Solar rejection system with movable sunshade

Patent metadata

Field	Value
Publication number	US-9815576-B2
Application number	US-201514799636-A
Country	US
Kind code	B2
Filing date	Jul 15, 2015
Priority date	Jul 16, 2014
Publication date	Nov 14, 2017
Grant date	Nov 14, 2017

Abstract

A solar rejection system includes an enclosure for housing a sensor, and a movable sunshade. The housing has an opening or aperture for admitting light to the sensor, and the sunshade is moved as needed to prevent harmful solar illumination of the sensor. The sunshade may be a flat panel. The sunshade panel is mounted to a hinge that is located on one side of a large diameter bearing that allows the shade to be rotated around the aperture of the sensor to always prevent the sun from illuminating the aperture. The hinge allows the shade to be tilted to either allow the sensor to see further off axis without obscuration or to block the sun when it moves in front of the sensor. Full closure of the sunshade on its hinge allows it to also function as an aperture door, blocking the opening or aperture.

First claim

What is claimed is:

1. A solar rejection system comprising:
an enclosure with an aperture; and
a movable sunshade movable to selectively block solar radiation from entering the aperture;
wherein the sunshade is rotatable relative to the enclosure about at least two axes;
wherein the at least two axes include an elevation axis for changing an elevation angle of the sunshade relative to the enclosure;
wherein the sunshade has a greatest extent that is larger than a distance between the elevation axis and the enclosure;
wherein the at least two axes include an azimuth axis aligned with a center of regard of a sensor that is in the enclosure;
wherein the sunshade is coupled to a bearing, to enable rotation of the sunshade along with the bearing; and
wherein the sunshade is hingedly coupled to the bearing.

2. The solar rejection system of claim 1 , wherein the azimuth axis is aligned with a center of the aperture.

3. The solar rejection system of claim 1 , wherein the sunshade is a flat panel.

4. The solar rejection system of claim 1 , wherein the sunshade has a length, an extent away from where the sunshade is hingedly coupled to the bearing, that is greater than a greatest extent of the aperture.

5. The solar rejection system of claim 1 , wherein the sunshade has a length, an extent away from where the sunshade is hingedly coupled to the bearing, that is greater than a width of the sunshade that is perpendicular to the length.

6. The solar rejection system of claim 1 , wherein the sunshade has a larger area than an area of the aperture.

7. The solar rejection system of claim 1 , wherein the sunshade is movable to fully close the aperture.

8. The solar rejection system of claim 1 , wherein the sunshade is tiltable to fully close the aperture.

9. The solar rejection system of claim 1 , wherein the solar rejection system is part of a spacecraft that also includes a sensor that is in the enclosure.

10. A solar rejection system comprising:
an enclosure with an aperture; and
a movable sunshade movable to selectively block solar radiation from entering the aperture;
wherein the sunshade is rotatable relative to the enclosure about at least two axes;
wherein the sunshade is movable to fully close the aperture; and
wherein the at least two axes include an azimuth axis aligned with a center of regard of a sensor that is in the enclosure, and an elevation axis.

11. The solar rejection system of claim 10 , wherein the sunshade is a flat panel.

12. The solar rejection system of claim 10 , wherein the sunshade is coupled to a bearing, to enable rotation of the sunshade along with the bearing.

13. The solar rejection system of claim 12 , wherein the sunshade is hingedly coupled to the bearing.

14. The solar rejection system of claim 13 , wherein the sunshade has a length, an extent away from where the sunshade is hingedly coupled to the bearing, that is greater than a greatest extent of the aperture.

15. The solar rejection system of claim 10 , wherein the solar rejection system is part of a spacecraft that also includes a sensor that is in the enclosure.

16. A method of protecting a sensor of a spacecraft from damage, the method comprising:
moving a sunshade from a stowed position in which the sunshade closes off an aperture in an enclosure of the spacecraft through which the sensor receives light;
pointing the sensor at a target; and
while the sensor is pointed at the target, positioning the sunshade relative to the enclosure, by rotating the sunshade as a single unit about an azimuth axis and an elevation axis, to prevent sunlight from reaching the sensor through the aperture of the enclosure.

Assignees

• Raytheon Co

Inventors

• Bullard Andrew L

Classifications

• B64G1/503

  Radiator panels · CPC title

• B64G1/506

  Heat pipes · CPC title

• B64G1/66

  Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title

• B64G1/546 Primary

  shielding electronic equipment · CPC title

• G03B11/045

  Lens hoods or shields · CPC title