Samer P. Wasif patents - FreshPatents.com
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Samer P. Wasif patents ... Muzaffer Sutcu, Walter R. Laster Utilizing a diluent to lower combustion instabilities in a gas turbine engine
All web results to the name "Muzaffer Sutcu"
CN A - 用于燃气涡轮机的过渡管道- Google Patentswww.google.com › patents
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US A1 * Muzaffer Sutcu Stepped inlet ring for a transition downstream from a combustor basket in a combustion turbine engine.
US A - High energy ignition device - Google Patentswww.google.com › patents
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US A1 * Muzaffer Sutcu Gas turbine igniter. US B Pratt & Whitney Canada Corp.
Patents - Orlando Sentinelwww.orlandosentinel.com › os-cfb-patents story,amp
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Dec 14, · Muzaffer Sutcu, Oviedo; and Ulrich Woerz, Oviedo. Gas turbine igniter with structure to reduce radial movement of igniter rod.
US A - High temperature, flexible pressure-actuated, brush seal...
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A high temperature, flexible brush seal comprises a bundle of fibers or bristles held tightly together and secured at one end with a backing plate. The...
Patent US Self-adjusting seal structure - Google Patenten
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Muzaffer Sutcu: Seal System Between Transition Duct Exit Section and Turbine Inlet in a Gas Turbine Engine: US * 16 dec 2009: 16 juni 2011: Muzaffer Sutcu:
Patent US High temperature flexible seal - Google Patents
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This device is concerned with sealing the sliding interfaces between structural panels that are roughly perpendicular to each other or whose edges are butted...
GAS TURBINE IGNITER - Patent application
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... map information provided by CartoDB, OpenStreetMap and contributors, CC-BY-SA. Patent applications by Muzaffer Sutcu, Oviedo, FL US.
Sutcu - Patent applications
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Muzaffer Sutcu, Oviedo, FL US. Patent application number Description Published; : Seal System Between Transition Duct Exit Section and Turbine Inlet in …
Patent EP A1 - A transition duct for a gas turbine - Google ...
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US *, 27 Aug 2010, 1 Mar 2012, Muzaffer Sutcu, Stepped inlet ring for a transition downstream from a combustor basket in a ...
Patent EP A1 - Conduit de transition pour turbine à gaz ...
patents.google.com
US *, 27 Aug 2010, 1 Mar 2012, Muzaffer Sutcu, Stepped inlet ring for a transition downstream from a combustor basket in a combustion turbine ...
US A - Igniter Google Patents
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Apr , Kiyoteru Mori, Spark plug and internal combustion engine provided with the same. US *, 3. Mai 2011, 8. Nov , Muzaffer Sutcu, Gas ...
US A - High energy ignition device Google Patents
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A spark igniter for gas turbine engines, having passage means for positioning a small quantity of liquid fuel directly in the path of the spark, which...
Patent US Gas turbine engine having an improved transition ...
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US *, 3 Mar 2011, Muzaffer Sutcu, Seal System Between ... Muzaffer Sutcu, Seal Member for Use in a Seal System Between a Transition Duct Exit ...
US B1 - Thermally free aft frame for a transition duct ...www.google.com › patents
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US A1 * Muzaffer Sutcu Seal System Between Transition Duct Exit Section and Turbine Inlet in a Gas Turbine Engine.
Patent US High-temperature, flexible, thermal barrier seal ...
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März 2011, Muzaffer Sutcu, Seal System Between Transition Duct Exit Section ... Juni 2011, Muzaffer Sutcu, Seal Member for Use in a Seal System Between a ...
Patent US Combination transition piece floating cloth seal ...
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US *, 3 maart 2011, Muzaffer Sutcu, Seal System Between ... US *, 16 dec 2009, 16 juni 2011, Muzaffer Sutcu, Seal Member for Use ...
Patente EP A1 - Conduit de transition pour turbine à gaz ...
patents.google.com
US *, 27 Ago 2010, 1 Mar 2012, Muzaffer Sutcu, Stepped inlet ring for a transition downstream from a combustor basket in a combustion turbine ...
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