Patents by Inventor Richard A. Carreras

Richard A. Carreras has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10331811
    Abstract: The present invention is a method for real-time predictive laser beam propagation through various atmospheric conditions and over predetermined distances. The invention includes loading input parameters into an embedded control scheme of a laser system. A prediction of one or more laser beam parameters is generated and a computational error is quantified for the generated laser beam parameters. One or more parameters for the laser system are then chosen based on the prediction and based on the quantified computational error. The chosen parameters are within a predetermined tolerance. A laser system is then built or adjusted using the one or more chosen parameters.
    Type: Grant
    Filed: July 28, 2015
    Date of Patent: June 25, 2019
    Assignee: TAU TECHNOLOGIES, LLC
    Inventors: Sami A. Shakir, Richard A. Carreras
  • Publication number: 20160034618
    Abstract: The present invention is a method for real-time predictive laser beam propagation through various atmospheric conditions and over predetermined distances. The invention includes loading input parameters into an embedded control scheme of a laser system. A prediction of one or more laser beam parameters is generated and a computational error is quantified for the generated laser beam parameters. One or more parameters for the laser system are then chosen based on the prediction and based on the quantified computational error. The chosen parameters are within a predetermined tolerance. A laser system is then built or adjusted using the one or more chosen parameters.
    Type: Application
    Filed: July 28, 2015
    Publication date: February 4, 2016
    Inventors: Sami A. Shakir, Richard A. Carreras
  • Patent number: 6752502
    Abstract: An optical quality, freestanding, compliant membrane mirror is cast with a concave parabolic shape, and includes a substrate and a reflective stress coating. The stress coating is in compression and applies a tensile shear stress to the substrate that opposes and offsets the intrinsic stress in the substrate that would otherwise decrease the concavity. The stress coating generates a force to restore the membrane mirror to its cast concave parabolic shape when an external force deforms the mirror.
    Type: Grant
    Filed: March 17, 2003
    Date of Patent: June 22, 2004
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Richard A. Carreras, Dan K. Marker, James M. Wilkes, Dennis Duneman, James R. Rotge
  • Publication number: 20030223135
    Abstract: A method for fabricating an optical quality, free-standing, compliant parabolic membrane mirror is described using an inverted parabolic mandrel created by rotating a liquid confined to a cylindrical container, forming a membrane substrate by pouring into the mandrel a fast curing liquid polymer and applying a reflective optical stress coating once the substrate has hardened.
    Type: Application
    Filed: March 17, 2003
    Publication date: December 4, 2003
    Inventors: Richard A. Carreras, Dan K. Marker, James M. Wilkes, Dennis Duneman, James R. Rotge
  • Patent number: 6533426
    Abstract: A method for fabricating an optical quality, free-standing, compliant parabolic membrane mirror using an inverted parabolic mandrel created by rotating a liquid confined to a cylindrical polymer and applying a reflective optical stress coating once the substrate has hardened. The stress coating applies a tensile force to the substrate that offsets the stress in the substrate that would otherwise decrease the convexity, and also generates a force to restore the membrane mirror to its original convex parabolic shape when the mirror is deformed by an external force.
    Type: Grant
    Filed: May 2, 2001
    Date of Patent: March 18, 2003
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Richard A. Carreras, Dan K. Marker, James M. Wilkes, Dennis Duneman, James R. Rotge
  • Publication number: 20020163744
    Abstract: Attorney Docket No. PRS0586A method for fabricating an optical quality, free-standing, compliant parabolic membrane mirror is described using an inverted parabolic mandrel created by rotating a liquid confined to a cylindrical container, forming a membrane substrate by pouring into the mandrel a fast curing liquid polymer and applying a reflective optical stress coating once the substrate has hardened.
    Type: Application
    Filed: May 2, 2001
    Publication date: November 7, 2002
    Inventors: Richard A. Carreras, Dan K. Marker, James M. Wilkes, Dennis Duneman, James R. Rotge
  • Patent number: 6332687
    Abstract: A membrane mirror having an optical quality spherical shape maintained by differential pressure takes a near parabolic shape when a plunger-induced displacement of the central area of the mirror is introduced. The focal length can be adjusted by varying the differential pressure.
