ClassID:

140310

F02K1/09 - CPC Classification

Classification description:

Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto; Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud

Recent Application in this class:
#1
20260110278
2026-04-23

VARIABLE AREA FAN NOZZLE ACTUATION SYSTEM

#2
20260071590
2026-03-12

VARIABLE FAN NOZZLE THRUST REVERSER ASSEMBLY

#3
20260043375
2026-02-12

DRIVE SYSTEM FOR TRANSLATING STRUCTURE

#4
20260002490
2026-01-01

Load Controlling Slider Assembly

#5
20250314218
2025-10-09

VARIABLE AREA NOZZLE ASSEMBLY

#6
20250230930
2025-07-17

COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

#7
20240401546
2024-12-05

TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM

#8
20240301844
2024-09-12

RAMJET PROPULSION METHOD

#9
20240092496
2024-03-21

Exhaust nozzle assembly for an aircraft propulsion system

#10
20240052799
2024-02-15

JET VECTORING APPARATUS

#11
20230265812
2023-08-24

Variable Area Fan Nozzle Actuation System

#12
20230075671
2023-03-09

Drive system for translating structure

#13
20230035756
2023-02-02

Variable area exhaust nozzle system and method for control thereof

#14
20220381200
2022-12-01

Drive system for translating structure

#15
20220195962
2022-06-23

SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIGH SPEED FLIGHT VEHICLE

#16
20220154643
2022-05-19

Geared turbofan engine gearbox arrangement

#17
20220049671
2022-02-17

Propulsion system arrangement for turbofan gas turbine engine

#18
20210404416
2021-12-30

Flexible sleeve for adjustable fan duct nozzle

#19
20210301761
2021-09-30

Variable area nozzle exhaust system with integrated thrust reverser

#20
20210262415
2021-08-26

High bypass ratio engine bypass duct nozzle with controlled nozzle area

#21
20210190004
2021-06-24

Exhaust nozzle of a gas turbine engine

#22
20210131380
2021-05-06

Drive system for translating structure

#23
20210062763
2021-03-04

Gas turbine engine variable area fan nozzle control

#24
20210040915
2021-02-11

Drive system for translating structure

#25
20210040914
2021-02-11

Drive system for translating structure

#26
20200400096
2020-12-24

Variable area fan nozzle for turbofan aircraft engine

#27
20200400071
2020-12-24

Geared turbofan engine gearbox arrangement

#28
20200325849
2020-10-15

Dual function cascade integrated variable area fan nozzle and thrust reverser

#29
20200325848
2020-10-15

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#30
20200317355
2020-10-08

Aircraft engine nacelle

#31
20200191156
2020-06-18

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#32
20200080513
2020-03-12

Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps

#33
20200032739
2020-01-30

Variable area fan nozzle with wall thickness distribution

#34
20200025150
2020-01-23

Ramjet propulsion method

#35
20200025148
2020-01-23

Translating outer cowl flow modulation device and method

#36
20200025147
2020-01-23

Propulsion system arrangement for turbofan gas turbine engine

#37
20200025140
2020-01-23

Bellmouth nozzle assembly for a gas turbine engine

#38
20200025035
2020-01-23

Gas turbine engine keel beam

#39
20200025022
2020-01-23

Dual-mode plug nozzle

#40
20190376470
2019-12-12

JET ENGINE WITH A RADIALLY VARIABLE WALL

#41
20190293020
2019-09-26

FLEXIBLE SLEEVE FOR ADJUSTABLE FAN DUCT NOZZLE

#42
20190218999
2019-07-18

Thrust reverser pivot door with extended forward edge

#43
20190162134
2019-05-30

RETENTION OF A NOZZLE ASSEMBLY FOR AN ENGINE

#44
20190136795
2019-05-09

Variable nozzle apparatus

#45
20190063367
2019-02-28

Hidden linkage for a translating cowl thrust reverser

#46
20190003422
2019-01-03

Gas turbine engine variable area fan nozzle control

#47
20180298924
2018-10-18

Nacelle for an aircraft turbojet engine provided with a hydraulic roto-linear actuator of a thrust reverser and of a variable-section nozzle

