1
Brian R Smith, Seyed Saddoughi: Dual bimorph synthetic pulsator. Lockheed Martin Corporation, Bracewell & Giuliani, June 28, 2011: US07967258 (11 worldwide citation)

The present invention provides a system and method for actively manipulating fluid flow over a surface using synthetic pulsators. Synthetic pulsators produce pulsed jet operable to manipulate the primary fluid flow proximate to the synthetic pulsator. The synthetic pulsator includes a synthetic jet ...


2
Seyed Saddoughi, Matthew Boespflug, Scott Donnelly: Dual bimorph synthetic pulsator. Lockheed Martin Corporation, Bracewell & Giuliani, March 30, 2010: US07686257 (6 worldwide citation)

The present invention provides a system and method for actively manipulating fluid flow over a surface using synthetic pulsators. Synthetic pulsators produce pulsed jet operable to manipulate the primary fluid flow proximate to the synthetic pulsator. The synthetic pulsator includes a synthetic jet ...


3
Grover Bennett, Matthew Boespflug, Seyed Saddoughi: Synthetic jet apparatus. Lockheed Martin Corporation, Reising Ethington P C, John J Snyder, September 23, 2014: US08841820 (5 worldwide citation)

A synthetic jet apparatus including a series of generally parallel spaced-apart bimorph piezoelectric plates defining first and second sets of fluid chambers. The chambers of the second set of fluid chambers are interleaved with the chambers of the first set of fluid chambers. The first and second s ...


4
Seyed Saddoughi, Pierre Pinard, Matthew Boespflug, Dennis Steenburgh: Mixing-enhancement inserts for pulse detonation chambers. Lockheed Martin Corporation, Bracewell & Giuliani, April 21, 2009: US07520123 (3 worldwide citation)

The present invention provides a pulse detonation insert that induces flow obstructions within the pulse detonation chambers, wherein the flow obstructions are operable to induce turbulence within a primary fluid flow passing over the obstructions. This turbulence may take the form of vortices that ...


5
Anurag Gupta, Seyed Saddoughi: Method and apparatus for supersonic and shock noise reduction in aircraft engines using pneumatic corrugations. General Electric Company, Penny A Clarke, March 30, 2010: US07685806 (1 worldwide citation)

An aircraft engine is provided with at least one pulse detonation device connected to an engine exhaust nozzle portion with a plurality of supersonic injectors. The flow from the pulse detonation device is passed through the supersonic injectors into the primary engine flow path. The injector flow i ...


6
Seyed Saddoughi, Matthew Boespflug, Scott Donnelly: Dual bimorph synthetic pulsator. ROBERT A McLAUCHLAN, December 7, 2006: US20060273197-A1

The present invention provides a system and method for actively manipulating fluid flow over a surface using synthetic pulsators. Synthetic pulsators produce pulsed jet operable to manipulate the primary fluid flow proximate to the synthetic pulsator. The synthetic pulsator includes a synthetic jet ...


7
Anurag Gupta, Seyed Saddoughi: Method and apparatus for supersonic and shock noise reduction in aircraft engines using pneumatic corrugations. General Electric Company, General Electric Company, Global Research, July 5, 2007: US20070151254-A1

An aircraft engine is provided with at least one pulse detonation device connected to an engine exhaust nozzle portion with a plurality of supersonic injectors. The flow from the pulse detonation device is passed through the supersonic injectors into the primary engine flow path. The injector flow i ...


8
Seyed Saddoughi, Pierre Pinard, Matthew Boespflug, Dennis Steenburgh: Mixing-enhancement inserts for pulse detonation chambers. ROBERT A McLAUCHLAN, November 16, 2006: US20060254254-A1

The present invention provides a pulse detonation insert that induces flow obstructions within the pulse detonation chambers, wherein the flow obstructions are operable to induce turbulence within a primary fluid flow passing over the obstructions. This turbulence may take the form of vortices that ...


9
Brian R Smith, Seyed Saddoughi: Dual bimorph synthetic pulsator. Supersonic Aerospace International, Lockheed Martin Corporation, Bracewell & Giuliani, September 16, 2010: US20100229952-A1

The present invention provides a system and method for actively manipulating fluid flow over a surface using synthetic pulsators. Synthetic pulsators produce pulsed jet operable to manipulate the primary fluid flow proximate to the synthetic pulsator. The synthetic pulsator includes a synthetic jet ...


10
Seyed Saddoughi, Grover Bennett JR: Heat Resistant Piezo Bimorph Synthetic Jet Apparatus. Lockheed Martin Corporation, June 7, 2012: US20120138704-A1

A heat resistant piezo bimorph synthetic jet apparatus comprises a working fluid chamber partially defined by a plate, a working fluid port that provides fluid flow communication between the working fluid chamber and a working fluid mass, and a bimorph piezoelectric structure included in the plate. ...



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