The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
대리인 / 주소
McGroary, James J.
인용정보
피인용 횟수 :
3인용 특허 :
11
초록▼
A coil system for a plasmoid thruster includes a bias coil, a drive coil and field coils. The bias and drive coils are interleaved with one another as they are helically wound about a conical region. A first field coil defines a first passage at one end of the conical region, and is connected in ser
A coil system for a plasmoid thruster includes a bias coil, a drive coil and field coils. The bias and drive coils are interleaved with one another as they are helically wound about a conical region. A first field coil defines a first passage at one end of the conical region, and is connected in series with the bias coil. A second field coil defines a second passage at an opposing end of the conical region, and is connected in series with the bias coil.
대표청구항▼
What is claimed as new and desired to be secured by Letters Patent of the United States is: 1. A coil system for a plasmoid thruster, comprising: a bias coil defined by a first plurality of conductors positioned parallel to one another and helically wound about a conical region, said first pluralit
What is claimed as new and desired to be secured by Letters Patent of the United States is: 1. A coil system for a plasmoid thruster, comprising: a bias coil defined by a first plurality of conductors positioned parallel to one another and helically wound about a conical region, said first plurality of conductors connected to one another in a parallel configuration; a drive coil defined by a second plurality of conductors positioned parallel to one another, interleaved with said first plurality of conductors, and helically wound about said conical region, said second plurality of connected to one another in a parallel configuration; a first field coil (i) defining a first passage at one end of said conical region, and (ii) connected in series with said bias coil; and a second field coil (i) defining a second passage at an opposing end of said conical region, and (ii) connected in series with said bias coil. 2. A coil system as in claim 1 wherein said one end of said conical region is smaller in diameter than said opposing end of said conical region, said coil system further comprising a preionizer coil positioned in said conical region adjacent said one end, said preionizer coil defining a third passage therethrough aligned with said first passage. 3. A coil system as in claim 1 further comprising means for supplying voltage independently to (i) a first circuit that includes a series combination of said first field coil, said bias coil and said second field coil, and (ii) a second circuit that includes said drive coil. 4. A coil system as in claim 1 further comprising a conically-shaped housing defining said conical region and supporting at least said bias coil and said drive coil. 5. A coil system as in claim 4 wherein said housing comprises an electrically insulating material. 6. A coil system as in claim 4 wherein said housing comprises a ceramic material. 7. A coil system as in claim 4 wherein said housing has parallel grooves formed therein and wrapped thereabout in a helical fashion with each of said grooves having one of said first plurality of conductors or one of said second plurality of conductors fitted therein. 8. A coil system for a plasmoid thruster, comprising: a biasing circuit that includes a first field coil defining a first passage therethrough, a second field coil defining a second passage therethrough larger than said first passage and coaxially aligned therewith, and a biasing coil defined by N parallel conductors helically wound about a conical region between said first field coil and said second field coil, said N parallel conductors having N ends terminating at each axial end of said conical region with said N ends at each said axial end being electrically coupled to one another, said biasing circuit being formed by a series combination of said first field coil, said biasing coil, and said second field coil; and a drive circuit that includes M parallel conductors helically wound about said conical region and interleaved with said N parallel conductors, said M parallel conductors having M ends terminating at each said axial end of said conical region with said M ends at each said axial end being electrically coupled to one another. 9. A coil system as in claim 8 wherein N=M. 10. A coil system as in claim 8 wherein said N parallel conductors interleaved with said M parallel conductors comprise (N+M) evenly-spaced parallel conductors. 11. A coil system as in claim 8 further comprising a preionizer coil positioned in said conical region at one said axial end thereof. 12. A coil system as in claim 8 further comprising: first voltage supply means completing said biasing circuit; and second voltage supply means completing said drive circuit. 13. A coil system as in claim 8 further comprising a conically-shaped housing defining said conical region and supporting said first field coil, said N parallel conductors, said M parallel conductors, and said second field coil. 14. A coil system as in claim 13 wherein said housing comprises an electrically insulating material. 15. A coil system as in claim 13 wherein said housing comprises a ceramic material. 16. A coil system as in claim 13 wherein said housing has parallel grooves formed therein and wrapped thereabout in a helical fashion with each of said grooves having one of said N parallel conductors or one of said M parallel conductors fitted therein. 17. A coil system for a plasmoid thruster, comprising: means for defining a conical region open at first and second axial ends thereof; a biasing circuit that includes a first field coil defining a first passage therethrough and positioned adjacent to said first axial end of said conical region, a second field coil defining a second passage therethrough larger than said first passage and positioned adjacent to said second axial end of said conical region wherein said first field coil is axially aligned with said second field coil, and a biasing coil defined by N parallel conductors helically wound about said means, said N parallel conductors having N ends terminating at each of said first axial end of said conical region and said second axial end of said conical region with said N ends at each of said first axial end and said second axial end being electrically coupled to one another, said biasing circuit being formed by a series combination of said first field coil, said biasing coil, and said second field coil; and a drive circuit that includes M parallel conductors helically wound about said means and interleaved with said N parallel conductors, said M parallel conductors having M ends terminating at each of said first axial end of said conical region and said second axial end of said conical region with said M ends at each of said first axial end and said second axial end being electrically coupled to one another. 18. A coil system as in claim 17 wherein N=M. 19. A coil system as in claim 17 wherein said N parallel conductors interleaved with said M parallel conductors comprise (N+M) evenly-spaced parallel conductors. 20. A coil system as in claim 17 further comprising a preionizer coil positioned in said conical region at said first axial end thereof. 21. A coil system as in claim 17 further comprising: first voltage supply means completing said biasing circuit; and second voltage supply means completing said drive circuit. 22. A coil system as in claim 17 wherein said means comprises an electrically insulating material. 23. A coil system as in claim 17 wherein said means comprises a ceramic material. 24. A coil system as in claim 17 wherein said means has parallel grooves formed therein and wrapped thereabout in a helical fashion with each of said grooves having one of said N parallel conductors or one of said M parallel conductors fitted therein.
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이 특허에 인용된 특허 (11)
Paul M. Koloc, Apparatus for generating a compound plasma configuration with multiple helical conductor elements.
Dailey Charles L. (Palos Verdes Estates CA) Lovberg Ralph H. (San Diego CA) Sackheim Robert L. (Rancho Palos Verdes CA) Biess John J. (Canoga Park CA), Hybrid chemical/electromagnetic propulsion system.
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