#48
20180298845
2018-10-18

Variable area fan nozzle actuation system

#49
20180119639
2018-05-03

Aircraft gas turbine engine nacelle

#50
20180094605
2018-04-05

TURBOFAN ENGINE FOR A CIVIL SUPERSONIC AIRCRAFT

#51
20170356387
2017-12-14

Dual function cascade integrated variable area fan nozzle and thrust reverser

#52
20170298870
2017-10-19

Thrust reverser of a turbofan pod comprising a single control for movable cowlings and a variable nozzle

#53
20170298867
2017-10-19

Sliding nozzle flap assembly

#54
20170167441
2017-06-15

Dielectric seal device

#55
20170138305
2017-05-18

Actuating device for moving a movable cover of a thrust reverser

#56
20170138303
2017-05-18

Gas turbine engine variable area fan nozzle with ice management

#57
20170107943
2017-04-20

Variable effective area fan nozzle

#58
20170082064
2017-03-23

Nacelle for an aircraft turbojet engine comprising a secondary nozzle section with rotary doors

#59
20170074211
2017-03-16

System and method for reducing idle thrust in a translating cowl thrust reverser

#60
20170074165
2017-03-16

Geared turbofan engine gearbox arrangement

#61
20170037813
2017-02-09

Exhaust nozzle with non-coplanar and/or non-axisymmetric shape

#62
20170016413
2017-01-19

Telescoping electrical cable

#63
20160369744
2016-12-22

Variable area fan nozzle hidden blocker door thrust reverser

#64
20160333822
2016-11-17

Variable area fan nozzle actuation system

#65
20160326984
2016-11-10

Thrust reversal for turbofan gas turbine engine

#66
20160288916
2016-10-06

Engine cowling of an aircraft gas turbine

#67
20160265476
2016-09-15

Sealing system for variable area fan nozzle

#68
20160245230
2016-08-25

Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

#69
20160230701
2016-08-11

Variable area fan nozzle with drive system health monitoring

#70
20160222917
2016-08-04

Nacelle for an aircraft engine with variable section nozzle

#71
20160208737
2016-07-21

System for actuating an exhaust cowl

#72
20160208641
2016-07-21

Translating variable area fan nozzle providing an upstream bypass flow exit

#73
20160186688
2016-06-30

Integrated thrust reverser actuation system

#74
20160169158
2016-06-16

Actuation system for a translating variable area fan nozzle

#75
20160169108
2016-06-16

Stepped fairing modulated exhaust cooling

#76
20160160798
2016-06-09

Integrated thrust reverser device and aircraft engine nacelle equipped therewith

#77
20160153356
2016-06-02

Geared turbofan engine gearbox arrangement

#78
20160097346
2016-04-07

Electric boost actuation system for translating rings

#79
20160025039
2016-01-28

Thrust reverser device

#80
20160010590
2016-01-14

Nozzle arrangement for a gas turbine engine

#81
20160003188
2016-01-07

Device for controlling a nozzle of variable cross-section of an aircraft

#82
20150369078
2015-12-24

Pivot door thrust reverser with variable area nozzle

#83
20150345423
2015-12-03

Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle

#84
20150315976
2015-11-05

Gas turbine engine variable area fan nozzle control

#85
20150308374
2015-10-29

Single actuator variable area fan nozzle system and method

#86
20150308373
2015-10-29

METHOD OF SCHEDULING PRESSURE IN VARIABLE PRESSURE ACTUATION SYSTEMS

#87
20150266588
2015-09-24

Aircraft comprising a control device for a jet pipe nozzle with variable cross-section powered by two independent electrical power supplies

