Laminar airfoil and the assembly and mounting of solar cell arrays on such airfoils

Patent metadata

Field	Value
Publication number	US-10991833-B2
Application number	US-201916430093-A
Country	US
Kind code	B2
Filing date	Jun 3, 2019
Priority date	Dec 5, 2017
Publication date	Apr 27, 2021
Grant date	Apr 27, 2021

Abstract

A vehicle such as an aircraft on which a solar cell assembly is mounted on a surface of the space vehicle. The solar cell assembly may be prepared on an assembly fixture. The solar cell assembly may then be removed from the assembly fixture and positioned on a top surface of the streamlined body of the vehicle. In examples, the solar cell assembly comprises a first film, an array of solar cells on top of the first film, and a second silicone film deposited over the solar cells.

First claim

The invention claimed is:

1. A vehicle comprising
(a) a streamlined body having a top surface,
(b) a double sided adhesive film positioned on and mounted to the top surface of the streamlined body, and
(c) a solar cell assembly bonded to the top surface by the double sided adhesive film, wherein the solar cell assembly comprises
(i) a first silicone film;
(ii) an array of interconnected solar cells having a front light receiving side and a back side, with the back side disposed directly over the first silicone film; and
(iii) a second silicone film comprising a first portion tapering in thickness and comprising a second portion of the second silicone film over the front side of the solar cells so as to encapsulate the solar cells and provide a smooth surface wherein the tapering of the second silicone film is no more than a gradation of two degrees.

2. The vehicle according to claim 1 , wherein the array of interconnected solar cells are III-V compound semiconductor multijunction solar cells.

3. The vehicle according to claim 1 , wherein the double sided adhesive film comprises a pressure sensitive adhesive.

4. The vehicle according to claim 3 , wherein the double sided adhesive film comprises one or more release liners.

5. The vehicle according to claim 1 , wherein the first silicone film is bonded to a polyimide film.

6. The vehicle according to claim 1 , where in the solar cell assembly further includes an ETFE film on top of the second silicone film.

7. The vehicle according to claim 1 , wherein the solar cell assembly has a substantially constant thickness in an area where the array of solar cells is arranged.

8. The vehicle according to claim 1 , wherein the vehicle is an aircraft or watercraft.

9. A vehicle according to claim 1 , wherein the streamlined body comprises an airfoil body, and at least a portion of the solar cell assembly is attached to a suction surface of the airfoil body.

10. The vehicle according to claim 9 , wherein the first portion is disposed adjacent to a leading edge of the airfoil body.

11. The vehicle according to claim 9 , wherein the first portion is adhered to the airfoil body prior to mounting the second portion on the airfoil.

12. The vehicle according to claim 1 , wherein the first portion tapers with increasing width in a direction away from an edge of the first portion to a thickness of 0.020 inches.

13. The vehicle according to claim 1 , wherein a thickness of the first portion of the second silicone film begins at an edge of the first portion at a thickness of between 0.003 and 0.005 inches and tapers in a direction away from the edge to a thickness between 0.020 and 0.040 inches.

14. The vehicle according to claim 1 , further comprising a film of ETFE material of between 0.001 and 0.020 inches in thickness mounted over the second silicone film.

15. The vehicle according to claim 14 , further comprising a pressure sensitive adhesive film of 0.001 inches in thickness, mounted between the second silicone film and the ETFE film.

16. The vehicle according to claim 1 , wherein the top surface of the streamlined body is formed by a carbon fiber composite.

17. A vehicle comprising:
(a) a streamlined body forming a portion of the vehicle having a top surface; and
(b) a solar cell assembly of interconnected III-V compound semiconductor multijunction solar cells bonded to the top surface, wherein the solar cell assembly comprises
(i) a first silicone film;
(ii) an array of interconnected solar cells having a front light receiving side and a back side, with the back side disposed directly over the first silicone film; and
(iii) a second silicone film comprising a first portion tapering with increasing width in a direction away from an edge of the first portion to a thickness of 0.020 inches 0.0020 inches and comprising a second portion of the second silicone film over the front side of the solar cells so as to encapsulate the solar cells and provide a smooth surface permitting laminar flow over the surface of the body.

18. The vehicle according to claim 17 , wherein a thickness of the first portion of the second silicone film begins at an edge of the first portion at a thickness of between 0.003 and 0.005 inches and tapers in a direction away from the edge to a thickness between 0.020 and 0.040 inches, wherein the tapering of the second silicone film is no more than a gradation of two degrees.

19. A vehicle comprising
(a) a streamlined body having a top surface,
(b) a double sided adhesive film positioned on and mounted to the top surface of the streamlined body, and
(c) a solar cell assembly bonded to the top surface by the double sided adhesive film, wherein the solar cell assembly comprises
(i) a first silicone film;
(ii) an array of interconnected solar cells having a front light receiving side and a back side, with the back side disposed directly over the first silicone film; and
(iii) a second silicone film comprising a first portion tapering in thickness and comprising a second portion of the second silicone film over the front side of the solar cells so as to encapsulate the solar cells and provide a smooth surface, wherein a thickness of the first portion of the second silicone film begins at an edge of the first portion at a thickness of between 0.003 and 0.005 inches and tapers in a direction away from the edge to a thickness between 0.020 and 0.040 inches.

Assignees

• Solaero Tech Corp

Inventors

• Kruse Matthew
• Hernandez Fadel

Classifications

• B64D27/353

  using solar cells · CPC title

• H10F77/50

  Encapsulations or containers (for photovoltaic modules H10F19/80) · CPC title

• B64D41/00 Primary

  Power installations for auxiliary purposes · CPC title

• H10F71/139

  using temporary substrates · CPC title

• H10F71/137

  Batch treatment of the devices · CPC title