Patents Assigned to TGS Innovations, LP
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Publication number: 20090101089Abstract: A power-generation device comprising at least one cylinder, at least one cylinder head, at least one piston having a crown for improved lubricant circulation and an output shaft, having a central axis having a fixed angular relationship to the central axis of the cylinder. A swash plate, having a first swash plate surface having a normal axis disposed at a first fixed angle to the central axis of the output shaft, is fixed to the output shaft. At least one connecting rod is connected to at least one piston. At least one follower is secured to the second end of a connecting rod. The first follower surface contacts, and conforms to, the orientation of the first swash plate surface.Type: ApplicationFiled: December 22, 2008Publication date: April 23, 2009Applicant: TGS Innovations, LPInventor: Thomas Glenn Stephens
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Patent number: 7469665Abstract: A power-generation device comprising at least one cylinder, at least one cylinder head, at least one piston and an output shaft, having a central axis having a fixed angular relationship to the central axis of the cylinder. A swash plate, having a first swash plate surface having a normal axis disposed at a first fixed angle to the central axis of the output shaft, is fixed to the output shaft. At least one connecting rod is connected to at least one piston. At least one follower is secured to the second end of a connecting rod. The first follower surface contacts, and conforms to, the orientation of the first swash plate surface.Type: GrantFiled: October 23, 2006Date of Patent: December 30, 2008Assignee: TGS Innovations LPInventor: Thomas Glenn Stephens
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Publication number: 20070164146Abstract: A rotary wing aircraft is provided with longitudinally oriented counter-rotating rotors with circumferentially spaced variable pitch rotor blades connected to rotatable support rings mounted on the aircraft fuselage. Rotor downwash may be guided laterally and longitudinally by respective sets of moveable guide vanes. Propulsion may be obtained by an engine providing thrust and power take-off for driving the rotors. An auxiliary or second engine may be drivingly connected to the rotors. One embodiment includes rotors with lift or blade pitch angle control mechanism for changing the resultant lift forces for providing aircraft lateral movement and movement about a yaw axis. A wind driven power turbine includes a similar pitch angle control mechanism.Type: ApplicationFiled: April 26, 2006Publication date: July 19, 2007Applicant: TGS INNOVATIONS, LPInventor: Thomas Stephens
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Publication number: 20070034178Abstract: A power-generation device comprising at least one cylinder, at least one cylinder head, at least one piston and an output shaft, having a central axis having a fixed angular relationship to the central axis of the cylinder. A swash plate, having a first swash plate surface having a normal axis disposed at a first fixed angle to the central axis of the output shaft, is fixed to the output shaft. At least one connecting rod is connected to at least one piston. At least one follower is secured to the second end of a connecting rod. The first follower surface contacts, and conforms to, the orientation of the first swash plate surface.Type: ApplicationFiled: October 23, 2006Publication date: February 15, 2007Applicant: TGS INNOVATIONS, LPInventor: Thomas Stephens
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Patent number: 7137366Abstract: A power-generation device comprising at least one cylinder, at least one cylinder head, at least one piston and an output shaft, having a central axis having a fixed angular relationship to the central axis of the cylinder. A swash plate, having a first swash plate surface having a normal axis disposed at a first fixed angle to the central axis of the output shaft, is fixed to the output shaft. At least one connecting rod is connected to at least one piston. At least one follower is secured to the second end of a connecting rod. The first follower surface contacts, and conforms to, the orientation of the first swash plate surface.Type: GrantFiled: September 10, 2004Date of Patent: November 21, 2006Assignee: TGS Innovations, LPInventor: Thomas Glenn Stephens
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Publication number: 20060249621Abstract: A rotary wing aircraft is provided with longitudinally oriented counter-rotating rotors with circumferentially spaced variable pitch elongated rotor blades connected at their opposite ends to rotatable support rings mounted on the aircraft fuselage. Rotor downwash may be guided laterally and longitudinally by respective sets of moveable guide vanes. Propulsion may be obtained by an engine providing thrust and power take-off for driving the rotors. An auxiliary or second engine may be drivingly connected to the rotors.Type: ApplicationFiled: May 4, 2005Publication date: November 9, 2006Applicant: TGS INNOVATIONS, LPInventor: Thomas Stephens