Orbital Research, Inc., developed, built, and tested three high-temperature components for use in the design of a data concentrator module in distributed turbine engine control. The concentrator receives analog and digital signals related to turbine engine control and communicates with a full authority digital engine control (FADEC) or high-level command processor. This data concentrator follows the Distributed Engine Controls Working Group (DECWG) roadmap for turbine engine distributed controls communication development that operates at temperatures at least up to 225 C. In Phase I, Orbital Research developed detailed specifications for each component needed for the system and defined the total system specifications. This entailed a combin...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
System studies have shown the benefits of reducing blade tip clearances in modern turbine engines. M...
Distributed engine control (DEC) systems alter aircraft engine design constraints be- cause of funda...
This paper covers the development of a distributed high temperature electronics demonstrator for int...
The presentation describes the challenges facing the turbine engine control system. These challenges...
Gas turbine engines for aero-propulsion systems are found to be highly optimized machines after over...
Turbine engine control technology is poised to make the first revolutionary leap forward since the a...
The performance of propulsion engine systems is sensitive to weight and volume considerations. This ...
This presentation provides an overview of the work performed at NASA Glenn Research Center in distri...
A new test facility is being constructed for developing turbine-cooling and combustor technology for...
There is a growing desire to install electronic power and control systems in high temperature harsh ...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
The Hot Section Technology (HOST) Project is a NASA-sponsored endeavor to improve the durability of ...
NASA's vision for an intelligent engine will be realized with the development of a truly distributed...
This paper presents an extreme environment capable Distributed Motor Controller (DMC) module suitabl...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
System studies have shown the benefits of reducing blade tip clearances in modern turbine engines. M...
Distributed engine control (DEC) systems alter aircraft engine design constraints be- cause of funda...
This paper covers the development of a distributed high temperature electronics demonstrator for int...
The presentation describes the challenges facing the turbine engine control system. These challenges...
Gas turbine engines for aero-propulsion systems are found to be highly optimized machines after over...
Turbine engine control technology is poised to make the first revolutionary leap forward since the a...
The performance of propulsion engine systems is sensitive to weight and volume considerations. This ...
This presentation provides an overview of the work performed at NASA Glenn Research Center in distri...
A new test facility is being constructed for developing turbine-cooling and combustor technology for...
There is a growing desire to install electronic power and control systems in high temperature harsh ...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
The Hot Section Technology (HOST) Project is a NASA-sponsored endeavor to improve the durability of ...
NASA's vision for an intelligent engine will be realized with the development of a truly distributed...
This paper presents an extreme environment capable Distributed Motor Controller (DMC) module suitabl...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
System studies have shown the benefits of reducing blade tip clearances in modern turbine engines. M...
Distributed engine control (DEC) systems alter aircraft engine design constraints be- cause of funda...