ClassID:

145419

F05D2250/121 - CPC Classification

Classification description:

Geometry; Two-dimensional rectangular square

Recent Application in this class:
#1
20240401533
2024-12-05

JOINTS BETWEEN ACOUSTIC PANELS

#2
20230160315
2023-05-25

Bore compartment seals for gas turbine engines

#3
20220186627
2022-06-16

LABYRINTH SEAL COMPRISING AN ABRADABLE ELEMENT WITH VARIABLE CELL DENSITY

#4
20220049610
2022-02-17

Impact-cooling tubular insert for a turbomachine distributor

#5
20220003121
2022-01-06

Inserts for airfoils of gas turbine engines

#6
20200024987
2020-01-23

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

#7
20200011248
2020-01-09

Reduced stress boss geometry for a gas turbine engine

#8
20190309634
2019-10-10

Turbine airfoil multilayer exterior wall

#9
20190145263
2019-05-16

TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES

#10
20190101003
2019-04-04

BLADES AND VANES FOR GAS TURBINE ENGINES AND THE MANUFACTURE THEREOF

#11
20190078446
2019-03-14

BLADE OF A TURBOMACHINE, INCLUDING A COOLING CHANNEL AND A DISPLACEMENT BODY SITUATED THEREIN, AS WELL AS A METHOD FOR MANUFACTURING

#12
20180265181
2018-09-20

Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole

#13
20180223680
2018-08-09

Nozzle assembly and method for forming nozzle assembly

#14
20180135519
2018-05-17

Turbine assembly

#15
20180058226
2018-03-01

Dual walled component for a gas turbine engine

#16
20170284212
2017-10-05

Seal carrier for a turbomachine, in particular a gas turbine

#17
20170145834
2017-05-25

AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER PEDESTALS FOR A GAS TURBINE ENGINE COMPONENT AND SYSTEMS FOR COOLING AN AIRFOIL PLATFORM

#18
20170058689
2017-03-02

Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element

#19
20160356222
2016-12-08

Reduced stress boss geometry for a gas turbine engine

#20
20160333735
2016-11-17

Angled impingement inserts with cooling features

#21
20160281510
2016-09-29

TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES

#22
20160258301
2016-09-08

Turbine rotor blade

#23
20160252016
2016-09-01

Gas turbine filtration system with inlet filter orientation assembly

#24
20160146041
2016-05-26

Blade or vane for a turbomachine and axial turbomachine

#25
20160040625
2016-02-11

Variable area nozzle and associated propulsion system and method

#26
20150040581
2015-02-12

Borescope assembly and method of installing borescope plugs

#27
20150014938
2015-01-15

Brush seal

#28
20140363300
2014-12-11

Closure bucket for turbo-machine

#29
20140086728
2014-03-27

Fan diffuser having a circular inlet and a rotationally asymmetrical outlet

#30
20110203282
2011-08-25

Assembly for directing combustion gas

#31
20110044822
2011-02-24

Gas turbine blade and gas turbine having the same

#32
20100247328
2010-09-30

Microcircuit cooling for blades

#33
20100077719
2010-04-01

Modular transvane assembly

#34
20080087021
2008-04-17

Ceramic matrix composite turbine engine components with unitary stiffening frame

#35
15272864
2017-11-14

Seal in a gas turbine engine having a shim base and a honeycomb structure with a number of cavities formed therein