ClassID:

145472

F05D2250/34 - CPC Classification

Classification description:

Geometry; Arrangement of components translated

Recent Application in this class:
#1
20230383710
2023-11-30

Articulating slider for nacelle

#2
20230193854
2023-06-22

Articulating slider for nacelle

#3
20230035756
2023-02-02

Variable area exhaust nozzle system and method for control thereof

#4
20220397078
2022-12-15

Thrust reverser with flaps controlled by a mechanism equipped with aeronautical bellcranks

#5
20220186684
2022-06-16

Thrust reverser provided with cable kinematics for scoop flaps

#6
20210270207
2021-09-02

Exhaust nozzle with vane support structure for a gas turbine engine

#7
20210207556
2021-07-08

Turbofan comprising a system comprising a screen for closing off the bypass duct

#8
20200248625
2020-08-06

Staggered heat exchanger array with side curtains

#9
20200025141
2020-01-23

Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means

#10
20200025140
2020-01-23

Bellmouth nozzle assembly for a gas turbine engine

#11
20190338727
2019-11-07

Hybrid articulating/translating trailing edge reverser

#12
20190024521
2019-01-24

Flow arrangement for placing in a hot gas duct of a turbomachine

#13
20180274484
2018-09-27

Jet engine comprising a nacelle equipped with reverser flaps

#14
20180238240
2018-08-23

Composite piston ring seal for axially and circumferentially translating ducts

#15
20180209376
2018-07-26

Aircraft thrust reverser system with alternate reverse thrust load path

#16
20180128183
2018-05-10

Turbine engine with a pair of contrarotating propellers placed upstream of the gas generator

#17
20170184033
2017-06-29

Method for the operation of a gas turbine by active hydraulic gap adjustment

#18
20170016412
2017-01-19

Thrust reverser of a turbojet engine nacelle, comprising control cylinders of movable cowls and a variable secondary nozzle

#19
20160348590
2016-12-01

Composite piston ring seal for axially and circumferentially translating ducts

#20
20160186688
2016-06-30

Integrated thrust reverser actuation system

#21
20160146155
2016-05-26

Gas turbine engine and method of assembling the same

#22
20160097346
2016-04-07

Electric boost actuation system for translating rings

#23
20160025039
2016-01-28

Thrust reverser device

#24
20160010507
2016-01-14

Retractable exhaust liner segment for gas turbine engines

#25
20150308374
2015-10-29

Single actuator variable area fan nozzle system and method

#26
20150292407
2015-10-15

Removable acoustic panels for turbojet engine casing

#27
20150125286
2015-05-07

ATR axial V-groove

#28
20150125285
2015-05-07

Integrated nozzle and plug

#29
20150125284
2015-05-07

ATR full ring sliding nacelle

#30
20150125270
2015-05-07

ATR guide pins for sliding nacelle

#31
20150059315
2015-03-05

Apparatus and method for bleeding off compressor air in a jet engine

#32
20140246514
2014-09-04

Turbomachine thrust reverser

#33
20140061332
2014-03-06

Thrust reverser for an aircraft jet engine

#34
20130280053
2013-10-24

Axial compressor

#35
20130125551
2013-05-23

Retractable exhaust liner segment for gas turbine engines

#36
20130075493
2013-03-28

Airplane jet engine thrust reverser having gratings or cascades

#37
20130047626
2013-02-28

Gas turbine engine generator switchable drive

#38
20120217320
2012-08-30

Thrust inverter with translatable cascade vanes having detachable front frame

#39
20120195742
2012-08-02

TURBINE BUCKET FOR USE IN GAS TURBINE ENGINES AND METHODS FOR FABRICATING THE SAME

#40
20120093652
2012-04-19

Unducted propeller with variable pitch blades for a turbomachine

#41
20110296813
2011-12-08

Variable area fan nozzle with bypass flow

#42
20110274549
2011-11-10

BLADE HAVING ASYMMETRICAL MID-SPAN STRUCTURE PORTIONS AND RELATED BLADED WHEEL STRUCTURE

#43
20100322775
2010-12-23

Anti-Erosion shield for rotor blades

#44
20100269511
2010-10-28

Nacelle for aircraft engine having a nozzle with a variable section

#45
20100229528
2010-09-16

Actuation system for a translating variable area fan nozzle

#46
20100229527
2010-09-16

Translating variable area fan nozzle providing an upstream bypass flow exit

#47
20100064659
2010-03-18

Translating variable area fan nozzle with split beavertail fairings

#48
20100054952
2010-03-04

Turbine blade

#49
20090010754
2009-01-08

Bearing-like structure to control deflections of a rotating component

#50
20080240915
2008-10-02

Airtight external shroud for a turbomachine turbine wheel

#51
20060024152
2006-02-02

Intake housing for axial fluid flow engines

#52
20060002796
2006-01-05

Turbine blade