ClassID:

145836

F05D2300/601 - CPC Classification

Classification description:

Materials; Properties thereof; Properties or characteristics given to material by treatment or manufacturing Fabrics

Sub-classes:
Recent Application in this class:
#1
20250376963
2025-12-11

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTING MEMBRANE

#2
20250341173
2025-11-06

CONTAINMENT RING FOR GAS TURBINE ENGINE

#3
20250264026
2025-08-21

FORMING GAS TURBINE ENGINE AIRFOILS FROM CMCS WITH A KICKBACK TO FACILITATE MANDREL REMOVAL

#4
20250101931
2025-03-27

THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE

#5
20240360773
2024-10-31

Fabric foreign material exclusion system

#6
20240018871
2024-01-18

Airfoil assembly with fiber-reinforced composite rings and toothed exit slot

#7
20230272718
2023-08-31

Airfoil having a structural cell and method of forming

#8
20230039569
2023-02-09

Thrust reverser comprising doors and at least one retractable deflector for closing a lateral opening

#9
20230020644
2023-01-19

Airfoil assembly with fiber-reinforced composite rings and toothed exit slot

#10
20220412288
2022-12-29

Textile cascade assembly

#11
20220403799
2022-12-22

Aircraft and direct drive engine under wing installation

#12
20220316426
2022-10-06

Door for thrust reverser of an aircraft propulsion assembly, comprising a flexible baffle

#13
20220282672
2022-09-08

FIRE PROTECTION STRUCTURE

#14
20220251958
2022-08-11

Reinforced blade

#15
20220243681
2022-08-04

Textile cascade assembly

#16
20210215049
2021-07-15

Fabric comprising aramid fibres for protecting a blade against impacts

#17
20200040822
2020-02-06

Thermal blanket for gas turbine engine

#18
20200011184
2020-01-09

Gas turbine blade

#19
20190093492
2019-03-28

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

#20
20180320633
2018-11-08

Aircraft and direct drive engine under wing installation

#21
20180245515
2018-08-30

Acoustic liner having multiple layers

#22
20180142698
2018-05-24

Fan blade with galvanic separator

#23
20180135635
2018-05-17

Airfoil structure having a shape memory alloy actuator

#24
20180128112
2018-05-10

Reinforced blade

#25
20180058331
2018-03-01

Corner flow reduction seals

#26
20180045064
2018-02-15

Hinged seal using wire mesh

#27
20180030892
2018-02-01

Inlet cap of an engine

#28
20180010614
2018-01-11

Non-Newtonian materials in aircraft engine airfoils

#29
20170369382
2017-12-28

Method of fabricating a fiber preform filled with refractory ceramic particles

#30
20170101878
2017-04-13

LOW MODULUS INSERT FOR A COMPONENT OF A GAS TURBINE ENGINE

#31
20170101876
2017-04-13

Fan platform for a gas turbine engine

#32
20170002667
2017-01-05

HEAT-RESISTANT TURBINE BLADE MADE FROM OXIDE CERAMIC

#33
20160327061
2016-11-10

Fire protection of a part made of a three-dimensional woven composite material

#34
20160222813
2016-08-04

Abradable Seal Material

#35
20160177780
2016-06-23

Blade arrangement of a jet engine or an aircraft propeller

#36
20160146030
2016-05-26

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

#37
20160123159
2016-05-05

Rotary device

#38
20160076391
2016-03-17

Hinged seal using wire mesh

#39
20160017712
2016-01-21

Turbine engine repair methods

#40
20160003062
2016-01-07

Fan blades with protective sheaths and galvanic shields

#41
20150198084
2015-07-16

Exhaust gas turbocharger

#42
20150192032
2015-07-09

Method for manufacturing a turbomachine casing from a composite material and associated casing

#43
20150003978
2015-01-01

Method for producing coupled turbine vanes, and turbine vanes

#44
20130136582
2013-05-30

Shroud segment producing method and shroud segment

#45
20130039769
2013-02-14

Centrifugal impeller and turbomachine

#46
20130028732
2013-01-31

ROLLING BEARING DEVICE HAVING A HYDRAULIC DAMPING DEVICE

#47
20120224967
2012-09-06

Elastic and Dust-Clinging Fan Blade Cover and Scent Pocket

#48
20120099982
2012-04-26

Turbine distributor element made of CMC, method for making same, distributor and gas turbine including same

#49
20120082808
2012-04-05

METHOD FOR INSTALLING HEAT SHIELDING ON A FIXED INTERNAL STRUCTURE OF A JET ENGINE NACELLE

#50
20110293828
2011-12-01

Method for manufacturing a complexly shaped composite material part

#51
20110241297
2011-10-06

Integral seal and sealant packaging

#52
20110121109
2011-05-26

Method of producing a nozzle or a divergent nozzle element made of a composite

#53
20110058953
2011-03-10

Turbine blade

#54
20100077721
2010-04-01

Composite fan case with integral containment zone

#55
20090263239
2009-10-22

Ring structure of metal construction having a run-in lining

#56
20090226310
2009-09-10

Containment cases and method of manufacture

#57
20090126336
2009-05-21

System providing braking in a gas turbine engine in the event of the turbine shaft breaking

#58
20090010762
2009-01-08

Damper for turbomachine vanes

#59
20080124222
2008-05-29

Heater assembly for deicing and/or anti-icing a component

#60
20080060752
2008-03-13

Rebonding a metallized fabric to an underlying layer

#61
20070272477
2007-11-29

Central body for a turbojet exhaust channel, turbojet

#62
20070187381
2007-08-16

Heater assembly for deicing and/or anti-icing a component

#63
20070069478
2007-03-29

Leakage seal for gas path of gas turbine

#64
20070020105
2007-01-25

Lamellate CMC structure with interlock to metallic support structure

#65
20060284337
2006-12-21

Interlaminar tensile reinforcement of SiC/SiC CMC's using fugitive fibers

#66
20060275133
2006-12-07

Customized fan blade and method of making same

#67
20060121296
2006-06-08

In-situ formed thermal barrier coating for a ceramic component

#68
20060121265
2006-06-08

Stacked laminate CMC turbine vane

#69
20060120874
2006-06-08

Stacked lamellate assembly

#70
20050232772
2005-10-20

Rotating seal arrangement for turbine bucket cooling circuits

#71
17976210
2024-03-26

Abradable material and design for jet engine applications