#F02C7/057

LOCKOUT MECHANISM FOR A VALVE ASSEMBLY

An assembly for use with a valve having a valve element disposed within a valve body flow passage, the assembly comprising an actuator (130) and a lockout mechanism configured to maintain the position…

DRIVE·Jan 1·1 min read

F02C7/057 GE AVIATION SYSTEMS LLC [US]

VALVE ASSEMBLY AND LOCKOUT MECHANISM

A valve assembly (100) including a valve body (110) with an inlet port (112) and an outlet port (114), a flow passage (116) and a valve element (120) disposed within the flow passage, an actuator (130…

DRIVE·Dec 6·1 min read

F02C7/057 GE AVIATION SYSTEMS LLC [US]

Method for operating a combustion chamber and combustion chamber

The combustion chamber (5) comprises a body (10) with a fuel supply duct (14) for supplying a fuel (F) into the body (10) and a carrier air supply duct (15) for supplying air (A) into the body (10). I…

DRIVE·Oct 15·1 min read

F02C7/057 ALSTOM TECHNOLOGY LTD [CH]

Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting said method

The invention relates to a method for protecting a gas turbine engine (10), comprising a compressor (11), a combustor (13) and a turbine (12), against high dynamical process values, especially in comb…

DRIVE·Nov 7·2 min read

F02C7/057 ALSTOM TECHNOLOGY LTD [CH]

Methods and systems for modeling turbine operation

Methods and systems for modeling turbine operation are disclosed. In one embodiment a method 200 for modeling turbine operation may include: determining 205 current performance parameters 130 of a tur…

DRIVE·Mar 28·1 min read

F02C7/057 GEN ELECTRIC [US]