Patents by Inventor Devin W. Hersey

Devin W. Hersey 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: 7417598
    Abstract: A compact, low profile electronically scanned antenna module is provided. The antenna module includes a multi-layer antenna integrated printed wiring board (AiPWB) that includes a radiator layer on a front surface. The radiator layer includes a plurality of RF radiating elements. The antenna module additionally includes a plurality of radiator electronics modules orthogonally connected to a back surface of the AiPWB. The electronics modules are interconnected with radiating elements through the AiPWB and include a plurality of beam steering electronic elements mounted to a multi layer conformable substrate. The orthogonal connections allow the antenna module to have outer dimensions that are substantially equal to the dimensions of a perimeter of the AiPWB.
    Type: Grant
    Filed: November 8, 2006
    Date of Patent: August 26, 2008
    Assignee: The Boeing Company
    Inventors: Julio A. Navarro, Devin W. Hersey, Michael H. Florian, Gordon D Osterhues, Percy Yen
  • Publication number: 20080106467
    Abstract: A compact, low profile electronically scanned antenna module is provided. The antenna module includes a multi-layer antenna integrated printed wiring board (AiPWB) that includes a radiator layer on a front surface. The radiator layer includes a plurality of RF radiating elements. The antenna module additionally includes a plurality of radiator electronics modules orthogonally connected to a back surface of the AiPWB. The electronics modules are interconnected with radiating elements through the AiPWB and include a plurality of beam steering electronic elements mounted to a multi layer conformable substrate. The orthogonal connections allow the antenna module to have outer dimensions that are substantially equal to the dimensions of a perimeter of the AiPWB.
    Type: Application
    Filed: November 8, 2006
    Publication date: May 8, 2008
    Inventors: Julio A. Navarro, Devin W. Hersey, Michael H. Florian, Gordon D. Osterhues, Percy Yen
  • Patent number: 4990412
    Abstract: A cryogenic compressor for compressing hydrogen and oxygen and method for compressing these two gases. In a first preferred embodiment, an electrochemical compressor (12) is operative to compress hydrogen and oxygen gas. These two gases separately enter chamber (120 and 132) in an enclosure (118). Between the two chambers is disposed a catalytic membrane (124), sandwiched between a porous cathode (122) and a porous anode (126). A catalytic reaction combines the gases to form water, producing an electrical current as a byproduct. Adjacent chamber 132 are disposed a porous anode (134) and a porous cathode (138), sandwiched on each side of a catalytic membrane (136). An electric potential applied to porous anode (134) and porous cathode (138) transports water molecules and hydrogen from chamber (132) through catalytic membrane (136) into a chamber (140). The pressure in chamber (140) is substantially greater than the pressure in chamber (132).
    Type: Grant
    Filed: March 3, 1989
    Date of Patent: February 5, 1991
    Assignee: The Boeing Company
    Inventor: Devin W. Hersey
  • Patent number: 4829785
    Abstract: A cryogenic cooling system using hydrogen as a primary refrigerant fluid and oxygen as a secondary refrigerant fluid to precool the hydrogen gas below its inversion temperature. In a first embodiment, the cryogenic cooling system (10) includes an electrochemical compressor (12) operative to compress hydrogen and oxygen gas without any moving parts. Compressed oxygen from the electrochemical compressor passes through a regenerative heat exchanger (24) in heat transfer relationship with low pressure oxygen, and expands through a Joule-Thomson expansion valve (28) absorbing heat from a compressed hydrogen gas stream in a precooler heat exchange (30). The low pressure oxygen provides additional cooling in a parasitic heat exchangeer (36), returning to the electrochemical compressor through the regenerative heat exchanger (24).
    Type: Grant
    Filed: October 11, 1988
    Date of Patent: May 16, 1989
    Assignee: The Boeing Company
    Inventor: Devin W. Hersey