Sevincer
Edip Sevincer, Schenectady, NY US
Patent application number | Description | Published |
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20090104028 | METHOD AND APPARATUS FOR DISTRIBUTING FLUID INTO A TURBOMACHINE - An apparatus for distributing a fluid in a gas flow path inside a turbomachine, comprising: a device for introducing the fluid into the gas flow path; and wherein the device is positioned within the gas flow path. A method for installing an apparatus that will distribute a fluid in a gas flow path inside a turbomachine, the method comprising: machining a casing groove along an inner surface of a casing; machining at least one port into the casing that is in fluid communication with the casing groove; machining an internal cavity in at least one stator blade that is in fluid communication with the casing groove; machining at least one orifice, that is in fluid communication with the internal cavity, on an orifice surface of the stator blade; and coupling a fluid supply to the at least one port. | 04-23-2009 |
20100143101 | COMPLIANT FOIL SEAL FOR ROTARY MACHINES - A compliant foil seal comprises a bottom foil configured to be located circumferentially around at least a portion of a rotor, and one or more upper foils configured to cooperate with a stator to position the bottom foil to compliantly face the rotor and be located between the stator and the rotor. A compliant foil seal assembly and a rotary machine are also presented. | 06-10-2010 |
Edip Sevincer, Scheneetady, NY US
Patent application number | Description | Published |
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20090085305 | HIGH TEMPERATURE SEAL - An apparatus for sealing gas path leakage within a turbomachine is provided. The apparatus may include at least one seal system, which may include at least one sealing shim, at least one spring; and at least one shim protection material. The seal system may be inserted between a first and a second structure of the turbomachine. The seal system may adjust for misalignments between the first and the second structures of the turbomachine. | 04-02-2009 |
Edip Sevincer, Watervliet, NY US
Patent application number | Description | Published |
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20120119447 | Transition Piece Sealing Assembly - The present application provides a seating assembly for use with a transition piece and a stage one nozzle of a gas turbine engine. The seating assembly may include a support member positioned between the transition piece and the stage one nozzle and a primary spring element positioned on the support member and in contact with the stage one nozzle. The primary spring element may include a single bend therein. | 05-17-2012 |
20120119449 | Transition Piece Sealing Assembly With Seal Overlay - The present application provides a sealing assembly for use with a transition piece and a stage one nozzle of a gas turbine engine. The sealing assembly may include a seal element, an overlay piece positioned on the seal element, and a side seal positioned on the overlay piece. | 05-17-2012 |