Patents Assigned to McVan Aerospace, LLC
  • Publication number: 20150014449
    Abstract: A method of operating a pressure compensated fuel injector includes: filling a fuel chamber with a charge of fuel by closing an injector valve and circulating a fuel from a fuel source through a plurality of recirculating valves and a cap valve; then isolating the fuel chamber and the charge of fuel from the fuel source; then equalizing a pressure within the fuel chamber to a rising pressure outside the fuel chamber by reducing a volume of the isolated fuel chamber; and then activating a solenoid that is coupled to the injector valve, opening the injector valve; and then further reducing the volume of the isolated fuel chamber to apply an over pressure within the chamber, pumping fuel from the fuel chamber through the injection orifice.
    Type: Application
    Filed: September 27, 2014
    Publication date: January 15, 2015
    Applicant: MCVAN AEROSPACE, LLC
    Inventors: Ray McKaig, Brian Donovan
  • Patent number: 8578894
    Abstract: Methods and apparatus are described for a reciprocating combustion engine. A method includes operating a dual-piston engine including introducing a gas into a pair of combustion chambers; introducing a fuel into the pair of combustion chambers; compressing the gas; combusting the gas and the fuel; and exhausting combusted gases. Each of the pistons drives a reciprocating crankshaft that protrudes through a cylinder wall and cooperatively rotate a pair of rotors by engaging substantially sinusoidal cam tracks on the rotors. An apparatus includes a cam driven, concentric drive rotary-valve dual-piston engine.
    Type: Grant
    Filed: July 9, 2012
    Date of Patent: November 12, 2013
    Assignee: McVan Aerospace, LLC
    Inventors: Ray McKaig, Brian Donovan
  • Patent number: 8215270
    Abstract: Methods and apparatus are described for a reciprocating combustion engine. A method includes operating a dual-piston engine including introducing a gas into a pair of combustion chambers; introducing a fuel into the pair of combustion chambers; compressing the gas; combusting the gas and the fuel; and exhausting combusted gases. Each of the pistons drives a reciprocating crankshaft that protrudes through a cylinder wall and cooperatively rotate a pair of rotors by engaging substantially sinusoidal cam tracks on the rotors. An apparatus includes a cam driven, concentric drive rotary-valve dual-piston engine.
    Type: Grant
    Filed: January 12, 2009
    Date of Patent: July 10, 2012
    Assignee: McVan Aerospace, LLC
    Inventors: Ray McKaig, Brian Donovan