Gravity-enforced photon momentum radiometer and measuring optical power

Patent metadata

Field	Value
Publication number	US-12169141-B2
Application number	US-202217831736-A
Country	US
Kind code	B2
Filing date	Jun 3, 2022
Priority date	Jun 3, 2021
Publication date	Dec 17, 2024
Grant date	Dec 17, 2024

Abstract

A gravity-enforced photon momentum radiometer incudes: a magnetic array; a diamagnetic shuttle that levitates above the magnetic array; a mirror on the diamagnetic shuttle that receives laser light and moves the diamagnetic shuttle due to the optical force; a tiltable platform for the magnetic array; a photogate producing gate light that can be blocked by a photo interrupter and that produces a detector signal that provides a position of the diamagnetic shuttle relative to the tiltable platform for determining a position of the diamagnetic shuttle relative to the photogate.

First claim

What is claimed is:

1. A gravity-enforced photon momentum radiometer for measuring optical power of laser light, the gravity-enforced photon momentum radiometer comprising:
a magnetic array that produces a diamagnetic levitation force;
a diamagnetic shuttle disposed proximate to the magnetic array such that the diamagnetic shuttle is in communication with the magnetic array and subjected to the diamagnetic levitation force from the magnetic array whereby the diamagnetic shuttle levitates above the magnetic array in response to the diamagnetic levitation force;
a mirror disposed on the diamagnetic shuttle and that receives an incident optical force from the laser light and moves, in response to receipt of the incident optical force, the diamagnetic shuttle in a direction of propagation of the laser light;
a tiltable platform on which is disposed the magnetic array, such that the magnetic array is interposed between the tiltable platform and the diamagnetic shuttle, wherein the tiltable platform positions the magnetic array at a tilt angle with respect to a reference platform, wherein tilt angle β depends on an amount of the incident optical force received by the mirror, and tilt angle β changes based on the amount of the incident optical force received by the mirror;
a photogate comprising an optical source that transmits gate light and a detector that detects the gate light from the photogate and produces a detector signal based on the amount of the gate light detected, wherein the gate light is subject to being blocked by a photo interrupter, the amount of blocking by the photo interrupter being dependent upon the position of the diamagnetic shuttle relative to the photogate as modified by the amount of the incident optical force received by the mirror, such that the detector signal provides a position of the diamagnetic shuttle relative to the tiltable platform; and
the photo interrupter disposed on the diamagnetic shuttle, and that moves relative to the photogate based on movement of the diamagnetic shuttle, and blocks the gate light as a function of the movement of the diamagnetic shuttle caused by receipt of the laser light by the mirror.

2. The gravity-enforced photon momentum radiometer of claim 1 , further comprising a pivot member in mechanical communication with the tiltable platform and interposed between the tiltable platform and the reference platform, such that tiltable platform pivots about the pivot member at tilt angle β with respect to reference platform.

3. The gravity-enforced photon momentum radiometer of claim 2 , further comprising a height sensor in mechanical communication with the tiltable platform and disposed on an end of the tiltable platform opposing the pivot member, such that the height sensor provides a height signal based on the height h of the tiltable platform with respect to the reference platform.

4. The gravity-enforced photon momentum radiometer of claim 3 , further comprising a height adjustment member in mechanical communication with the tiltable platform and disposed on an end of the tiltable platform opposing the pivot member, such that the height adjustment member adjusts the height h of the tiltable platform with respect to the reference platform.

5. The gravity-enforced photon momentum radiometer of claim 4 , further comprising a phase sensitive detector in communication with the photogate and that receives the detector signal from the photogate, demodulates the detector signal at a modulation frequency f m , and produces a balanced position signal for the diamagnetic shuttle from the detector signal.

6. The gravity-enforced photon momentum radiometer of claim 5 , further comprising an electrical feedback controller in communication with the phase sensitive detector and the height sensor and that receives the balanced position signal from the phase sensitive detector, receives a height signal from the height sensor, produces a height control signal based on the balanced position signal and the height signal, and communicates the height control signal to the height adjustment member, such that the height adjustment member adjusts the height h of the tiltable platform with respect to the reference platform under control of the height control signal from the electrical feedback controller.

7. The gravity-enforced photon momentum radiometer of claim 1 , further comprising an air shield in which the magnetic array, the diamagnetic shuttle, the mirror, the tiltable platform, the photogate, and the photo interrupter are disposed.

8. The gravity-enforced photon momentum radiometer of claim 1 , wherein the diamagnetic shuttle, the mirror, and the photo interrupter are non-metallic to prevent eddy currents during motion in the magnetic field of the magnetic array.

9. The gravity-enforced photon momentum radiometer of claim 1 , wherein the magnetic array comprises a plurality of magnets that provide a nonuniform magnetic field to levitate the diamagnetic shuttle in a vertical direction relative to the reference platform and to constrain motion of the diamagnetic shuttle in a horizontal plane relative to the reference platform.

10. The gravity-enforced photon momentum radiometer of claim 1 , wherein the mirror reflects laser light that provides the incident optical force to the diamagnetic shuttle, such that the mirror is highly reflective at the wavelength of the laser light whereby the laser light reflects from the mirror in an absence significant absorption or transmission of the laser light by the mirror that otherwise would produce heat.

11. The gravity-enforced photon momentum radiometer of claim 1 , wherein the mirror reflects laser light that provides the incident optical force to the diamagnetic shuttle, and the optical power of the laser light is determined from the mass of the diamagnetic shuttle, the gravitational acceleration of the diamagnetic shuttle, and the tilt angle β of the magnetic array.

12. A process for measuring optical power of laser light with a gravity-enforced photon momentum radiometer, the process comprising:
producing a diamagnetic levitation force by a magnetic array of the gravity-enforced photon momentum radiometer, the gravity-enforced photon momentum radiometer comprising:
the magnetic array;
a diamagnetic shuttle disposed proximate to the magnetic array such that the diamagnetic shuttle is in communication with the magnetic array;
a mirror disposed on the diamagnetic shuttle;
a tiltable platform on which is disposed the magnetic array, such that the magnetic array is interposed between the tiltable platform and the diamagnetic shuttle, wherein the tiltable platform positions the magnetic array at a tilt angle β with respect to a reference platform, wherein tilt angle β depends on an amount of the incident optical force received by the mirror, and tilt angle β changes based on the amount of the incident optical force received by the mirror;
a photogate comprising an optical source light and a detector; and
the photo interrupter disposed on the diamagnetic shuttle;

subjecting the diamagnetic shuttle to the diamagnetic levitation force from the magnetic array;
levitating the diamagnetic shuttle above the magnetic array in response to the diamagnetic levitation force;
receiving the laser light by the mirror;
moving, the diamagnetic shuttle, in response to the mirror receiving the incident optical force of the laser light in a direction of propagation of the laser light;
positioning, by the tiltable platform, the magnetic array at a tilt angle β with respect to the reference platform, wherein tilt angle β depends on an amount of the incident optical force received by the mirror;
changing the tilt angle β

Assignees

• Government Of The Us Secretary Of Commerce

Inventors

• Williams Paul Andrew
• Rahn Daniel
• Vaskuri Anna Katariina

Classifications

• G01J1/0414

  using plane or convex mirrors, parallel phase plates, or plane beam-splitters · CPC title

• G01B21/08

  for measuring thickness · CPC title

• G01J1/0403

  Mechanical elements; Supports for optical elements; Scanning arrangements · CPC title

• G01J1/4257 Primary

  applied to monitoring the characteristics of a beam, e.g. laser beam, headlamp beam (monitoring arrangements for lasers in general H01S3/0014) · CPC title