    Type: Grant
    Filed: November 2, 2000
    Date of Patent: December 25, 2001
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Richard A. Carreras, Dan K. Marker, James M. Wilkes, Dennis Duneman, James R. Rotge
  • Patent number: 6113242
    Abstract: A thin membrane is mounted on an optically flat circular outer ring and stretched over a smaller optically flat circular inner ring. Differential pressure is applied to the annulus formed between the inner and outer rings to prestrain the membrane and separately applied to the inner ring where the mirror figure will be produced. The inner ring has a doubly curved top surface and is optically fiat so that the membrane can freely move across the inner ring as incremental stress is applied via the annulus. A calculated combination of annulus stress and differential pressure on the inner ring produces an optical quality mirror figure in the inner ring area.
    Type: Grant
    Filed: January 15, 1999
    Date of Patent: September 5, 2000
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Dan K. Marker, Richard A. Carreras, James M. Wilkes, Dennis Duneman
  • Patent number: 6107617
    Abstract: Large space-based optical systems are expected to produce optical beams with large wavefront phase aberrations due to their size, weight limitations, optical misaligments and primary mirror imperfections. The present invention combines a phase diversity wavefront sensor with a real-time programmable two-dimensional array of liquid crystal variable retarders for wavefront correction.
    Type: Grant
    Filed: June 5, 1998
    Date of Patent: August 22, 2000
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Gordon D. Love, Richard A. Carreras, Sergio Restaino, Janet S. Fender, Dennis Duneman
  • Patent number: 4831246
    Abstract: A system and method for large angle off-axis steering of the composite beam from a phased array telescope system.
    Type: Grant
    Filed: April 14, 1988
    Date of Patent: May 16, 1989
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Patricia J. Wallentine, Mark G. Baciak, Richard A. Carreras, Elinor L. Coates, David G. Haralson
  • Patent number: 4740677
    Abstract: In an optically phased array of multiple laser telescopes, the phasing between the telescopes is accomplished by sampling adjacent outgoing wavefronts. The two samples of each wavefront are then combined to form an interference pattern on a camera. This image is then converted to digital signals, employing an error signal representative of the phase difference. It is necessary that the telescopes be pointing in the same direction. This is assured by having each telescope associated with an optical sensor which produces an X or Y tilt error. The X or Y tilt error is corrected by the optical component referred to as the optical path difference adjustor (OPDA). A signal processing circuit is disclosed which receives X and Y tilt error signals, as well as phase error signals, and produces therefrom drive signals which correct and drive the OPDA in an array of multiple laser telescopes.
    Type: Grant
    Filed: December 15, 1986
    Date of Patent: April 26, 1988
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Richard A. Carreras, Mark G. Baciak, Elinor L. Coates, Morton Jenks
  • Patent number: 4689758
    Abstract: The microcomputer controlled image processor receives an interference pattern of samples of pairs of transmitted laser beams from a charge couple device (CCD) camera. The present invention then calculates an optical path difference between each pair of beams using: an analog amplifier, an analog-to-digital (A/D) converter, a multiple accumulator controller, a programmable read-only-memory (PROM), a microcomputer, and a random access memory (RAM). The analog amplifier and A/D converter amplify and convert to digital the interference pattern received from the CCD camera. The multiple accumulator controller (MAC) receives the digital camera signal from the A/D converter, and adds correction factors for the non-linearities in the CCD camera. The PROM stores these correction factors, and supplies them to the multiple accumulator controller when needed. The random access memory receives and stores the corrected data from the multiple accumulator controller, and supplies the data to the microcomputer.
    Type: Grant
    Filed: January 8, 1985
    Date of Patent: August 25, 1987
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Richard A. Carreras
  • Patent number: 4667090
    Abstract: A plurality of telescopes provide output return signals which are applied both directly and in sampled form to a photo-detector cell. The detected signals from the photo-detector will represent the constant and transient errors of the telescope system. A low pass filter insures that the tracker provides only the constant or D.C. component of the error, while a high pass filter insures that the existing measuring devices for each telescope beam provide only the transient or A.C. component of the error. The A.C. and D.C. error signals are summed together with the appropriate applied gains on each channel such that the sum reconstructs the original telescope position error with good fidelity.
    Type: Grant
    Filed: June 10, 1985
    Date of Patent: May 19, 1987
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Richard A. Carreras, Salvatore J. Cusumano, Morton B. Jenks, Robert I. Suizu