#88
20150192092
2015-07-09

Sliding nozzle flap assembly

#89
20150143794
2015-05-28

Geared turbofan engine gearbox arrangement

#90
20150135678
2015-05-21

Gas turbine engine with noise attenuating variable area fan nozzle

#91
20150113941
2015-04-30

Translating outer cowl flow modulation device and method

#92
20150107220
2015-04-23

Variable area fan nozzle systems with improved drive couplings

#93
20150097056
2015-04-09

Thrust reverser with retractable cascade vanes

#94
20150082927
2015-03-26

Actuating device for moving a movable cover of a thrust reverser

#95
20140366554
2014-12-18

Variable area fan nozzle for gas turbine engine

#96
20140348630
2014-11-27

Noise reducing vane

#97
20140319243
2014-10-30

Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle

#98
20140234081
2014-08-21

TRANSLATING VARIABLE AREA FAN NOZZLE PROVIDING AN UPSTREAM BYPASS FLOW EXIT

#99
20140131481
2014-05-15

Threaded rod for system for deploying a deployable divergent segment of a thruster

#100
20140030057
2014-01-30

AFT cascade translating variable area fan nozzle

#101
20140027537
2014-01-30

Variable area fan nozzle with one or more integrated blocker doors

#102
20140026536
2014-01-30

Variable area fan nozzle position and skew sensing

#103
20140003916
2014-01-02

Turbomachine with fan(s) for aircraft, with mobile jet nozzle

#104
20140000238
2014-01-02

Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle

#105
20130312387
2013-11-28

Variable area fan nozzle actuation system

#106
20130292489
2013-11-07

Thrust reverser having a lockable variable nozzle section

#107
20130269312
2013-10-17

Device for controlling a variable section nozzle of an aircraft

#108
20130255225
2013-10-03

Gas turbine engine thrust reverser system

#109
20130200178
2013-08-08

Cascade-style variable area fan duct nozzle

#110
20130192247
2013-08-01

Gas turbine engine variable area fan nozzle with ice management

#111
20130192241
2013-08-01

Gas turbine engine variable area fan nozzle control

#112
20130186219
2013-07-25

Integrated thrust reverser actuator and variable area fan nozzle actuator

#113
20130167505
2013-07-04

Seal for a variable area fan nozzle

#114
20130160425
2013-06-27

Variable area fan nozzle with drive system health monitoring

#115
20130145743
2013-06-13

CASE ASSEMBLY WITH FUEL DRIVEN ACTUATION SYSTEMS

#116
20130104557
2013-05-02

Gas turbine engine exhaust nozzle cooling valve

#117
20130092756
2013-04-18

VARIABLE AREA NOZZLE FOR GAS TURBINE ENGINE

#118
20130092754
2013-04-18

NACELLE FOR A POWER PLANT WITH A VARIABLE-AREA FAN NOZZLE

#119
20130087661
2013-04-11

Propulsive unit for an aircraft

#120
20130062435
2013-03-14

Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle

#121
20130048807
2013-02-28

Multi axis slide carriage system

#122
20130026301
2013-01-31

NACELLE FOR VARIABLE SECTION NOZZLE PROPULSION UNIT

#123
20130025259
2013-01-31

Ducted fan gas turbine assembly

#124
20120291415
2012-11-22

Dual function cascade integrated variable area fan nozzle and thrust reverser

#125
20120192543
2012-08-02

EXHAUST NOZZLE FOR A BYPASS AIRPLANE TURBOJET HAVING A DEPLOYABLE SECONDARY COVER AND A RETRACTABLE CENTRAL BODY

#126
20120167549
2012-07-05

Flade discharge in 2-D exhaust nozzle

#127
20120137654
2012-06-07

Thrust reverser and variable area fan nozzle actuation system and method

#128
20120124963
2012-05-24

Method of varying a fan duct nozzle throat area of a gas turbine engine

