Patents-Review.com
ClassID:

145603 ⎘

F05D2260/94 - CPC Classification

Classification description:

Function Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]

Sub-classes:
Recent Application in this class:
#1
20250257737
2025-08-14

CENTRIFUGAL COMPRESSOR IMPELLER AND METHOD OF PRODUCING THE SAME

 #2
20250257715
2025-08-14

PRESTRESSING DEVICE, AND A RELATED ARRANGEMENT, WIND TURBINE, AND METHOD

 #3
20250223907
2025-07-10

SUPER-COOLED ICE IMPACT PROTECTION FOR A GAS TURBINE ENGINE

 #4
20250027420
2025-01-23

Integrally bladed rotor with increased rim bending stiffness

 #5
20240426216
2024-12-26

Super-cooled ice impact protection for a gas turbine engine

 #6
20240093610
2024-03-21

Super-cooled ice impact protection for a gas turbine engine

 #7
20230228196
2023-07-20

Super-cooled ice impact protection for a gas turbine engine

 #8
20210372286
2021-12-02

Distributed nested cell damping system

 #9
20200376561
2020-12-03

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

 #10
20200240292
2020-07-30

Divot for outer case shroud

 #11
20200131931
2020-04-30

Additively deposited gas turbine engine cooling component

 #12
20190219484
2019-07-18

Gas turbine engine with lifing calculations based upon actual usage

 #13
20190128143
2019-05-02

Tunable compliant attachment structure

 #14
20190003482
2019-01-03

Multi-piece compressor wheel

 #15
20180326496
2018-11-15

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

 #16
20180252515
2018-09-06

Methods for monitoring components using micro and macro three-dimensional analysis

 #17
20180073390
2018-03-15

ADDITIVELY DEPOSITED GAS TURBINE ENGINE COOLING COMPONENT

 #18
20170336288
2017-11-23

Gas turbine engine with lifing calculations based upon actual usage

 #19
20170276145
2017-09-28

Blade with a platform and a hollow bumper

 #20
20170241292
2017-08-24

Turbomachine blade, comprising a root with reduced stress concentrations

 #21
20170114652
2017-04-27

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

 #22
20160369818
2016-12-22

FUEL PUMP

 #23
20160348587
2016-12-01

Brackets for gas turbine engine components

 #24
20160327055
2016-11-10

Fan blade with root through holes

 #25
20160201466
2016-07-14

Coating pocket stress reduction for rotor disk of a gas turbine engine

 #26
20160153290
2016-06-02

GAS TURBINE BLADE AND METHOD OF PROTECTING SAME

 #27
20160082510
2016-03-24

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

 #28
20160069188
2016-03-10

Gas turbine engine airfoil structure

 #29
20160047245
2016-02-18

Rotor for gas turbine engine

 #30
20160017716
2016-01-21

Turbomachine component with a stress relief cavity

 #31
20160003139
2016-01-07

Turbocharger

 #32
20150377139
2015-12-31

Exhaust flue

 #33
20150369067
2015-12-24

Structural guide vane outer diameter K gussets

 #34
20150345299
2015-12-03

Systems and methods for pre-stressing blades

 #35
20150292967
2015-10-15

Strain gauge and accelerometer measurement for thrust estimation

 #36
20150128613
2015-05-14

Tapered thread for gas turbine shroud

 #37
20140363307
2014-12-11

Rotor disc with fluid removal channels to enhance life of spindle bolt

 #38
20140308113
2014-10-16

Structure and method for providing compliance and sealing between ceramic and metallic structures

 #39
20140305129
2014-10-16

Gas turbine engine support strut assembly

 #40
20140290271
2014-10-02

Mounting arrangement

 #41
20140271119
2014-09-18

Method and apparatus for controlling modulated cooling of a gas turbine component

