY plane is 11.25 inches and the vertical radius mapped onto XY plane is 8.75 inches.
18. A construction method for an antenna dish of claim 17, wherein said antenna dish simultaneously receives signals transmitted from three satellites positioned within a range of 18 degrees longitude (w101, w110, w119).