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Class Information
Number: 415/173.1
Name: Rotary kinetic fluid motors or pumps > Bearing, seal, or liner between runner portion and static part > Between blade edge and static part
Description: Device wherein the means is located between a peripheral part of a working member blade* on the runner* and the fixed element.


Sub-classes under this class:

Class Number Class Name Patents
415/173.4 Erodable or permanently deformable 229
415/173.5 Labyrinth seal 132
415/173.3 Resilient, flexible, or resiliently biased 160
415/173.2 Selectively adjustable 99


Patents under this class:
1 2 3 4 5 6 7 8

Patent Number Title Of Patent Date Issued
7628587 Gas turbine blade shroud Dec. 8, 2009
7625169 Variable displacement turbine liner Dec. 1, 2009
7621719 Multiple cooling schemes for turbine blade outer air seal Nov. 24, 2009
7614845 Turbomachine inner casing fitted with a heat shield Nov. 10, 2009
7611324 Method and system to facilitate enhanced local cooling of turbine engines Nov. 3, 2009
7607885 Methods and apparatus for operating gas turbine engines Oct. 27, 2009
7607893 Counter tip baffle airfoil Oct. 27, 2009
7604453 Methods and system for recuperated circumferential cooling of integral turbine nozzle and shroud assemblies Oct. 20, 2009
7604455 Rotor disc assembly with abrasive insert Oct. 20, 2009
7600977 Turbine blade tip cap Oct. 13, 2009
7600967 Stator assembly, module and method for forming a rotary machine Oct. 13, 2009
7597533 BOAS with multi-metering diffusion cooling Oct. 6, 2009
7591632 Side channel compressor with housing shells and running wheel Sep. 22, 2009
7588412 Cooled shroud assembly and method of cooling a shroud Sep. 15, 2009
7575409 Apparatus and method for active control of blade tip clearance Aug. 18, 2009
7563071 Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine Jul. 21, 2009
7563069 Clip Jul. 21, 2009
7563074 Impeller for a centrifugal compressor Jul. 21, 2009
7559740 Protection device for a turbine stator Jul. 14, 2009
7559741 Turbomachine having an axially displaceable rotor Jul. 14, 2009
7556475 Methods and apparatus for assembling turbine engines Jul. 7, 2009
7553128 Blade outer air seals Jun. 30, 2009
7549840 Through thickness reinforcement of SiC/SiC CMC's through in-situ matrix plugs manufactured using fugitive fibers Jun. 23, 2009
7534086 Multi-layer ring seal May. 19, 2009
7524166 Compressor cleaning system Apr. 28, 2009
7524220 Water jet propeller Apr. 28, 2009
7517189 Cooling circuit for gas turbine fixed ring Apr. 14, 2009
7513740 Turbine ring Apr. 7, 2009
7513040 Manufacturable and inspectable cooling microcircuits for blade-outer-air-seals Apr. 7, 2009
7494317 Ring seal attachment system Feb. 24, 2009
7478993 Cooling fan using Coanda effect to reduce recirculation Jan. 20, 2009
7465145 Tip clearance control system Dec. 16, 2008
7458772 Guide vane ring of a turbomachine and associated modification method Dec. 2, 2008
7452183 Thermally compliant turbine shroud assembly Nov. 18, 2008
7448846 Thermally compliant turbine shroud mounting Nov. 11, 2008
7448849 Seal Nov. 11, 2008
7448850 Closed loop, steam cooled turbine shroud Nov. 11, 2008
7442004 Thermally compliant C-clip Oct. 28, 2008
7438520 Thermally compliant turbine shroud mounting assembly Oct. 21, 2008
7410173 Hydrodynamic brush seal Aug. 12, 2008
7407368 Turbine shroud segment Aug. 5, 2008
7387488 Cooled turbine shroud Jun. 17, 2008
7371043 CMC turbine shroud ring segment and fabrication method May. 13, 2008
7367776 Turbine engine stator including shape memory alloy and clearance control method May. 6, 2008
7360989 Device for axially holding a ring spacer sector of a high-pressure turbine of a turbomachine Apr. 22, 2008
7360991 Methods and apparatus for fabricating gas turbine engines Apr. 22, 2008
7338251 Turbo compressor Mar. 4, 2008
7338250 Gas turbine engine blade containment assembly Mar. 4, 2008
7334985 Shroud with aero-effective cooling Feb. 26, 2008
7334984 Turbine shroud assembly with enhanced blade containment capabilities Feb. 26, 2008

1 2 3 4 5 6 7 8


 
 
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