 #42
20140193267
2014-07-10

DMZ fracture boundary limit

 #43
20140147285
2014-05-29

Fixture for an airfoil shroud and method for modifying an airfoil shroud

 #44
20140119929
2014-05-01

Rotor blade for a turbomachine and turbomachine

 #45
20140112772
2014-04-24

Exhaust case for a turbomachine with a flexible hub

 #46
20140082912
2014-03-27

TURBOMACHINE INCLUDING A CRACK ARRESTMENT SYSTEM AND METHOD

 #47
20140076466
2014-03-20

Process for producing a turbine housing and turbine housing

 #48
20140003905
2014-01-02

Turbomachine monitoring system and method

 #49
20130186161
2013-07-25

Roll peening tooling and process

 #50
20130183149
2013-07-18

Housing-side structure of a turbomachine

 #51
20130156584
2013-06-20

COMPRESSOR ROTOR WITH INTERNAL STIFFENING RING OF DISTINCT MATERIAL

 #52
20130142631
2013-06-06

Exhaust gas housing for a gas turbine and gas turbine having an exhaust gas housing

 #53
20130125560
2013-05-23

Lateral turbojet improved in order to limit the deformation thereof

 #54
20130111907
2013-05-09

Hollow fan blade tuning using distinct filler materials

 #55
20130101434
2013-04-25

Support ring for a rotary assembly

 #56
20130078086
2013-03-28

Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg

 #57
20120308376
2012-12-06

Variable geometry turbocharger lower vane ring retaining system

 #58
20120213631
2012-08-23

Unflared compressor blade

 #59
20120207615
2012-08-16

Cooling of a gas turbine component designed as a rotor disk or turbine blade

 #60
20120166061
2012-06-28

Hub unit for a high temperature electronic monitoring system

 #61
20120163958
2012-06-28

Hub unit for a high temperature electronic monitoring system

 #62
20120137691
2012-06-07

Gas turbine assembly and method therefor

 #63
20120082551
2012-04-05

Gas turbine blade and method of protecting same

 #64
20120051938
2012-03-01

Shell for aircraft turbo-engine stator with mechanical blade load transfer slits

 #65
20120003086
2012-01-05

Turbine nozzles and methods of manufacturing the same

 #66
20110300342
2011-12-08

Ceramic coating systems and methods

 #67
20110296829
2011-12-08

Variable geometry exhaust turbocharger

 #68
20110274538
2011-11-10

Ceramic gas turbine shroud

 #69
20110158844
2011-06-30

Ring-shaped disk for gas turbine

 #70
20110158811
2011-06-30

Turbomachinery component

 #71
20110142597
2011-06-16

Turbine blade structure

 #72
20110113785
2011-05-19

THERMAL MACHINE

 #73
20110081234
2011-04-07

Gas turbine engine thermal expansion joint

 #74
20110064583
2011-03-17

Compressor impeller blade with variable elliptic connection

 #75
20110058953
2011-03-10

Turbine blade

 #76
20110048023
2011-03-03

Fuel nozzle swirler assembly

 #77
20110023499
2011-02-03

Gas turbine combustor exit duct and hp vane interface

 #78
20110008162
2011-01-13

Structure of radial turbine scroll

 #79
20100288052
2010-11-18

METHOD AND DEVICE FOR IMPLEMENTING SIMULATED TEST OF CENTRIFUGAL STRESS IN TURBINE BLADE

 #80
20100287948
2010-11-18

UNLOADED SPEED CONTROL FOR AVAILABILITY IMPROVEMENTS TO HEAVY FUEL FIRED GAS TURBINES

 #81
20100287944
2010-11-18

AVAILABILITY IMPROVEMENTS TO HEAVY FUEL FIRED GAS TURBINES

 #82
20100284811
2010-11-11

Turbine shroud ring with rotation proofing recess

 #83
20100236257
2010-09-23

Gas turbine combustor exit duct and HP vane interface

 #84
20100209234
2010-08-19

Method for producing a turbine housing and turbine housing

 #85
20100193605
2010-08-05

THERMALLY BALANCED AERO STRUCTURES

 #86
20100192590
2010-08-05

THERMALLY BALANCED MATERIALS

 #87
20100181366
2010-07-22

Control of case wall growth during repair and method

