F05D2250/23 - CPC Classification Index

#1

20220106884

2022-04-07

Turbine engine component with deflector

#2

20200368851

2020-11-26

Systems and methods for manufacturing film cooling hole diffuser portion

#3

20200240638

2020-07-30

Film-cooled multi-walled structure with one or more indentations

#4

20200024987

2020-01-23

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

#5

20190120081

2019-04-25

Blade ring segment for turbine section, turbine section having the same, and gas turbine having the turbine section

#6

20190093493

2019-03-28

Seal structure for gas turbine rotor blade

#7

20190048931

2019-02-14

Intershaft seal assembly with multi-axis stepped grooves

#8

20180363466

2018-12-20

Turbine engine component with deflector

#9

20180361512

2018-12-20

Systems and methods for manufacturing film cooling hole diffuser portion

#10

20180328188

2018-11-15

Turbine engine airfoil insert

#11

20180320532

2018-11-08

Rotor assembly cover plate

#12

20180291769

2018-10-11

Mounted ceramic matrix composite component with clamped flange attachment

#13

20180291752

2018-10-11

Engine component with flow enhancer

#14

20180283184

2018-10-04

Turbine airfoil with biased trailing edge cooling arrangement

#15

20180230911

2018-08-16

Apparatus including heat exchanger and sound attenuator for gas turbine engine

#16

20180230064

2018-08-16

Ceramic matrix composite components having a deltoid region and methods for fabricating the same

#17

20180195396

2018-07-12

Blade, cut-back of blade or vane and gas turbine having the same

#18

20180163556

2018-06-14

Assembly of turbine engine parts comprising a fan blade having an integrated platform, and corresponding turbine engine

#19

20180023399

2018-01-25

Forming cooling passages in thermal barrier coated, combustion turbine superalloy components

#20

20170370241

2017-12-28

Turbine shroud with abradable layer having dimpled forward zone

#21

20170002674

2017-01-05

Turbine shroud with clamped flange attachment

#22

20160369636

2016-12-22

Turbine component thermal barrier coating with depth-varying material properties

#23

20160362989

2016-12-15

Turbine component thermal barrier coating with crack isolating engineered groove features

#24

20160348537

2016-12-01

Gas turbine diffuser outer diameter and inner diameter wall strips for turbine exhaust manifold pressure oscillation reduction

#25

20160333735

2016-11-17

Angled impingement inserts with cooling features

#26

20160319669

2016-11-03

Hollow blade having internal damper

#27

20160273771

2016-09-22

Film cooled multi-walled structure with one or more indentations

#28

20160273364

2016-09-22

Turbine engine component with diffuser holes

#29

20160251966

2016-09-01

Engine component

#30

20160230664

2016-08-11

Pedestals with heat transfer augmenter

#31

20160222828

2016-08-04

Blade outer air seal having angled retention hook

#32

20160201480

2016-07-14

Airfoil with an integrally stiffened composite cover

#33

20160186605

2016-06-30

Shroud assembly for a turbine engine

#34

20150369055

2015-12-24

Bell mouth inlet for turbine blade

#35

20150345305

2015-12-03

Fastback vorticor pin

#36

20150040581

2015-02-12

Borescope assembly and method of installing borescope plugs

#37

20140294598

2014-10-02

Turbine blade

#38

20140030102

2014-01-30

Turbine bucket with notched squealer tip

#39

20130302141

2013-11-14

Convective shielding cooling hole pattern

#40

20130216363

2013-08-22

Surface area augmentation of hot-section turbomachine component

#41

20130202439

2013-08-08

ROTATING ASSEMBLY FOR A TURBINE ASSEMBLY

#42

20120163993

2012-06-28

LEADING EDGE AIRFOIL-TO-PLATFORM FILLET COOLING TUBE

#43

20120051923

2012-03-01

Composite vane mounting

#44

20120027604

2012-02-02

Composite vane mounting

#45

20120003084

2012-01-05

Flow discouraging systems and gas turbine engines

#46

20110171010

2011-07-14

Sealing System Between a Shroud Segment and a Rotor Blade Tip and Manufacturing Method for Such a Segment

#47

20110085915

2011-04-14

Blade for a gas turbine

#48

20100021302

2010-01-28

Blade arrangement

#49

20090136350

2009-05-28

Damping and sealing system for turbine blades

#50

20080152475

2008-06-26

Method for preventing backflow and forming a cooling layer in an airfoil

#51

20080063521

2008-03-13

Curved variable pitch wedge retention in vane outer base

#52

20070246293

2007-10-25

Method and device for reducing engine noise

#53

20060093480

2006-05-04

Airfoil with three-pass serpentine cooling channel and microcircuit

#54

20060053767

2006-03-16

Method and device for reducing engine noise