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Class Information
Number: 415/209.4
Name: Rotary kinetic fluid motors or pumps > Working fluid passage or distributing means associated with runner (e.g., casing, etc.) > Vane or deflector > Plural and arcuately or circularly arranged in radial plane around runner axis > Having specific vane mounting means > Vane fixed between radially separate surfaces
Description: Device wherein the vane* or other directing means is held intermediate two structures at opposite ends of the vane or other directing means, and wherein the two structures lie at different distances from the runner"s* axis of rotation.


Patents under this class:
1 2 3

Patent Number Title Of Patent Date Issued
7600970 Ceramic matrix composite vane seals Oct. 13, 2009
7553130 Nozzle ring adhesive bonded blading for aircraft engine compressor Jun. 30, 2009
7510372 Wedge repair of mechanically retained vanes Mar. 31, 2009
7491030 Magnetically actuated guide vane Feb. 17, 2009
7470109 Machine tooled diaphragm partitions and nozzles Dec. 30, 2008
7452182 Multi-piece turbine vane assembly Nov. 18, 2008
7427187 Welded nozzle assembly for a steam turbine and methods of assembly Sep. 23, 2008
7410342 Airfoil support Aug. 12, 2008
7360990 Methods and apparatus for assembling gas turbine engines Apr. 22, 2008
7329087 Seal-less CMC vane to platform interfaces Feb. 12, 2008
7329096 Machine tooled diaphragm partitions and nozzles Feb. 12, 2008
7311495 Vane support in a gas turbine engine Dec. 25, 2007
7195454 Bullnose step turbine nozzle Mar. 27, 2007
7185433 Turbine nozzle segment and method of repairing same Mar. 6, 2007
7172388 Multi-point seal Feb. 6, 2007
7172389 Method for making a repaired turbine engine stationary vane assembly and repaired assembly Feb. 6, 2007
7160078 Mechanical solution for rail retention of turbine nozzles Jan. 9, 2007
7147434 Nozzle ring with adhesive bonded blading for aircraft engine compressor Dec. 12, 2006
7121793 Undercut flange turbine nozzle Oct. 17, 2006
7063505 Gas turbine engine frame having struts connected to rings with morse pins Jun. 20, 2006
7052234 Turbine vane collar seal May. 30, 2006
7048499 In-line centrifugal fan May. 23, 2006
6942453 Turbine nozzle segment Sep. 13, 2005
6935837 Methods and apparatus for assembling gas turbine engines Aug. 30, 2005
6921246 Methods and apparatus for assembling gas turbine nozzles Jul. 26, 2005
6905308 Turbine nozzle segment and method of repairing same Jun. 14, 2005
6884030 Methods and apparatus for securing multi-piece nozzle assemblies Apr. 26, 2005
6845558 Method of fabricating vanes Jan. 25, 2005
6793457 Fabricated repair of cast nozzle Sep. 21, 2004
6742987 Cradle mounted turbine nozzle Jun. 1, 2004
6685431 Method for repairing a turbine vane Feb. 3, 2004
6655912 Guide vane stage of a compressor Dec. 2, 2003
6644916 Vane and method of construction thereof Nov. 11, 2003
6626641 Nozzle for turbine Sep. 30, 2003
6619917 Machined fan exit guide vane attachment pockets for use in a gas turbine Sep. 16, 2003
6595747 Guide vane stage of a compressor Jul. 22, 2003
6579061 Selective step turbine nozzle Jun. 17, 2003
6558115 Turbine guide blade May. 6, 2003
6553665 Stator vane assembly for a turbine and method for forming the assembly Apr. 29, 2003
6547518 Low hoop stress turbine frame support Apr. 15, 2003
6517313 Segmented turbine vane support structure Feb. 11, 2003
6494677 Turbine nozzle segment and method of repairing same Dec. 17, 2002
6471470 Vane adjustment mechanism for variable capacity turbine, and assembling method for the same Oct. 29, 2002
6450763 Replaceable variable stator vane for gas turbines Sep. 17, 2002
6439841 Turbine frame assembly Aug. 27, 2002
6431830 Nozzle ring for a gas turbine Aug. 13, 2002
6416278 Turbine nozzle segment and method of repairing same Jul. 9, 2002
6409473 Low stress connection methodology for thermally incompatible materials Jun. 25, 2002
6409472 Stator assembly for a rotary machine and clip member for a stator assembly Jun. 25, 2002
6398485 Device for positioning of nozzles of a stator stage and for cooling of rotor discs in gas turbines Jun. 4, 2002

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