 #88
20100180605
2010-07-22

Structural attachment system for transition duct outlet

 #89
20100132376
2010-06-03

Mid turbine frame for gas turbine engine

 #90
20100132373
2010-06-03

Method of assembly and disassembly of a gas turbine mid turbine frame

 #91
20100132372
2010-06-03

Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine

 #92
20100086401
2010-04-08

Stator vane assembly

 #93
20100080695
2010-04-01

Turbine nozzle for a gas turbine engine

 #94
20100054954
2010-03-04

Turbine bucket for a turbomachine and method of reducing bow wave effects at a turbine bucket

 #95
20100014962
2010-01-21

Turbine vane of a gas turbine

 #96
20100008774
2010-01-14

Variable geometry turbocharger lower vane ring retaining system

 #97
20090317247
2009-12-24

Exhaust-driven turbocharger for a motor vehicle

 #98
20090246014
2009-10-01

Method and system for supporting stator components

 #99
20090191053
2009-07-30

Diaphragm and blades for turbomachinery

 #100
20090148298
2009-06-11

BLADE DISK SEAL

 #101
20090136352
2009-05-28

Turbomachine blade

 #102
20090136347
2009-05-28

Turbine bucket shroud internal core profile

 #103
20090120102
2009-05-14

Turbine engine frame having an actuated equilibrating case

 #104
20090038151
2009-02-12

Method for establishing a location of an elevated stress region

 #105
20090022600
2009-01-22

Steam turbine rotating blade

 #106
20090022599
2009-01-22

Methods and apparatus for assembling a steam turbine bucket

 #107
20090016873
2009-01-15

Gas turbine systems involving feather seals

 #108
20080286099
2008-11-20

Steam turbine exhaust hood and method of fabricating the same

 #109
20080286098
2008-11-20

Wear minimization system for a compressor diaphragm

 #110
20080284109
2008-11-20

Seal assembly

 #111
20080260535
2008-10-23

Blade/disk dovetail backcut for blade/disk stress reduction (6FA+E, stage2)

 #112
20080181779
2008-07-31

Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies

 #113
20080063529
2008-03-13

Undercut fillet radius for blade dovetails

 #114
20080003109
2008-01-03

Component of variable thickness having residual compressive stresses therein, and method therefor

 #115
20070292271
2007-12-20

Rotor blade for a compressor or a gas turbine

 #116
20070269316
2007-11-22

TURBINE BLADE WITH TRAILING EDGE CUTBACK AND METHOD OF MAKING SAME

 #117
20070243067
2007-10-18

Gas turbine or compressor blade

 #118
20070172357
2007-07-26

Predicting crack propagation in the shaft dovetail of a generator rotor

 #119
20070158388
2007-07-12

Apparatus and method for welding superalloys

 #120
20070147996
2007-06-28

Airfoil with heating source

 #121
20070140855
2007-06-21

Turbine disk

 #122
20070122275
2007-05-31

Methods and apparatus for assembling turbine nozzles

 #123
20070122266
2007-05-31

ASSEMBLY FOR CONTROLLING THERMAL STRESSES IN CERAMIC MATRIX COMPOSITE ARTICLES

 #124
20070089414
2007-04-26

Exhaust turbo-supercharger

 #125
20070033941
2007-02-15

Transition piece for gas turbine

 #126
20060045732
2006-03-02

Duct with integrated baffle

 #127
20060013683
2006-01-19

Spacer arrangement

 #128
20060008350
2006-01-12

Turbine blade

 #129
20050175462
2005-08-11

Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels

 #130
20050169761
2005-08-04

Rotor blade for a rotary machine

 #131
20050169758
2005-08-04

Rotor blade for a rotary machine

 #132
20050085949
2005-04-21

Method and apparatus for controlling steam turbine inlet flow to limit shell and rotor thermal stress

 #133
20050036890
2005-02-17

Conical tip shroud fillet for a turbine bucket

 #134
20050002780
2005-01-06

Turbine shroud segment