Patents Assigned to Lookheed Martin Corporation
  • Publication number: 20120074263
    Abstract: A cross flow instability inhibiting assembly generates periodic aerodynamic disturbances on a swept wing. The cross flow instability inhibiting assembly is dynamic in that it can be selectively turned on and off as needed. The cross flow instability inhibiting assembly is a strip of material separating a set of electrodes from a set of electrodes. When energized, the fields created between the electrodes and electrodes create plasma disturbances around the electrodes. The electric fields and plasma create heating and body force disturbances on the air or surrounding fluid. These plasma generated disturbances disrupt development of unstable voriticity due to cross flow, inhibiting transition to turbulent flow of the wing to which it is attached. The electrodes may be connected to electrical power in series or they may be connected to an alternating configuration. The system allows for various uses based on the design of the wing and the conditions in which the host aircraft is flying.
    Type: Application
    Filed: September 29, 2010
    Publication date: March 29, 2012
    Applicant: Lookheed Martin Corporation
    Inventors: Craig M. Hansen, Paul D. McClure, Sergey Macheret
  • Publication number: 20100256843
    Abstract: A train control system comprising a vital brake interface unit that is disposed between the train control processors and the braking system. The brake interface unit ensures that any failure in the control processors or the interface itself is detectable and, when detected, causes the system to fail safely (i.e., the train's brakes are applied). By virtue of the use of redundant circuitry paths, the vital braking interface unit enables real-time verification of system circuitry without actually applying the train's brakes.
    Type: Application
    Filed: April 2, 2010
    Publication date: October 7, 2010
    Applicant: Lookheed Martin Corporation
    Inventors: Harvey Bergstein, Thomas R. Metzger, Michael R. Pawlak, Warren H. Klinck, JR.
  • Publication number: 20100243448
    Abstract: A whispering gallery mode resonator based optical sensor assembly comprises a flow channel permeable to optical energy and first and second optical waveguides adjacent to a section of the flow channel and adapted to be in first and second evanescent field couplings respectively with the section such that the section forms a whispering gallery mode resonator. The resonator is responsive to an optical signal conveyed in the first optical waveguide and communicates a second optical signal to the second optical waveguide indicative of a resonance wavelength of the whispering gallery mode resonator. A detector optically coupled to the second optical waveguide detects the output signal. A signal processor detects a shift in the output signal responsive to an analyte fluid flowing through the flow channel. The shift is indicative of the identity of at least one constituent of the analyte fluid.
    Type: Application
    Filed: March 17, 2010
    Publication date: September 30, 2010
    Applicant: Lookheed Martin Corporation
    Inventors: Scott Maurer, Stephanie Groves, Kee Koo