#129
20120124962
2012-05-24

Method of varying a fan duct throat area

#130
20120111662
2012-05-10

ENGINE EXHAUST

#131
20120109593
2012-05-03

Gas turbine engine with variable area fan nozzle

#132
20120096831
2012-04-26

Gas turbine engine with variable area fan nozzle

#133
20120023901
2012-02-02

Variable area fan nozzle with acoustic system for a gas turbine engine

#134
20120011825
2012-01-19

Gas turbine engine with noise attenuating variable area fan nozzle

#135
20110318173
2011-12-29

Guide system for nacelle assembly

#136
20110296813
2011-12-08

Variable area fan nozzle with bypass flow

#137
20110289900
2011-12-01

Thrust reversing variable area nozzle

#138
20110277448
2011-11-17

Guide system for nacelle assembly

#139
20110154804
2011-06-30

Exhaust for a gas turbine engine

#140
20110120081
2011-05-26

Variable area fan nozzle bearing track

#141
20110120080
2011-05-26

Variable area fan nozzle cowl airfoil

#142
20110120079
2011-05-26

VARIABLE AREA FAN NOZZLE STIFFENERS AND PLACEMENT

#143
20110004388
2011-01-06

TURBOFAN TEMPERATURE CONTROL WITH VARIABLE AREA NOZZLE

#144
20100269511
2010-10-28

Nacelle for aircraft engine having a nozzle with a variable section

#145
20100229528
2010-09-16

Actuation system for a translating variable area fan nozzle

#146
20100229527
2010-09-16

Translating variable area fan nozzle providing an upstream bypass flow exit

#147
20100193632
2010-08-05

Integral composite slider for aircrafts

#148
20100115958
2010-05-13

Radially translating fan nozzle nacelle

#149
20100095650
2010-04-22

TRANSLATING CORE COWL FOR A GAS TURBINE ENGINE

#150
20100064659
2010-03-18

Translating variable area fan nozzle with split beavertail fairings

#151
20100050595
2010-03-04

GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE

#152
20100044503
2010-02-25

Jet engine nacelle for an aircraft and aircraft comprising such a nacelle

#153
20100005807
2010-01-14

Liquid propellant rocket engine with a propulsion chamber shutter

#154
20100005777
2010-01-14

Dual function cascade integrated variable area fan nozzle and thrust reverser

#155
20090320488
2009-12-31

Gas turbine engine with noise attenuating variable area fan nozzle

#156
20090288386
2009-11-26

Tri-body variable area fan nozzle and thrust reverser

#157
20090199536
2009-08-13

PROCESS FOR REVERSING THE THRUST PRODUCED BY A PROPULSION UNIT OF AN AIRCRAFT, DEVICE FOR ITS IMPLEMENTATION, NACELLE EQUIPPED WITH SAID DEVICE

#158
20090188233
2009-07-30

THRUST REVERSER FORMING AN ADAPTIVE NOZZLE

#159
20090094961
2009-04-16

Thrust reversing variable area nozzle

#160
20090067993
2009-03-12

COATED VARIABLE AREA FAN NOZZLE

#161
20090013664
2009-01-15

Thrust reverser and VAFN arrangement

#162
20080163606
2008-07-10

Variable area nozzle with woven sleeve extension

#163
20080156900
2008-07-03

Exhaust nozzle assembly

#164
20080155960
2008-07-03

Method of operating an exhaust nozzle assembly

#165
20080022690
2008-01-31

Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl

#166
20070214795
2007-09-20

Continuous real time EGT margin control

#167
20070000232
2007-01-04

Gas turbine engine and method of operating same

#168
20060277914
2006-12-14

Combi-Supersonic-Adjusting-Nozzle

#169
20060016171
2006-01-26

Split shroud exhaust nozzle

#170
20050103933
2005-05-19

Variable cam exhaust nozzle

#171
14497226
2018-08-07

Dual panel actuator system for jet engines