Patents Represented by Attorney, Agent or Law Firm William J. Benman
-
Patent number: 4464019Abstract: This invention provides a unitary oil coupled optical arrangement for color selective prepolarization of the light incident upon two light valves. The optical arrangement is immersed within a single tank. It includes dichroic filters which act on polarized light from a light source which has been polarized into two beams by passing through and being reflected from a prepolarizing optical thin film stack. The first dichroic filter provides light of a first color and a first polarization while the second dichroic filter provides light of a second color and a second polarization. The light from each of the filters is then combined into a single beam by a thin film polarization-selective beam combiner prior to being applied to the main polarizing prism. The main prism then passes light of a first polarization and a first color to a first light valve and light of the second polarization and a second color to the second light valve in a conventional manner.Type: GrantFiled: December 28, 1981Date of Patent: August 7, 1984Assignee: Hughes Aircraft CompanyInventor: Ralph J. Gagnon
-
Patent number: 4461542Abstract: A first color selective beam splitter is provided for splitting light from a source into first and second beams, the first beam being blue and the second beam having red and green color components.A second beam splitter is provided for directing light of the first beam to a blue liquid crystal light valve. The light valve modulates the polarization of the light in the first beam and returns it to the second beam splitter which converts the modulations of polarization to modulations of intensity in the conventional manner and reflects it to a first projection lens.A third beam splitter is provided for splitting the second beam into third and fourth beams having first and second polarization states, respectively. The third beam is reflected to a red filter. The fourth beam is transmitted through a green filter.The output of each filter is a substantially monochromatic beam of a single polarization state. The filter outputs are recombined into a single beam which illuminates a fourth beam splitter.Type: GrantFiled: December 28, 1981Date of Patent: July 24, 1984Assignee: Hughes Aircraft CompanyInventor: Ralph J. Gagnon
-
Patent number: 4425028Abstract: A full color high contrast image projection system with oil coupled dichroics and a single projection lens is disclosed. The invention includes a unitary optical tank in which a prepolarizer and dichroic separators are mounted in fixed alignment relative to a main polarizing prism. The prepolarizer acts on the incident light from a source to polarize the green light and reflect the S component out of the system. The red and blue components are transmitted unchanged. The main polarizer is mounted at a 90.degree. twist relative to the prepolarizer so that it reflects the green light to a first light valve via a first dichroic separator. The polarized red and blue components are transmitted to second and third light valves via a second dichroic separator. The light valves modulate the polarization state of incident light before returning it to the second beamsplitter. The second beamsplitter then recombines the individual beams into a single output beam.Type: GrantFiled: December 28, 1981Date of Patent: January 10, 1984Assignee: Hughes Aircraft CompanyInventors: Ralph J. Gagnon, Robert T. Carson
-
Patent number: 4410865Abstract: A tri-mode spherical cavity microwave filter comprising two tandemly disposed generally spherical bodies each of which defines a spherical cavity which supports three identical, mutually orthogonal modes of electromagnetic energy, a cavity coupling aperture connecting the cavities, a plurality of cavity tuning holes, and a plurality of coupling tuning holes. One of the spherical cavities has an input aperture, and another has an output aperture. The cavity tuning holes and coupling tuning holes are adapted to receive cavity tuners and coupling tuners, respectively.Type: GrantFiled: February 24, 1982Date of Patent: October 18, 1983Assignee: Hughes Aircraft CompanyInventors: Frederick A. Young, Edward L. Griffin
-
Patent number: 4385833Abstract: An optic receiver capable of detecting the angle of incidence of optical energy in a plurality of fields of view relative to an airborne frame of reference. Incoming rays are reflected by surfaces arranged at predetermined angles relative to an input aperture so as to reflect rays in predetermined fields of view into parallelism with the receiver axis and ultimately to a line image at an output aperture. Power distribution along the line image varies with the azimuth of the target reflection. Computation of target azimuth from the power distribution along the line image is facilitated by photodetectors mounted on the element and associated electronic circuitry.Type: GrantFiled: December 5, 1980Date of Patent: May 31, 1983Assignee: Santa Barbara Research CenterInventor: Leland V. Gardner
-
Patent number: 4384367Abstract: An improved low-cost microwave receiver is disclosed. The receiver is intended for use in the Multipoint Distribution Services (MDS) for the reception of television signals transmitted in the 2 to 2.5 GHz region. The receiver of the present invention is of the single-conversion superheterodyne type utilizing printed circuit and microstrip transmission line construction. Printed circuit board and microstrip transmission line construction permits low-cost fabrication without machined resonant cavities or waveguide components.Type: GrantFiled: June 10, 1981Date of Patent: May 17, 1983Assignee: Theta-Com of CaliforniaInventors: Charles T. King, Bernard E. Sigmon
-
Patent number: 4383318Abstract: An improved laser pumping system is provided which utilizes optic fibers configured in a fan-in arrangement and an array of light emitting diodes or diode lasers to which the optic fibers are connected for concentrating light energy on a lasing medium. The improvement is an increase of the amount of light energy that can be applied to the laser within a fixed volume.Type: GrantFiled: December 15, 1980Date of Patent: May 10, 1983Assignee: Hughes Aircraft CompanyInventors: James D. Barry, Arthur J. Einhorn
