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Class Information
Number: 416/219R
Name: Fluid reaction surfaces (i.e., impellers) > Specific working member mount > Blade received in well or slot
Description:


Sub-classes under this class:

Class Number Class Name Patents
416/220R Having blade locking means 288
416/219A Non-turbo machine 21


Patents under this class:
1 2 3 4

Patent Number Title Of Patent Date Issued
7419362 Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1) Sep. 2, 2008
7419361 Blade/disk dovetail backcut for blade/disk stress reduction (7FA+e, stage 2) Sep. 2, 2008
7416393 Apparatus and method for joining a rotor blade to a rotor mount of a gas turbine rotor Aug. 26, 2008
7416389 Methods and apparatus for assembling rotatable machines Aug. 26, 2008
7399159 Detachable leading edge for airfoils Jul. 15, 2008
7329101 Ceramic composite with integrated compliance/wear layer Feb. 12, 2008
7326035 Device for attaching a moving blade to a turbine rotor disk in a turbomachine Feb. 5, 2008
7318704 Gas turbine engine structure Jan. 15, 2008
7306434 Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts Dec. 11, 2007
7300253 Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turb Nov. 27, 2007
7287958 Methods and apparatus for assembling rotatable machines Oct. 30, 2007
7278620 Fixture mounting assembly Oct. 9, 2007
7264447 Sealing arrangement for an axial turbine wheel Sep. 4, 2007
7217099 Coated forward stub shaft dovetail slot May. 15, 2007
7201558 Seal arrangement for a fan-turbine rotor assembly Apr. 10, 2007
7198463 Rotating blade body and rotary machine using rotating blade body Apr. 3, 2007
7182577 Turbine rotor blade and turbine Feb. 27, 2007
7165944 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge Jan. 23, 2007
7163375 Lightened interblade platform for a turbojet blade support disc Jan. 16, 2007
7156621 Blade fixing relief mismatch Jan. 2, 2007
7153102 Bladed disk fixing undercut Dec. 26, 2006
7134844 Install blade bracket for a ceiling suspended fan Nov. 14, 2006
7121803 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge Oct. 17, 2006
7104759 Compressor blade platform extension and methods of retrofitting blades of different blade angles Sep. 12, 2006
7090464 Methods and apparatus for assembling rotatable machines Aug. 15, 2006
7056094 Rotor and a retaining plate for the same Jun. 6, 2006
7029237 Retention capacity of blade having an asymmetrical hammerhead connection Apr. 18, 2006
7007382 Slot machining Mar. 7, 2006
6945754 Methods and apparatus for designing gas turbine engine rotor assemblies Sep. 20, 2005
6908285 Methods and apparatus for assembling rotatable machines Jun. 21, 2005
6902376 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge Jun. 7, 2005
6901821 Stator damper anti-rotation assembly Jun. 7, 2005
6893226 Rotor disc for gas turbine engine May. 17, 2005
6860721 Indentor arrangement Mar. 1, 2005
6860722 Snap on blade shim Mar. 1, 2005
6851932 Vibration damper assembly for the buckets of a turbine Feb. 8, 2005
6837685 Methods and apparatus for repairing a rotor assembly of a turbine Jan. 4, 2005
6811894 Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof Nov. 2, 2004
6773234 Methods and apparatus for facilitating preventing failure of gas turbine engine blades Aug. 10, 2004
6769877 Undercut leading edge for compressor blades and related method Aug. 3, 2004
6751863 Method for providing a rotating structure having a wire-arc-sprayed aluminum bronze protective coating thereon Jun. 22, 2004
6739837 Bladed rotor with a tiered blade to hub interface May. 25, 2004
6739836 Connection of blades on a rotor disc of a gas turbine May. 25, 2004
6692231 Molded fan having repositionable blades Feb. 17, 2004
6682307 Sealing system for a rotor of a turbo engine Jan. 27, 2004
6652237 Bucket and wheel dovetail design for turbine rotors Nov. 25, 2003
6602548 Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof Aug. 5, 2003
6592330 Method and apparatus for non-parallel turbine dovetail-faces Jul. 15, 2003
6582195 Compressor rotor blade spacer apparatus Jun. 24, 2003
6575704 Turbomachine and sealing element for a rotor thereof Jun. 10, 2003

1 2 3 4


 
 
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