Patents by Inventor Philip S. Dunlap

Philip S. Dunlap 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: 10036135
    Abstract: A membrane system isolates environment volume, contains hazards, enables detoxification, hazard removal, infrastructure restoration, and substance recovery. The flexible membrane system adjusts to advantageously shape its isolated volume and integrate existing infrastructure. Pollution and hazardous energy, including crude oil, toxic-gas, radioactive fallout, fire, and other hazards are isolated, while concurrently enabling access within the isolated volume. Pod encapsulated and readily deployed, the membrane system operates semi-autonomously, uses selective-filtering, specific gravity and substance differences to channel matter, mitigate hazards, protect the biosphere, preserve infrastructure and capture substances.
    Type: Grant
    Filed: October 23, 2015
    Date of Patent: July 31, 2018
    Inventors: Philip S. Dunlap, Michael J. Muse-Fisher, Nicholas A. Trutanich, Nathan M. Dunlap
  • Publication number: 20170114513
    Abstract: A membrane system isolates environment volume, contains hazards, enables detoxification, hazard removal, infrastructure restoration, and substance recovery. The flexible membrane system adjusts to advantageously shape its isolated volume and integrate existing infrastructure. Pollution and hazardous energy, including crude oil, toxic-gas, radioactive fallout, fire, and other hazards are isolated, while concurrently enabling access within the isolated volume. Pod encapsulated and readily deployed, the membrane system operates semi-autonomously, uses selective-filtering, specific gravity and substance differences to channel matter, mitigate hazards, protect the biosphere, preserve infrastructure and capture substances.
    Type: Application
    Filed: October 23, 2015
    Publication date: April 27, 2017
    Inventors: Philip S. Dunlap, Michael J. Muse-Fisher, Nicholas A. Trutanich, Nathan M. Dunlap
  • Patent number: 8802966
    Abstract: A method for transmitting power over long distances to a remote device is described. The method includes positioning a lens between a photon source and a photon receiver, the lens, photon source and photon receiver being physically separate systems, focusing a plurality of photons originating from the photon source using the lens, collecting the photons at a receiver, and utilizing the collected photons to generate electrical power.
    Type: Grant
    Filed: December 6, 2011
    Date of Patent: August 12, 2014
    Assignee: The Boeing Company
    Inventors: Philip S. Dunlap, Robert J. Budica
  • Publication number: 20130140916
    Abstract: A method for transmitting power over long distances to a remote device is described. The method includes positioning a lens between a photon source and a photon receiver, the lens, photon source and photon receiver being physically separate systems, focusing a plurality of photons originating from the photon source using the lens, collecting the photons at a receiver, and utilizing the collected photons to generate electrical power.
    Type: Application
    Filed: December 6, 2011
    Publication date: June 6, 2013
    Inventors: Philip S. Dunlap, Robert J. Budica
  • Patent number: 5853143
    Abstract: The flight vehicle includes an elongated central body having a central axis defined therein and a circumference. A plurality of elongated portions are positioned about the central body. A plurality of airbreathing engines are axisymetrically positioned about the central axis of the central body and between the respective elongated portions. Each flowpath includes a forebody, an inlet, an isolator duct, a combustor, a nozzle, and a mechanism for injecting fuel into the combustor. The forebody externally compresses the air flow. The inlet is downstream of the forebody to capture air flow. The isolator duct is downstream of the inlet to further reduce velocity of the air flow. The combustor is downstream of the isolator duct and finally, the nozzle is downstream of the combustor. The fuel/air mixture is burned in the combustor and expanded in the nozzle for providing thrust. A control mechanism is positioned about the central body for providing control of the flight vehicle.
    Type: Grant
    Filed: December 23, 1996
    Date of Patent: December 29, 1998
    Assignee: Boeing North American, Inc.
    Inventors: Marty K. Bradley, Kevin G. Bowcutt, Harry Shortland, Philip S. Dunlap