Patents-Review.com
ClassID:

145644 ⎘

F05D2270/095 - CPC Classification

Classification description:

Control; Purpose of the control system to cope with emergencies by temporary overriding set control limits

Recent Application in this class:
#1
20240301835
2024-09-12

Method of controlling a combustor

 #2
20240254929
2024-08-01

DEVICE FOR BLOCKING THE SHUT-OFF OF A PROPULSION ENGINE FOR AIRCRAFT

 #3
20200025109
2020-01-23

Supersonic aircraft turbofan

 #4
20190352001
2019-11-21

PROPULSION SYSTEM FOR A SINGLE-ENGINE HELICOPTER

 #5
20180209347
2018-07-26

Dual inline valve with manual override

 #6
20170211413
2017-07-27

Overspeed protection device of an aircraft engine

 #7
20170101938
2017-04-13

Method for detecting a failure of a first turbine engine of a twin-engine helicopter and for operating the second turbine engine, and corresponding device

 #8
20170081974
2017-03-23

Gas turbine engine uncontrolled high thrust detection system and method

 #9
20160326984
2016-11-10

Thrust reversal for turbofan gas turbine engine

 #10
20120317955
2012-12-20

Surge margin control

 #11
20120109426
2012-05-03

Aircraft power plant, an aircraft, and a method of piloting said aircraft

 #12
20100262350
2010-10-14

Corrected megawatt backup curve methodology

 #13
20100185377
2010-07-22

System and method for starting a gas turbine engine with inoperable exhaust gas turbine temperature sensor

 #14
20100145590
2010-06-10

System and method for lean blowout protection in turbine engines

 #15
20070113563
2007-05-24

Method for lean blowout protection in turbine engines

 #16
20070095070
2007-05-03

Control logic for fuel controls on APUs

 #17
20070051090
2007-03-08

Control logic for fuel controls on APUs

 #18
20060254282
2006-11-16

Control logic for fuel controls on APUs

 #19
20060201132
2006-09-14

Gas turbine control system

 #20
20050204745
2005-09-22

Gas turbine control system