F05D2250/42 - CPC Classification Index

#1

20250075664

2025-03-06

AERO-ACOUSTICALLY DAMPENED BLEED VALVE

#2

20240280033

2024-08-22

INSERTION TOOL AND METHOD

#3

20230358181

2023-11-09

Aero-acoustically dampened bleed valve

#4

20230228220

2023-07-20

Aero-acoustically dampened bleed valve

#5

20220056851

2022-02-24

Tube assembly for a gas turbine engine

#6

20210388737

2021-12-16

Insertion tool and method

#7

20210033044

2021-02-04

Gimbal assembly and manufacture thereof

#8

20200217271

2020-07-09

Linkage assembly preventing axial rotation of the link rod for a gas turbine engine

#9

20190170088

2019-06-06

System for actuating a panel of a turbojet engine nacelle

#10

20190145274

2019-05-16

Variable displacement turbocharger

#11

20190078533

2019-03-14

Linkage assembly preventing axial rotation of the link rod

#12

20180372026

2018-12-27

Gimbal assembly and manufacture thereof

#13

20180371949

2018-12-27

PLANT SYSTEMS

#14

20180245484

2018-08-30

Oil tank mount arrangement on a geared turbofan engine

#15

20180149113

2018-05-31

Turbofan nacelle including a reverser flap

#16

20180030849

2018-02-01

Device for the individual adjustment of a plurality of variable-pitch radial stator vanes in a turbomachine

#17

20170082064

2017-03-23

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

#18

20170044982

2017-02-16

Heat exchanger for cooled cooling air

#19

20160326896

2016-11-10

Turbine component connection with thermally stress-free fastener

#20

20160273389

2016-09-22

Oil tank mount arrangement on a geared turbofan engine

#21

20160169156

2016-06-16

Thrust reverser system with translating-rotating hinge assembly

#22

20160040625

2016-02-11

Variable area nozzle and associated propulsion system and method

#23

20150307189

2015-10-29

Set of swashplates for controlling the pitch of rotor blades, a rotor and an aircraft having such a set

#24

20150226155

2015-08-13

Thrust deflecting device and aircraft engine

#25

20150159502

2015-06-11

Exhaust gas turbocharger, in particular for a motor vehicle

#26

20140366453

2014-12-18

Panel attachment system and a method of using the same

#27

20140245750

2014-09-04

Circumferentially retained fairing

#28

20140245747

2014-09-04

Gas turbine engine two degree of freedom variable bleed valve for ice extraction

#29

20140212306

2014-07-31

Turbine, particularly for an exhaust gas turbocharger, and exhaust gas turbocharger

#30

20140131481

2014-05-15

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

#31

20130306755

2013-11-21

Linked ring petal actuation for variable area fan nozzle

#32

20120304665

2012-12-06

MOUNT DEVICE FOR TRANSITION DUCT IN TURBINE SYSTEM

#33

20110262266

2011-10-27

Linear Actuator for a Variable-Geometry Member of a Turbocharger, and a Turbocharger Incorporating Same

#34

20110255973

2011-10-20

Damping element and method for damping rotor blade vibrations, a rotor blade, and a rotor

#35

20110185725

2011-08-04

Connecting device, driving device and charging device

#36

20110173973

2011-07-21

TURBINE INLET FLOW MODULATOR

#37

20110150374

2011-06-23

Horizontally and vertically adjustable bearing

#38

20110146051

2011-06-23

Method of mounting a heat exchanger in a gas turbine engine assembly

#39

20110135451

2011-06-09

Gas turbine

#40

20110038742

2011-02-17

Turbine, in particular for an exhaust gas turbocharger, and exhaust gas turbocharger

#41

20100314194

2010-12-16

Trailing edge for an aircraft engine, of the type with moving chevrons

#42

20100196146

2010-08-05

Turbocharger with variable turbine geometry

#43

20100193628

2010-08-05

Continuous composite fan duct and thrust reverser

#44

20100107599

2010-05-06

Thrust reverser for a jet engine

#45

20100104431

2010-04-29

Combined axial and transverse constraint and alignment system and method for rotary machines

#46

20100058769

2010-03-11

Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system

#47

20090288389

2009-11-26

Integral thrust vector and roll control system

#48

20050120702

2005-06-09

Two-axis thrust vectoring nozzle

#49

20050069406

2005-03-31

Method and apparatus for turbomachine active clearance control