Patents by Inventor Robin Reeder

Robin Reeder 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: 5600480
    Abstract: An improved electro-optic modulator having reduced amplitude of acoustic resonances is provided. Acoustic energy is efficiently removed from the electro-optic crystal and channeled into electrode and side dielectric bars where it is dissipated by materials acoustically matched to the electro-optic crystal, that is, materials that have acoustic impedances within .+-.15% of that of the electro-optic material.
    Type: Grant
    Filed: September 17, 1993
    Date of Patent: February 4, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Kuei-Ru Chien, Robin A. Reeder
  • Patent number: 5285509
    Abstract: A waveguide coupler for coupling electromagnetic power between a first rectangular waveguide and a second rectangular waveguide includes a one-dimensional intermediate waveguide formed of two plates spaced apart by a distance equal to a common height of the two waveguides. This enables a wave emanating from the first waveguide to spread apart transversely so as to equal the width of the second waveguide, the width of the second waveguide being greater than the width of the first waveguide. A cylindrical lens is located between the intermediate waveguide and the second waveguide to provide for a conversion between a cylindrical wavefront and a planar wavefront. The coupler is operative in reciprocal fashion such that a wave emanating from the first waveguide spreads out in width and is then converted to a planar waveguide prior to entering the second waveguide; and a wave emanating from the second waveguide is converted to a wave of contracting width for entry into the first waveguide.
    Type: Grant
    Filed: December 18, 1992
    Date of Patent: February 8, 1994
    Assignee: Hughes Aircraft Company
    Inventors: Robin A. Reeder, Gregory R. Sasaki
  • Patent number: 5198919
    Abstract: This invention discloses a narrow field of view scanner (10) incorporating two multi-faceted polygon scanning wheels (12, 16) having a slightly different number of facets (14, 18). Each scanning wheel (12, 16) turns at an angular rate such that a facet (14) on one wheel (12) rotates through a predetermined field of view at the same rate as a facet (18) on the other wheel (16). Further, each of the scanning wheels (12, 16) scan in opposite scanning directions. This does not necessarily mean, however, that the wheels are actually rotating in opposite directions. Because both of the scanning wheels (12, 16) are scanning in opposite directions, the scanning of one scanning wheel (16) substantially cancels the scanning of the other scanning wheel (12). Because of the difference in the number of facets (14, 18) between the two scanning wheels (12, 16), the scanning is not entirely cancel out.
    Type: Grant
    Filed: August 26, 1991
    Date of Patent: March 30, 1993
    Assignee: Hughes Aircraft Company
    Inventor: Robin A. Reeder
  • Patent number: 5018153
    Abstract: A method and apparatus which corrects the amplutide variation in the output in an electro-optic modulated laser system (10). Birefringence within the electro-optic crystal (25) causes elliptical polarization of the linearly polarized laser light (22) produced by the laser gain medium (16), in turn causing a loss in the laser output (27). The loss owing to the elliptical polarization is corrected by either applying a D.C. bias from voltage source (30) directly to the electro-optic crystal (25) or by inserting a quarter-wave plate (32) within the laser's resonant cavity.
    Type: Grant
    Filed: February 23, 1990
    Date of Patent: May 21, 1991
    Assignee: Hughes Aircraft Company
    Inventors: Kuei-Ru Chien, Robin A. Reeder, H. Dean Stovall
  • Patent number: 4815820
    Abstract: A method and improved apparatus for aligning a diffraction grating, as, for example, one used in tuning the output of a laser. The total angular misalignment .epsilon. between the incident and diffracted beams is a function of three angles: the tuning angle .theta.16, the angle of tilt .beta. between the plane of the grating 15 and the tuning rotational axis, and the angle .alpha. between the grating lines and the projection of the turning rotational axis in the plane of the grating 15. The present invention provides a method of aligning the diffraction grating so that the residual alignment error is very small over the desired range of tuning angle .theta. 16, by adjusting only .alpha. or only .beta. to zero at two reference tuning angles .theta..sub.0 and .theta..sub.1. Knowledge of the value of either .alpha. or .beta. is not necessary. For a CO.sub.2 laser tuned over the wavelength range 9.11 to 10.88 .mu.
    Type: Grant
    Filed: May 8, 1986
    Date of Patent: March 28, 1989
    Assignee: Hughes Aircraft Company
    Inventors: John A. McNeil, Robin A. Reeder
  • Patent number: 4740986
    Abstract: A reflectance-outcoupled laser resonator 10 with an improved electro-optical Q-switch 13, 18,19, 21 is disclosed which is alignment stable. The laser performance is insensitive to angular movements of the resonator elements. This resonator requires fewer optical components and lower total cost than other resonators which are designed to perform similar functions. The invention includes a laser medium 12, two prisms 13, 21, a polarizer 18, an electro-optic crystal 19, and an alignment wedge 20. A polarization preserving folding prism 13 allows great flexibility in resonator design by passing any arbitrary polarization state without change. A double end-reflector prism 21 serves as both cavity end reflectors of the resonator and also serves as a component of the Q-switch 13, 18, 19, 21.
    Type: Grant
    Filed: December 20, 1985
    Date of Patent: April 26, 1988
    Assignee: Hughes Aircraft Company
    Inventor: Robin A. Reeder