-
Patent number: 4355312Abstract: A processor for operating on video and azimuth signals from a radar system having an antenna which scans in azimuth. The processor enhances the signal-to-noise ratio of the video signals while imposing thereon a substantially constant azimuth delay error.The processor includes a first circuit for forming and storing a count indicative of the video signal history in each range zone. The processor also includes a second circuit for generating and removing a flag signal indicative of azimuth leading and trailing edges respectively of a target pulse in the video signal. A gating circuit is included to pass video signals, for a given range zone, to an output terminal during the presence of a flag signal associated with the zone.Type: GrantFiled: October 2, 1980Date of Patent: October 19, 1982Assignee: Hughes Aircraft CompanyInventors: Gerald L. Bosi, Randolph L. Hack, Thomas C. Cantwell, Richard D. Wilmot
-
Patent number: 4352982Abstract: An improved photodector which in utilizing a low noise load network instead of a resistor has the advantages in signal-to-noise ratio of a large load resistance without the deleterious effect on response time. The circuit includes a conventional photodiode with an operational amplifier at its output. The load network is disposed in the feedback path of the operational amplifier. It consists of a second operational amplifier, a fixed resistor and a variable resistor.Type: GrantFiled: August 21, 1980Date of Patent: October 5, 1982Assignee: Hughes Aircraft CompanyInventors: Robert L. Forward, Gary D. Thurmond
-
Patent number: 4326800Abstract: An auto-alignment system for high energy lasers wherein a low energy reference beam is provided at the vertex of a primary mirror that is grated to diffract a low energy holographic replica of the high energy beam. A photodetector based servo-control system compares the line-of-sight of the reference beam to that of the low energy replica and generates control signals which actuate a beam steering mirror to reposition the main beam. The servo-control system also includes a wavefront sensor. This sensor analyzes the wavefront profile of the low energy replica and generates control signals which actuate a deformable mirror to correct spurious wavefront aberrations.Type: GrantFiled: May 5, 1980Date of Patent: April 27, 1982Assignee: Hughes Aircraft CompanyInventor: John M. Fitts
-
Patent number: 4325633Abstract: An optic receiver capable of detecting the angle of incidence of optical energy relative to an airborne frame of reference. Incoming reflected rays are reflected by a one piece detector element into a line image. Power distribution along the line image varies with the azimuth of the target. Computation of target azimuth from the power distribution along the line image is facilitated by photodetectors mounted on this element and associated electronic circuitry.Type: GrantFiled: June 2, 1980Date of Patent: April 20, 1982Assignee: Hughes Aircraft CompanyInventor: Leland V. Gardner
-
Patent number: 4302774Abstract: A system is disclosed for frequency compensation and amplitude compression of signals from a scene having targets which radiate infrared energy. The system uses at least two combinations, where each combination consists of an operational amplifier and a variable resistance element. These combinations are electrically coupled to each other. A circuit connected to one of the amplifiers provides high frequency compensation for radiated energy by small targets in the infrared scene. The system also utilizes a reference source which is coupled to the input of another of the amplifiers.Type: GrantFiled: May 3, 1979Date of Patent: November 24, 1981Assignee: Hughes Aircraft CompanyInventor: Ake W. Alm
-
Patent number: 4298872Abstract: A sidelobe blanking system is provided which uses as much of the existing radar tracking system as possible while requiring a minimal number of additional components. The sidelobe blanking system includes a guard antenna and two phase shifters the first of which is operably coupled to the main radar antenna's sum pattern. The phase shifters create signals of opposite polarities which represent the complex conjugate of the sum pattern from the main radar antenna. The system includes two summing circuits which add the signal received by the guard antenna to the complex conjugate signals of opposite polarity. The system also includes a phase detector which compares the outputs of the first and second summing circuits and generates a signal representative of the cosine of the relative phase angle.Type: GrantFiled: May 27, 1980Date of Patent: November 3, 1981Assignee: Hughes Aircraft CompanyInventor: William E. Rodgers
-
Patent number: 4242656Abstract: A two-terminal active network which simulates a low noise-temperature resistor is disclosed. In a preferred embodiment, a pair of operational amplifiers, each connected in the manner of a "current pump," comprises the active elements of the network. A resistive voltage divider network provides both positive and negative feedback to the operational amplifiers. Simulated resistors can be obtained with a wide range of equivalent resistance values and effective noise temperatures.Type: GrantFiled: June 8, 1979Date of Patent: December 30, 1980Assignee: Hughes Aircraft CompanyInventors: Robert L. Forward, Dale M. Sipma
-
Patent number: 4232280Abstract: A class of two-terminal active networks which simulate low-noise temperature resistors is disclosed. A single field effect transistor or other suitable amplifier comprises the active element of the network. A dual transformer feedback arrangement or a single transformer feedback arrangement comprises the remainder of the circuit. Either positive or negative simulated resistors can be obtained with a wide range of equivalent resistance values and effective noise temperatures.Type: GrantFiled: March 8, 1979Date of Patent: November 4, 1980Assignee: Hughes Aircraft CompanyInventor: Robert L. Forward