F05D2300/606 - CPC Classification Index

#1

20240287650

2024-08-29

NICKEL-BASED SUPERALLOY, SINGLE-CRYSTAL BLADE AND TURBOMACHINE

#2

20220082065

2022-03-17

Geared gas turbine engine arrangement with core split power ratio

#3

20210355866

2021-11-18

Geared turbofan arrangement with core split power ratio

#4

20200109684

2020-04-09

Geared turbofan arrangement with core split power ratio

#5

20200080223

2020-03-12

Multifunctional nanocellular single crystal nickel for turbine applications

#6

20200025069

2020-01-23

Geared turbofan arrangement with core split power ratio

#7

20190126345

2019-05-02

DIRECTIONAL SOLIDIFICATION APPARATUS AND RELATED METHODS

#8

20180333772

2018-11-22

Hybrid turbine blade for improved engine performance or architecture

#9

20180202293

2018-07-19

Turbine component having multiple controlled metallic grain orientations, apparatus and manufacturing method thereof

#10

20170304929

2017-10-26

Dual alloy turbine rotors and methods for manufacturing the same

#11

20170268089

2017-09-21

Methods for processing bonded dual alloy rotors including differential heat treatment processes

#12

20170159461

2017-06-08

Stacking of rotor blades on centroids

#13

20170136536

2017-05-18

Casting methods and articles

#14

20170130289

2017-05-11

High elastic modulus shafts and method of manufacture

#15

20170022827

2017-01-26

Hybrid bonded turbine rotors and methods for manufacturing the same

#16

20160341045

2016-11-24

Method for forming components using additive manufacturing and re-melt

#17

20160298467

2016-10-13

ARTICLE HAVING VARIABLE COATING

#18

20160251772

2016-09-01

Multifunctional nanocellular single crystal nickel for turbine applications

#19

20160222802

2016-08-04

CMC blade with monolithic ceramic platform and dovetail

#20

20160222790

2016-08-04

Manufacturing method for a dual wall component

#21

20160168684

2016-06-16

Articles for high temperature service and method for making

#22

20160131084

2016-05-12

Geared turbofan arrangement with core split power ratio

#23

20160017733

2016-01-21

Multiple coating configuration

#24

20160003051

2016-01-07

Article with sections having different microstructures and method therefor

#25

20150354379

2015-12-10

Dual alloy turbine rotors and methods for manufacturing the same

#26

20150322799

2015-11-12

Method for forming components using additive manufacturing and re-melt

#27

20150321250

2015-11-12

Method for forming a directionally solidified replacement body for a component using additive manufacturing

#28

20150321249

2015-11-12

Hybrid turbine blade for improved engine performance or architecture

#29

20150121844

2015-05-07

Geared turbofan arrangement with core split power ratio

#30

20150013852

2015-01-15

Method for manufacturing components made of single crystal (SX) or directionally solidified (DS) nickelbase superalloys

#31

20140363305

2014-12-11

Hybrid turbine blade for improved engine performance or architecture

#32

20140123890

2014-05-08

Single crystal welding of directionally compacted materials

#33

20140060708

2014-03-06

High elastic modulus shafts and method of manufacture

#34

20130302533

2013-11-14

Repair of directionally solidified alloys

#35

20130216368

2013-08-22

Turbine stator airfoils with individual orientations

#36

20130189108

2013-07-25

Blade rim segment for a turbomachine and method for manufacture

#37

20130022803

2013-01-24

UNIDIRECTIONALLY-SOLIDIFICATION PROCESS AND CASTINGS FORMED THEREBY

#38

20120285933

2012-11-15

MONOCRYSTALLINE WELDING OF DIRECTIONALLY COMPACTED MATERIALS

#39

20120273468

2012-11-01

SINGLE CRYSTAL WELDING OF DIRECTIONALLY SOLIDIFIED MATERIALS

#40

20120251330

2012-10-04

Turbine airfoil component and method for making

#41

20120101792

2012-04-26

TURBINE COMPONENT AND METHOD FOR DEVELOPING A COMPONENT

#42

20110129347

2011-06-02

PROCESS FOR PRODUCING A JOIN TO SINGLE-CRYSTAL OR DIRECTIONALLY SOLIDIFIED MATERIAL

#43

20110008157

2011-01-13

Method of making turbine stator airfoils with individual orientations

#44

20100247291

2010-09-30

Gas turbine engine article having columnar microstructure

#45

20090297701

2009-12-03

Process for Repairing a Component with a Directional Microstructure

#46

20090297359

2009-12-03

High modulus metallic component for high vibratory operation

#47

20090280291

2009-11-12

Elongate component having longitudinal grains with different widths

#48

20080282972

2008-11-20

Method and mould for casting articles with a pre-determined crystalline orientation

#49

20070125299

2007-06-07

Method and mould for casting articles with a pre-determined crystalline orientation

#50

20060062674

2006-03-23

Axial-flow thermal turbomachine

#51

20050196268

2005-09-08

High modulus metallic component for high vibratory operation

#52

20050139581

2005-06-30

High-strength superalloy joining method for repairing turbine blades

#53

20050109818

2005-05-26

Welding method

#54

20050067065

2005-03-31

Method of removing casting defects

#55

20050050705

2005-03-10

Repair of nickel-based alloy turbine disk

#56

20050005444

2005-01-13

Process and apparatus for producing a turbine component, turbine component and use of the apparatus