IP Library Granted Patent US 7,301,095
Granted Patent B2
US 7,301,095 · App. 11/249,143 · Granted Nov 27, 2007

Solar cell array

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Quick Facts
Patent No.
US 7,301,095
App. No.
11/249,143
Granted
Nov 27, 2007
Kind
B2
Abstract

A solar panel for a spacecraft has a base with a face, and at least one row of solar cells and at least one elongated reflector are mounted on the face of the base. The reflectors and the rows are mounted generally parallel to each other in an alternating fashion. The reflector has first and second reflecting sides when the reflector is in a deployed position. The reflector is mounted so that the first side of the reflector is adjacent to a row of solar cells and reflects radiation incident on the first side onto the adjacent row of solar cells when the reflector is in a deployed position. Preferably, a plurality of rows and a plurality of reflectors are mounted on the face of the base, with at least one of the reflectors being disposed between two adjacent rows of solar cells.

Claims (44)

1. A solar panel comprising:

a base having a face;

a row of solar cells mounted on the face of the base; and

an elongated, collapsible, self-deploying reflector having a first and a second reflecting side when the reflector is in a deployed position, wherein the reflector is mounted on the face of the base so that the first side of the reflector is adjacent to the row of solar cells, and the first reflecting side of the reflector is oriented to reflect radiation incident on the first side onto the adjacent row of solar cells when the reflector is in the deployed position.

2. A solar panel according to claim 1 , wherein the row is only one solar cell in width.

3. A solar panel according to claim 1 , wherein the reflector comprises a flexible sheet having a reflective surface, the sheet being joined to the base; and an erector for erecting the sheet, the erector being biased towards the erect position whereby, absent external forces, the erector will raise the sheet, thereby deploying the reflector to its operational position.

4. A solar panel according to claim 3 , wherein the erector comprises a folded metal plate.

5. A solar panel according to claim 1 , wherein the reflector comprises a metal sheet having a reflective surface, the sheet being joined to the base; the sheet being creased longitudinally and being preformed to be biased to form the collapsible reflector, so that whereby, absent external forces, the sheet will raise itself to form the reflector in its deployed position.

6. A solar panel according to claim 5 , wherein the metal sheet is preformed so that each of the sides of the reflector has a roughly concave shape when the reflector is in its deployed position.

7. A solar panel according to claim 5 , wherein the metal sheet is titanium.

8. A solar panel according to claim 5 , wherein the metal sheet is titanium and has a thickness of approximately 0.0015 inches.

9. A solar panel according to claim 1 , wherein the solar cells in the row are electrically connected to the other solar cells in the row by electrical interconnect wiring, the electrical interconnect wiring being substantially under an adjacent reflector.

10. A solar panel according to claim 1 , wherein the row is one solar cell in width, and the solar cells have dual ohmics, the dual ohmics being substantially under an adjacent reflector.

11. A solar panel according to claim 1 , wherein the row is one solar cell in width, the solar cells have dual ohmics, and the solar cells in the row are electrically connected to the other solar cells in the row by electrical interconnect wiring, the interconnect wiring being substantially under an adjacent reflector.

12. A solar panel according to claim 1 , wherein at least two of the solar cells in the row are electrically connected to each other in parallel by electrical interconnect wiring, the electrical interconnect wiring being substantially under an adjacent reflector.

13. A solar panel comprising:

a base having a face;

a plurality of spaced-apart rows of solar cells; and

a plurality of elongated collapsible, self-deploying reflectors, each reflector having a first and a second reflecting side when the reflector is in a deployed position, wherein the reflectors and the rows are mounted on the face of the base in an alternating fashion so that the first side of each of the reflectors is adjacent to a row of solar cells, and the first reflecting side is oriented to reflect radiation incident on the first side onto the adjacent row of solar cells when the reflector is in the deployed position.

14. A solar panel as in claim 13 , wherein at least one of the reflectors is disposed between two adjacent rows so that when the at least one reflector is in the deployed position the first reflecting side is oriented to reflect radiation incident on the first side onto the first adjacent row of solar cells and the second reflecting side reflects radiation incident on the second side onto the second adjacent row of solar cells.

15. A solar panel according to claim 13 , wherein each row is only one solar cell in width.

16. A solar panel according to claim 13 , wherein each reflector comprises a flexible sheet having a reflective surface, the sheet being joined to the base; and an erector for erecting the sheet, the erector being biased towards the erect position whereby, absent external forces, the erector will raise the sheet, thereby deploying the reflector to its operational position.

17. A solar panel according to claim 16 , wherein the erector comprises a folded metal plate.

18. A solar panel according to claim 13 , wherein each reflector comprises a metal sheet having a reflective surface, the sheet being joined to the base; the sheet being creased longitudinally and being preformed to be biased to form the reflector, so that whereby, absent external forces, the sheet will raise itself to form the reflector in its deployed position.

19. A solar panel according to claim 18 , wherein the metal sheet is preformed so that each of the sides of the reflector has a roughly concave shape when the reflector is in its deployed position.

20. A solar panel according to claim 18 , wherein the metal sheet is titanium.

21. A solar panel according to claim 18 , wherein the metal sheet is titanium and has a thickness of approximately 0.0015 inches.

