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George Frey

George Frey, Houston, TX US

Patent application numberDescriptionPublished
20100068035APPARATUS AND METHOD FOR COOLING A TURBINE - A cooling system for a turbine includes a blower configured to generate a cooling gas flow to be passed through a rotor cavity of the turbine; piping configured to deliver the cooling gas flow to the turbine; and at least one valve configured to control the cooling gas flow. The piping is operatively connected to the rotor of the turbine. A method of cooling a turbine includes generating a cooling gas flow with a blower to be passed through a rotor cavity of the turbine; and delivering the cooling gas flow to the turbine.03-18-2010

George Frey, Englewood, CO US

Patent application numberDescriptionPublished
20090105760SYSTEMS AND METHODS FOR SPINAL STABILIZATION - Spinal stabilization systems are disclosed having spanning portions extending between and securable to pedicle screw assemblies, the spanning portions have stiffness characteristics that may be variable or selectively adjustable, and/or have non-linear behavior with respect to force versus distortion. Additionally, the systems may utilize a plurality of spanning portions in which two or more of the spanning portions have different stiffness characteristics.04-23-2009
20090105836Devices and techniques for a posterior lateral disc space approach - This invention relates to devices and instruments for implant insertion through a posterior lateral opening to the disc space. The instruments include an implant inserter, and the devices include a spinal fusion implant engageable by the implant inserter. The implant provides bilateral support of the adjacent vertebrae when inserted into the disc space from a postero-lateral approach.04-23-2009
20090177285Devices and techniques for a posterior lateral disc space approach - This invention relates to devices and instruments for implant insertion through a posterior lateral opening to the disc space. The instruments include an implant inserter, and the devices include a spinal fusion implant engageable by the implant inserter. The implant provides bilateral support of the adjacent vertebrae when inserted into the disc space from a postero-lateral approach.07-09-2009
20090281551METHODS AND APPARATUS FOR INSERTION OF INTERVERTEBRAL IMPLANTS AND DEVICES THEREFOR - Surgical device and methods for using same for distraction of adjacent vertebrae and insertion of an intervertebral implant material thereinbetween are disclosed. In a method, a leading end of the surgical device having major and minor dimensions is inserted between adjacent vertebrae with the minor dimension aligned in the rostral-caudal direction, and then the leading end is rotated to a second orientation to align the major dimension with the rostral-caudal direction. The surgical device includes slots permitting expansion thereof to allow an implant to be disposed from the leading end into the intervertebral space. In another form, the a first member of a surgical device is initially inserted in an orientation, and second member is moved relative to the first member to expand the first member for distracting the vertebrae, the implant then being disposed from the leading end into the intervertebral space.11-12-2009
20100004752Vertebral body and disc space replacement devices - A vertebral replacement device for supporting adjacent vertebrae includes a vertebral body member having at least one of an upper or lower disc replacement member engaged thereto at one end thereof. The disc replacement device can be positioned in a spinal disc space when disengaged from the vertebral body member.01-07-2010

Patent applications by George Frey, Englewood, CO US

George Frey, Greenville, SC US

Patent application numberDescriptionPublished
20090185894Turbine Casing - The turbine casing as described herein may include a first section flange, a second section flange, the first section flange and the second section flange meeting at a joint, and a heat sink positioned about the joint.07-23-2009
20090185898TURBINE CASING WITH FALSE FLANGE - A turbine casing may include an outer surface with a false flange and an inner surface with a heat sink positioned adjacent to the false flange.07-23-2009