An ever increasing number of actuation functions historically performed by hydraulics or pneumatics are being accomplished by electric actuation. If 'end to end' systems are considered, electric actuators (EA's) are potentially lighter and more efficient. In general, system redundancies may be more easily implemented and operationally monitored. Typically, electrical components exhibit longer mean times to failure and projected lifetime costs of EA's are potentially much lower than those of other options. EA's have certain characteristics which must be considered in their application. The actual mechanical loadings must be established, for the more easily controlled EA may be operated much closer to its full capabilities. At higher rates of...
Since the late 70's, several research and development projects deal with future Power-by-Wire-techno...
International audienceThis paper deals with safety-critical, high-power actuation in aerospace appli...
At present, actuation systems for the Thrust Vector Control (TVC) for launch vehicles are hydraulic ...
The power to move aircraft control surfaces has advanced from being manually generated (by the pilot...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
The more electric aircraft concept aims to improve the fuel consumption, the weight and both the mai...
Transportation represents a 20% of green-house effect gases emissions worldwide. There is a trend t...
During the last two decades, the aerospace industry has experienced a significant research boom in t...
An electro-hydrostatic actuator was evaluated at NASA Dryden Flight Research Center, Edwards, Califo...
This chapter presents the motivations behind the more electric aircraft initiative, with a focus on ...
An electromechanical actuator was developed that will follow a proportional control command with min...
A long‐term goal for general aviation aircraft is to reduce or eliminate the use of fluid power syst...
Electromechanical actuators are gaining interest in the aerospace industry within the More Electrica...
Aerospace electromechanical actuators utilizing induction motors are under development in sizes up t...
Since the late 70's, several research and development projects deal with future Power-by-Wire-techno...
International audienceThis paper deals with safety-critical, high-power actuation in aerospace appli...
At present, actuation systems for the Thrust Vector Control (TVC) for launch vehicles are hydraulic ...
The power to move aircraft control surfaces has advanced from being manually generated (by the pilot...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
The more electric aircraft concept aims to improve the fuel consumption, the weight and both the mai...
Transportation represents a 20% of green-house effect gases emissions worldwide. There is a trend t...
During the last two decades, the aerospace industry has experienced a significant research boom in t...
An electro-hydrostatic actuator was evaluated at NASA Dryden Flight Research Center, Edwards, Califo...
This chapter presents the motivations behind the more electric aircraft initiative, with a focus on ...
An electromechanical actuator was developed that will follow a proportional control command with min...
A long‐term goal for general aviation aircraft is to reduce or eliminate the use of fluid power syst...
Electromechanical actuators are gaining interest in the aerospace industry within the More Electrica...
Aerospace electromechanical actuators utilizing induction motors are under development in sizes up t...
Since the late 70's, several research and development projects deal with future Power-by-Wire-techno...
International audienceThis paper deals with safety-critical, high-power actuation in aerospace appli...
At present, actuation systems for the Thrust Vector Control (TVC) for launch vehicles are hydraulic ...