IP Library Granted Patent US 8,746,620
Granted Patent B1
US 8,746,620 · App. 13/747,626 · Granted Jun 10, 2014

Adaptive solar airframe

Inventors: John Peter Moussouris (Palo Alto, CA); Sergey V. Frolov (New Providence, NJ); Michael Cyrus (Summit, NJ)
Assignee: Sunlight Photonics Inc.
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,746,620
App. No.
13/747,626
Granted
Jun 10, 2014
Kind
B1
Abstract

Methods and apparatus for an adaptable solar airframe are provided herein. In some embodiments, an adaptable solar airframe includes a solar PV system having at least one solar tracking system and being able to follow the sun position in order to increase sunlight collection and power output; and an expandable body having an aerodynamic cross-section that minimizes parasitic air drag at any given thickness of the body, further being at least partially transparent to sunlight, further enclosing the solar PV system, and further being able to change its shape in response to changes in the positions of the solar PV system.

Claims (26)

1. An adaptable solar airframe comprising:

a solar PV system having at least one solar tracking system and being able to follow the sun's position in order to optimize sunlight collection and power output; and

an expandable body having an aerodynamic cross-section, further being at least partially transparent to sunlight, further enclosing the solar PV system, and further being able to change its shape to reduce parasitic air drag while compensating for the changes in the position of the solar PV system as the solar PV system follows the sun's position.

2. The adaptable solar airframe of claim 1 , wherein the solar PV system comprises broad area PV cells.

3. The adaptable solar airframe of claim 1 , wherein the solar PV system comprises a concentrated PV system.

4. The adaptable solar airframe of claim 3 , wherein the solar PV system further comprises an optical dispersive element.

5. The adaptable solar airframe of claim 1 , wherein the expandable body is symmetric in shape and produces zero aerodynamic lift.

6. The adaptable solar airframe of claim 1 , wherein the solar tracking system is able to provide a variable pitch angle to the solar PV system with respect to the sun.

7. The adaptable solar airframe of claim 1 , wherein the solar tracking system is able to provide a variable roll angle to the solar PV system with respect to the sun.

8. The adaptable solar airframe of claim 1 , wherein the expandable body comprises flexible plastic film.

9. The adaptable solar airframe of claim 1 , wherein the expandable body is operable to expand in the vertical direction.

10. The adaptable solar airframe of claim 1 , wherein the expandable body is operable to expand in the span-wise direction.

11. The adaptable solar airframe of claim 1 , further comprising an air pump configured to increase air pressure inside the airframe.

12. The adaptable solar airframe of claim 1 , further comprising at least one of expandable or rotating struts.

13. The adaptable solar airframe of claim 1 , wherein the expandable body is collapsible.

14. An aircraft comprising the adaptable solar airframe of claim 1 .

15. The aircraft of claim 14 , wherein the adaptable solar airframe is retractable.

16. The aircraft of claim 14 , wherein the solar PV system follows the sun by rotating a roll angle and a pitch angle of a solar collector.

17. The adaptable solar airframe of claim 1 , wherein:

the solar PV system tilts at a pitch angle to match the sun position; and

the expandable body changes its shape to contain the solar PV system at any pitch angle.

18. The adaptable solar airframe of claim 17 , wherein the change in shape of the expandable body reduces the parasitic air drag.

19. An airplane comprising the adaptive solar airframe of claim 1 .

20. The airplane of claim 19 , wherein the adaptive solar airframe has zero lift.

21. The airplane of claim 19 , wherein the adaptive solar airframe is a pod that can be towed behind the airplane.

22. The airplane of claim 21 , further comprising a storage compartment into which the adaptive solar airframe may be retracted and stored or from which it may be extracted and expanded.

Assignments (7)
CHANGE OF NAME Recorded May 23, 2019
From: SUNLIGHT PHOTONICS INC.
To: SUNLIGHT AEROSPACE INC.
Reel/Frame 049263/0897 →
CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT SERIAL NO. 13/856,592 PREVIOUSLY RECORDED AT REEL: 034961 FRAME: 0933. ASSIGNOR(S) HEREBY CONFIRMS THE RELEASE OF SECURITY INTEREST. Recorded Feb 26, 2015
From: VENEARTH FUND, LLC
To: SUNLIGHT PHOTONICS INC.
Reel/Frame 035110/0526 →
RELEASE OF SECURITY INTEREST Recorded Feb 13, 2015
From: VENEARTH FUND, LLC
To: SUNLIGHT PHOTONICS INC.
Reel/Frame 034961/0933 →
AMENDMENT NO. 5 TO PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Jan 17, 2014
From: SUNLIGHT PHOTONICS INC.
To: VENEARTH FUND, LLC
Reel/Frame 032087/0659 →
AMENDMENT NO. 4 TO PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Jul 29, 2013
From: SUNLIGHT PHOTONICS INC.
To: VENEARTH FUND, LLC
Reel/Frame 030918/0922 →
AMENDMENT NO. 3 TO PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Feb 22, 2013
From: SUNLIGHT PHOTONICS INC.
To: VENEARTH FUND, LLC
Reel/Frame 029855/0507 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 29, 2013
From: MOUSSOURIS, JOHN PETER; FROLOV, SERGEY V.; CYRUS, MICHAEL
To: SUNLIGHT PHOTONICS INC.
Reel/Frame 029712/0092 →