IP Library Granted Patent US 7,439,486
Granted Patent B2
US 7,439,486 · App. 11/825,282 · Granted Oct 21, 2008

Inflatable spherical integrating source for spaceflight applications

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Quick Facts
Patent No.
US 7,439,486
App. No.
11/825,282
Granted
Oct 21, 2008
Kind
B2
Abstract

A method for calibrating a sensor in a vehicle, such as a space capsule or other space borne apparatus, uses an expandable integrating sphere. A sensor in the vehicle measures the energy from an electromagnetic energy source within the integrating sphere through a calibration window. The expandable fluid impermeable integrating sphere expands when filled with a fluid, such that when filled with the fluid, its interior is viewable through the calibration window. The system includes a source of fluid to fill the integrating sphere and a fluid regulator coupled to the vehicle to determine when to supply the fluid to the integrating sphere to maintain an appropriate gas pressure level with the integrating sphere.

Claims (8)

1. A method for deploying an optical integrating sphere, comprising:

securing an expandable and unexpanded optical integrating sphere to a vehicle over a calibration window; and

expanding the optical integrating sphere.

2. A method for deploying an optical integrating sphere according to claim 1 , wherein the optical integrating sphere is expanded by injection of a fluid.

3. A method for deploying an optical integrating sphere according to claim 2 , further comprising regulating the fluid to be within a specified fluid pressure range.

4. A method for deploying an optical integrating sphere as in claim 3 , further comprising turning on a source of electromagnetic energy within the interior of the optical integrating sphere.

5. A method for deploying an optical integrating sphere as in claim 4 , wherein the said source of electromagnetic energy is a first source of electromagnetic energy, further comprising turning on a second source of electromagnetic energy within the interior of the optical integrating sphere upon detecting a failure in the first source of electromagnetic energy.

6. A method for deploying an optical integrating sphere as in claim 5 , wherein a fluid flow rate into the optical integrating sphere upon inflation is set at a rate to minimize a risk of damaging the first and second sources of electromagnetic energy.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 12, 2012
From: RAYTHEON COMPANY
To: OL SECURITY LIMITED LIABILITY COMPANY
Reel/Frame 029117/0335 →