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Class Information
Number: 60/755
Name: Power plants > Combustion products used as motive fluid > Combustion products generator > Combustor liner > Having means to direct flow along inner surface of liner
Description: Device having means to direct incoming air so that it has a flow component parallel with a wall of the flame enclosing means.










Sub-classes under this class:

Class Number Class Name Patents
60/756 Air directed to flow along inner surface of liner dome 145
60/757 In an axial direction 206


Patents under this class:
1 2 3 4

Patent Number Title Of Patent Date Issued
8695322 Thermally decoupled can-annular transition piece Apr. 15, 2014
8695351 Hula seal with preferential cooling having spring fingers and/or adjacent slots with different widths Apr. 15, 2014
8689562 Combustion cavity layouts for fuel staging in trapped vortex combustors Apr. 8, 2014
8689561 Vortex premixer for combustion apparatus Apr. 8, 2014
8677759 Ring cooling for a combustion liner and related method Mar. 25, 2014
8673234 Reactor vessel and liner Mar. 18, 2014
8671692 Annular gas turbine combustor including converging and diverging segments Mar. 18, 2014
8661828 Sealing between a combustion chamber and a turbine nozzle in a turbomachine Mar. 4, 2014
8661826 Combustion apparatus Mar. 4, 2014
8590314 Combustor liner helical cooling apparatus Nov. 26, 2013
8578715 Gas turbine, method of controlling air supply and computer program product for controlling air supply Nov. 12, 2013
8516822 Angled vanes in combustor flow sleeve Aug. 27, 2013
8490400 Combustor assembly comprising a combustor device, a transition duct and a flow conditioner Jul. 23, 2013
8490401 Annular combustion chamber for a gas turbine engine Jul. 23, 2013
8479524 Combustion chamber arrangement for operating a gas turbine Jul. 9, 2013
8453455 Paneled combustion liner having nodes Jun. 4, 2013
8429916 Dual walled combustors with improved liner seals Apr. 30, 2013
8413449 Gas turbine having an improved cooling architecture Apr. 9, 2013
8402764 Transition duct with spiral cooling channels Mar. 26, 2013
8387396 Airfoil, sleeve, and method for assembling a combustor assembly Mar. 5, 2013
8359867 Combustor having a flow sleeve Jan. 29, 2013
8333077 Replaceable orifice for combustion tuning and related method Dec. 18, 2012
8316541 Combustor heat shield with integrated louver and method of manufacturing the same Nov. 27, 2012
8307655 System for cooling turbine combustor transition piece Nov. 13, 2012
8307656 Gas turbine engine systems involving cooling of combustion section liners Nov. 13, 2012
8307657 Combustor liner cooling system Nov. 13, 2012
8291709 Combustion chamber of a turbomachine including cooling grooves Oct. 23, 2012
8272220 Impingement cooling plate for a hot gas duct of a thermal machine Sep. 25, 2012
8245513 Combustion chamber Aug. 21, 2012
8245514 Combustion liner for a gas turbine engine including heat transfer columns to increase cooling of a hula seal at the transition duct region Aug. 21, 2012
8240123 Integrated biomass energy system Aug. 14, 2012
8234872 Turbine air flow conditioner Aug. 7, 2012
8156744 Annular combustion chamber for a gas turbine engine Apr. 17, 2012
8151570 Transition duct cooling feed tubes Apr. 10, 2012
8141365 Plunged hole arrangement for annular rich-quench-lean gas turbine combustors Mar. 27, 2012
8127526 Recoatable exhaust liner cooling arrangement Mar. 6, 2012
8127553 Zero-cross-flow impingement via an array of differing length, extended ports Mar. 6, 2012
8113004 Wall element for use in combustion apparatus Feb. 14, 2012
8104288 Effusion cooling techniques for combustors in engine assemblies Jan. 31, 2012
8099961 Gas-turbine combustion chamber wall Jan. 24, 2012
8051662 Transition duct assemblies and gas turbine engine systems involving such assemblies Nov. 8, 2011
8051663 Gas turbine engine systems involving cooling of combustion section liners Nov. 8, 2011
8047008 Replaceable orifice for combustion tuning and related method Nov. 1, 2011
8024933 Wall elements for gas turbine engine combustors Sep. 27, 2011
8015818 Cooled transition duct for a gas turbine engine Sep. 13, 2011
8015829 Combustor Sep. 13, 2011
7992391 Transverse wall of a combustion chamber provided with multi-perforation holes Aug. 9, 2011
7966832 Combustor Jun. 28, 2011
7942005 Combustion chamber in a turbomachine May. 17, 2011
7895841 Method and apparatus to facilitate reducing NO.sub.x emissions in turbine engines Mar. 1, 2011

1 2 3 4










 
 
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