ClassID:

145565

F05D2260/532 - CPC Classification

Classification description:

Function; Kinematic linkage, i.e. transmission of position using gears of the bevelled or angled type

Recent Application in this class:
#1
20260092565
2026-04-02

Gas Turbine Engine Tower Shaft Assembly

#2
20240084713
2024-03-14

System for controlling discharge doors of a turbomachine

#3
20210087975
2021-03-25

Compact accessory systems for a gas turbine engine

#4
20200256258
2020-08-13

Accessory gearbox for gas turbine engine with compressor drive

#5
20200157969
2020-05-21

Gas turbine

#6
20190368424
2019-12-05

Hybrid amplification of high spool motoring via low spool power extraction and motoring of a differential geared generator

#7
20190242465
2019-08-08

Mechanism for driving blade orientation adjustment bodies

#8
20190186289
2019-06-20

Structure and method to mitigate rotor bow in turbine engine

#9
20190112984
2019-04-18

Compact accessory systems for a gas turbine engine

#10
20180363481
2018-12-20

Variable pitch change control method

#11
20180320591
2018-11-08

Combined two engine cycle with at least one recuperated cycle engine for rotor drive

#12
20180274390
2018-09-27

Bowed rotor prevention system

#13
20180223868
2018-08-09

Turbine Engine Compressor with Variable-Pitch Vanes

#14
20180187770
2018-07-05

Oil quieting direction control baffle

#15
20180058332
2018-03-01

System and apparatus for diversified gearbox

#16
20170284220
2017-10-05

Anti-windmilling system for a gas turbine engine

#17
20170276016
2017-09-28

Idler gear connection for multi-stage variable vane actuation

#18
20170146112
2017-05-25

Gear baffle configured with lubricant outlet passage

#19
20170009660
2017-01-12

Housing for driving an apparatus for a turbine engine

#20
20160201567
2016-07-14

System and apparatus for diversified gearbox

#21
20160138476
2016-05-19

Intermediate casing for turbomachine and accessory gearbox drive assembly

#22
20160131082
2016-05-12

Thrust reverser with hidden linkage blocker doors

#23
20160003144
2016-01-07

Combined two engine cycle with at least one recuperated cycle engine for rotor drive

#24
20140038770
2014-02-06

Generating device for aircraft

#25
20140026589
2014-01-30

Sealing arrangement of accessory to aircraft engine

#26
20130318999
2013-12-05

GAS TURBINE ENGINE WITH A COUNTER ROTATING FAN

#27
20130193688
2013-08-01

Bevel gear arrangement for axial accessory gearbox

#28
20120308362
2012-12-06

Dual input drive AGB for gas turbine engines

#29
15042331
2017-05-30

Bowed rotor prevention system