F05D2300/437 - CPC Classification Index

#1

20240255056

2024-08-01

Non-metallic engine case inlet compression seal for a gas turbine engine

#2

20240011405

2024-01-11

System for an improved stator assembly

#3

20220259980

2022-08-18

System for an improved stator assembly

#4

20220221056

2022-07-14

Non-metallic engine case inlet compression seal for a gas turbine engine

#5

20210347700

2021-11-11

Preceramic ionic systems

#6

20210332762

2021-10-28

Air-sealing device intended to be inserted between an aircraft dual-flow turbine engine casing element, and a nacelle element

#7

20210231018

2021-07-29

Cooled polymer component

#8

20210123355

2021-04-29

SYSTEM FOR AN IMPROVED STATOR ASSEMBLY

#9

20210123354

2021-04-29

System for an improved stator assembly

#10

20200386166

2020-12-10

Isolation seals for gas turbine engines

#11

20200023452

2020-01-23

Attachment of structures having different physical characteristics

#12

20190271233

2019-09-05

Blade rub material

#13

20190218972

2019-07-18

THERMALLY PROTECTED THERMOPLASTIC DUCT AND ASSEMBLY

#14

20190218914

2019-07-18

Fan blade with filled pocket

#15

20190178092

2019-06-13

Cooled polymer component

#16

20190093492

2019-03-28

Non-metallic engine case inlet compression seal for a gas turbine engine

#17

20190062220

2019-02-28

Preceramic ionic systems

#18

20180291841

2018-10-11

Intermediate casing hub for an aircraft turbojet engine including a composite outlet pipe

#19

20180230840

2018-08-16

Two pieces stator inner shroud

#20

20180087386

2018-03-29

Fan for aircraft turbomachine

#21

20180010614

2018-01-11

Non-Newtonian materials in aircraft engine airfoils

#22

20170326587

2017-11-16

Method of protecting an article having a complex shape

#23

20170239762

2017-08-24

System and method for in situ repair of gas turbine engine casing clearance

#24

20170058688

2017-03-02

Ring-shaped thermomechanical part for turbine engine

#25

20160341216

2016-11-24

Blade and shroud with socket for a compressor of an axial turbomachine

#26

20160298479

2016-10-13

Fan blade platform seal with leading edge winglet

#27

20160222785

2016-08-04

Balancing apparatus, arrangement and method

#28

20160153298

2016-06-02

Method for assembling turbomachine parts and assembly used during such a method

#29

20160146030

2016-05-26

Non-metallic engine case inlet compression seal for a gas turbine engine

#30

20160123171

2016-05-05

Turbine shroud with locating inserts

#31

20160108753

2016-04-21

Insulating test engine hood for a turbine engine on a test bench

#32

20160032736

2016-02-04

COATING PROCESS AND COATED ARTICLE

#33

20160017712

2016-01-21

Turbine engine repair methods

#34

20160009927

2016-01-14

Antifouling layer for compressor blades

#35

20160003106

2016-01-07

Method for the production of a curved ceramic sound attenuation panel

#36

20160003075

2016-01-07

Gas turbine engine stator vane assembly with split shroud

#37

20150354380

2015-12-10

Organic matrix composite structural inlet guide vane for a turbine engine

#38

20150337668

2015-11-26

Blade rub material

#39

20150322809

2015-11-12

Blade rub material

#40

20150308277

2015-10-29

Blade retaining ring for an internal shroud of an axial-flow turbomachine compressor

#41

20150247412

2015-09-03

Turbine engine blade made of composite material with a bulb-shaped root

#42

20150202707

2015-07-23

Attachment of structures having different physical characteristics

#43

20150198056

2015-07-16

Abradable seal having nanolayer material

#44

20150078893

2015-03-19

Seal arrangement for a turbomachine and process for the production thereof

#45

20140030085

2014-01-30

Compliant assembly

#46

20130259658

2013-10-03

Variable vane inner platform damping

#47

20130189092

2013-07-25

Gas turbine engine stator vane assembly with inner shroud

#48

20130129494

2013-05-23

Axial turbomachine compressor outer casing

#49

20130108427

2013-05-02

Co-injected composite shell for an axial turbomachine compressor

#50

20120189438

2012-07-26

Gas turbine engine stator vane assembly

#51

20120073299

2012-03-29

High temperature manifolds for gas turbine engines

#52

20110241295

2011-10-06

Method of forming a seal element

#53

20100279104

2010-11-04

Turbine friendly abradable material

#54

20100266415

2010-10-21

Hybrid structure fan blade

#55

20090317228

2009-12-24

Apparatus and method for controlling a blade tip clearance for a compressor

#56

20090223632

2009-09-10

ABRADABLE MATERIAL COMPOSITION, A THERMOMECHANICAL PART OR CASING INCLUDING A COATING, AND A METHOD OF FABRICATING OR REPAIRING A COATING PRESENTING SAID COMPOSITION

#57

20090185909

2009-07-23

Self-assembly micro blade

#58

20070003412

2007-01-04

Abradable material composition, a thermomechanical part or casing including a coating, and a method of fabricating or repairing a coating presenting said composition