22. A solar panel according to claim 13 , wherein the solar cells in a row are electrically connected to the other solar cells in the row by electrical interconnect wiring, the electrical interconnect wiring being substantially under an adjacent reflector.

23. A solar panel according to claim 13 , wherein the rows are one solar cell in width, and the solar cells have dual ohmics, the dual ohmics being substantially under an adjacent reflector.

24. A solar panel according to claim 13 , wherein the rows are one solar cell in width, the solar cells have dual ohmics, and the solar cells in a row are electrically connected to the other solar cells in the row by electrical interconnect wiring, the interconnect wiring being substantially under an adjacent reflector.

25. A solar panel according to claim 13 , wherein at least two of the solar cells in one of the rows are electrically connected to each other in parallel by electrical interconnect wiring, the electrical interconnect wiring being substantially under an adjacent reflector.

26. A solar panel comprising:

a base;

a plurality of spaced-apart parallel rows of solar cells mounted on the base; and

a collapsible and self-deploying reflector mounted on the base between each of the rows of solar cells, the reflector comprising two reflective sides that are oriented to reflect incident energy onto the adjacent rows of solar cells.

27. A solar cell array, comprising:

a first column of solar cells;

a second column of solar cells;

a compressible and self-deploying concentrator positioned between the first column of solar cells and the second column of solar cells, wherein the concentrator is compressible to a first height and extendible to a second height.

28. A solar cell array according to claim 27 , further comprising a means for urging the concentrator from the first height to the second height.

29. A solar cell array according to claim 27 , further comprising a deployment means urging the reflector to the second position.

30. A solar cell array, comprising:

a plurality of spaced-apart rows of solar cells;

a reflector positioned between two of the rows of solar cells, the reflector compressible to a first position and configured to self-deploy from the first position to a second position.

Assignments (13)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 8, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
To: NORTHROP GRUMMAN SYSTEMS CORPORATION
Reel/Frame 055256/0892 →
CHANGE OF NAME Recorded Feb 4, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
Reel/Frame 055223/0425 →
CHANGE OF NAME Recorded Nov 1, 2018
From: ORBITAL ATK, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
Reel/Frame 047400/0381 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jun 6, 2018
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
To: ORBITAL ATK, INC.
Reel/Frame 046477/0874 →
RELEASE OF SECURITY INTEREST Recorded Oct 8, 2015
From: BANK OF AMERICA, N.A.
To: ALLIANT TECHSYSTEMS INC.; FEDERAL CARTRIDGE CO.; EAGLE INDUSTRIES UNLIMITED, INC.; AMMUNITION ACCESSORIES, INC.; ORBITAL ATK, INC. (F/K/A ALLIANT TECHSYSTEMS INC.)
Reel/Frame 036816/0624 →
RELEASE OF SECURITY INTEREST Recorded Oct 7, 2015
From: BANK OF AMERICA, N.A.
To: ALLIANT TECHSYSTEMS INC.
Reel/Frame 036807/0671 →
SECURITY AGREEMENT Recorded Sep 30, 2015
From: ORBITAL ATK, INC.; ORBITAL SCIENCES CORPORATION
To: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
Reel/Frame 036732/0170 →
CHANGE OF NAME Recorded May 22, 2015
From: ALLIANT TECHSYSTEMS INC.
To: ORBITAL ATK, INC.
Reel/Frame 035753/0373 →
SECURITY AGREEMENT Recorded Nov 26, 2013
From: ALLIANT TECHSYSTEMS INC.; CALIBER COMPANY; EAGLE INDUSTRIES UNLIMITED, INC.; FEDERAL CARTRIDGE COMPANY; SAVAGE ARMS, INC.; SAVAGE RANGE SYSTEMS, INC.; SAVAGE SPORTS CORPORATION
To: BANK OF AMERICA, N.A.
Reel/Frame 031731/0281 →
SECURITY AGREEMENT Recorded Nov 4, 2010
From: ALLIANT TECHSYSTEMS INC.; AMMUNITION ACCESSORIES INC.; ATK COMMERCIAL AMMUNITION COMPANY INC.; ATK COMMERCIAL AMMUNITION HOLDINGS COMPANY; ATK LAUNCH SYSTEMS INC.; ATK SPACE SYSTEMS INC.; FEDERAL CARTRIDGE COMPANY; EAGLE INDUSTRIES UNLIMITED, INC.; EAGLE MAYAGUEZ, LLC; EAGLE NEW BEDFORD, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 025321/0291 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 31, 2008
From: ATK SPACE SYSTEMS INC.
To: ALLIANT TECHSYSTEMS INC.
Reel/Frame 020723/0559 →
MERGER Recorded Mar 26, 2008
From: AEC-ABLE ENGINEERING COMPANY, INC.
To: ATK SPACE SYSTEMS INC.
Reel/Frame 020704/0187 →
SECURITY AGREEMENT Recorded Aug 24, 2007
From: AMMUNITION ACCESSORIES INC.; ATK COMMERCIAL AMMUNITION COMPANY INC.; ATK COMMERCIAL AMMUNITION HOLDINGS COMPANY INC.; ATK LAUNCH SYSTEMS INC.; ATK SPACE SYSTEMS INC.; FEDERAL CARTRIDGE COMPANY; MICRO CRAFT INC.; ALLIANT TECHSYSTEMS INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 019733/0757 →