1
Elliot Matel Elliot Matel
Schmalz Jacob, Gulke John, Matel Elliot: Evaporative emissions control system. Briggs & Stratton, October 22, 2008: EP1983185-A2

The invention provides a fuel tank venting system for an engine. The fuel tank venting system includes a fuel tank (20), a carburetor (35), and a fuel tank vent passageway (50). The carburetor (35) is coupled to the fuel tank (20). The fuel tank vent passageway (50) is in fluid flow communication wi ...


2
Anthony S. McCoppin
Michael A Spohn, John A Haury, Anthony S McCoppin, John F Kalafut, Herbert M Grubic, James A Dedig: Fluid Delivery System, Fluid Path Set, and Pressure Isolation Mechanism with Hemodynamic Pressure Dampening Correction. Medrad, Gregory L Bradley, Medrad, July 12, 2007: US20070161970-A1

The fluid delivery system includes a pressurizing device for delivering injection fluid under pressure, a low pressure fluid delivery system, and a pressure isolation mechanism. The pressure isolation mechanism includes a first lumen associated with the pressurizing device, a second lumen associated ...


3
Anthony S. McCoppin
Michael A Spohn, John A Haury, Anthony S McCoppin, John F Kalafut, Herbert M Grubic, James A Dedig: Fluid Delivery System, Fluid Path Set, and Pressure Isolation Mechanism with Hemodynamic Pressure Dampening Correction. April 21, 2011: US20110092828-A1

The fluid delivery system includes a pressurizing device for delivering injection fluid under pressure, a low pressure fluid delivery system, and a pressure isolation mechanism. The pressure isolation mechanism includes a first lumen associated with the pressurizing device, a second lumen associated ...


4
Dan Miller
Philip P Truax, Daniel N Miller, Jeffrey W Hamstra, Patrick J Yagle: System and method for actively manipulating and controlling fluid flow over a surface. Lockheed Martin Corporation, Koestner Bertani, January 27, 2004: US06682021 (18 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic fluid flow over a surface. More specifically, the present invention provides a system and method to control aerodynamic or hydrodynamic fluid flow behavior of a ducted fluid flow ...


5
Charles Sperry
Hargrove William Walter, Harris Dale Carvin, Akers Michael James, Sperry Charles Richard: Vacuum vial infusion system.. Lilly Co Eli, June 26, 1985: EP0146310-A1 (12 worldwide citation)

This invention relates generally to systems for intravenously administering medicine to a patient and more particularly to a vacuum vial infusion system for reconstituting a drug from a dried state to a liquid state while the drug is still within the vial. The drug is administered by means of an int ...


6
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Lockheed Martin Corporation, Bracewell & Giuliani, March 31, 2009: US07510149 (11 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


7
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Lockheed Martin Corporation, Bracewell & Giuliani, October 18, 2011: US08038102 (9 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


8
Dan Miller
Daniel N Miller, Patrick J Yagle, Kerry B Ginn, Jeffrey W Hamstra: Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle. Lockheed Martin Corporation, Koesnter Bertani, November 8, 2005: US06962044 (6 worldwide citation)

The present invention reveals a method and apparatus for controlling the effective area and thrust vector angle of a fluid flow. In one embodiment, the fluid flow is controlled in an advanced, high aspect ratio, complex aperture geometry nozzle using asymmetric injection into the subsonic portion of ...


9
Dan Miller
Daniel N Miller, Brent N McCallum, Stewart A Jenkins, David M Wells: Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation. Bracewell & Giuliani, August 14, 2012: US08240616 (4 worldwide citation)

Systems and methods to provide distributed flow control actuation to manage the behavior of a global flow field, are provided. An example of a system can include an aerodynamic structure having an outer surface, and an array of a plurality of effectors connected to the outer surface of the aerodynam ...


10
Dan Miller
Daniel N Miller, Neal D Domel, Cole W Schemm: Exhaust plume heat effect reducing method and apparatus. Lockheed Martin Corporation, Reising Ethington P C, John J Snyder, November 27, 2012: US08316631 (2 worldwide citation)

An apparatus for reducing heating effects of an exhaust plume of a jet engine on an impinged surface includes fluid injectors disposed adjacent and aimed into an exhaust plume zone that's to be occupied by an exhaust plume when the engine is running. A flow generator transmits fluid flow into such a ...