Flexible gas turbine operation requires adapted hot gas parts design and lifetime assessment methods. The High Temperature Cyclic Test Rig (HTCTR) is developed to cyclically test internally cooled components from combustor and turbine sections of gas turbines in close-to-engine conditions for a wide range of operating conditions in order to improve component lifetime management. These advanced tests should serve as basis for new model development and validation for conditions that are more representative of those in an engine than the standard material specimen tests
The problem of calculating turbine engine component durability is addressed. Nonlinear, finite-eleme...
Phase I of the Hyperbaric Advanced Hot Section Materials & Coating Test Rig Program has been success...
The requirements to reduce engine fuel burn costs and gaseous emissions combine to ensure that gas t...
Flexible gas turbine operation requires adapted hot gas parts design and lifetime assessment methods...
TutorialThe main driver to define the time between overhauls of a gas turbine is the life of the hot...
LecturePg. 23-32Traditional service and maintenance contracts are evolving to new form of relationsh...
The major technology areas needed to perform a life prediction of an aircraft turbine engine hot sec...
The Institute of Test and Simulation for Gas Turbines develops digital twins and simulation models t...
The Thermochemical Power Group (TPG) of the University of Genoa, Italy, has developed a new flexible...
The development of centralized heat supply for large cities requires the estimation of the individua...
In this thesis a test rig for blade life assessment has been designed. The test article is a blade f...
The paper presents the design and prototyping of a gas generator system for turbocharger experimenta...
The first two years of a two-phase program aimed at improving the high temperature crack initiation ...
In this thesis it was designed a test rig for the life assessment of DS gas turbine blade (first sta...
Abstract- A fast growing amount of renewable energy from wind or solar plants with their inherent pr...
The problem of calculating turbine engine component durability is addressed. Nonlinear, finite-eleme...
Phase I of the Hyperbaric Advanced Hot Section Materials & Coating Test Rig Program has been success...
The requirements to reduce engine fuel burn costs and gaseous emissions combine to ensure that gas t...
Flexible gas turbine operation requires adapted hot gas parts design and lifetime assessment methods...
TutorialThe main driver to define the time between overhauls of a gas turbine is the life of the hot...
LecturePg. 23-32Traditional service and maintenance contracts are evolving to new form of relationsh...
The major technology areas needed to perform a life prediction of an aircraft turbine engine hot sec...
The Institute of Test and Simulation for Gas Turbines develops digital twins and simulation models t...
The Thermochemical Power Group (TPG) of the University of Genoa, Italy, has developed a new flexible...
The development of centralized heat supply for large cities requires the estimation of the individua...
In this thesis a test rig for blade life assessment has been designed. The test article is a blade f...
The paper presents the design and prototyping of a gas generator system for turbocharger experimenta...
The first two years of a two-phase program aimed at improving the high temperature crack initiation ...
In this thesis it was designed a test rig for the life assessment of DS gas turbine blade (first sta...
Abstract- A fast growing amount of renewable energy from wind or solar plants with their inherent pr...
The problem of calculating turbine engine component durability is addressed. Nonlinear, finite-eleme...
Phase I of the Hyperbaric Advanced Hot Section Materials & Coating Test Rig Program has been success...
The requirements to reduce engine fuel burn costs and gaseous emissions combine to ensure that gas t...