| 1. | Actuateurs et senseurs électro-actifs - Offre technologique Onera |
| | Electro Active Actuators and Sensors... Composite frame for amplified elliptic actuator (Cedrat Technologies) Laminar actuator developed by LMP... Amplified actuators, PZT stacks, PZT ribbons, active composites / materials, light or thin actuators.... Large stroke and high forces - compact, light and powerful actuators with a high bandwidth.... |
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| 2. | Office National d'Études et de Recherches Aérospatiales |
| | Discussion of some issues concerning high fidelity simulations (DNS / LES / DES) applied to flow control Here, high fidelity simulations means " accurate " modeling turbulence Do we need a (high fidelity) realistic modelling of the actuator ?... Are these expensive simulations really necessary for flow control (Is URANS good enough ?) Additional constraints brought by actuators in simulations... |
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| 3. | Electro Active Actuators and Sensors - Onera's Technological Offer |
| | Electro Active Actuators and Sensors - Onera's Technological OfferWho are we ?Technology Transfer... Electro Active Actuators and Sensors. Applications. Composite frame for amplified elliptic actuator (Cedrat Technologies) Laminar actuator developed by LMP. Aeronautics & Space. Keywords... Amplified actuators, PZT stacks, PZT ribbons, active composites / materials, light or thin actuators.. |
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| 4. | Successful test campaign on the VASCO demonstrator - January 2007 - Onera |
| | It was equipped with 13 actuators, i.e. piezo-electric contacts, one in the center and the others arranged around it, and excited mechanically.... In addition, we implemented what is known as MIMO (Multi Input Multi Output), a solution where each sensor can interact with all of the actuators ", they specified at Onera.... |
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| 5. | Experimental validation of a flap actuator for helicopter blades - ONERA / DADS-EN |
| | Experimental validation of a flap actuator for helicopter blades - ONERA / DADS-EN... Experimental validation of a flap actuator for helicopter blades... A full scale adaptable flap actuator model was made by Onera (figures 1 and 2). It includes a standard actuator based on using prestressed piezoelectric stacks.... |
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| 6. | PUMA Project - Plasmas For Aerodynamics Flow Control - Onera |
| | The ionic wind generated and the electric properties of several Dielectric Barrier Discharge (DBD) or Corona Discharge (CD) type surface actuators were characterized with and without a flow.... A jet type actuator called the " Plasma Synthetic Jet " (PSJ) was defined, developed and characterized with and without a flow.... |
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| 7. | The Homer test bench - The deformable mirrors - ONERA / DOTA-EN |
| | Number of actuators for DM1... 52 in the pupil+a ring of guard actuators... Number of actuators for DM2... Mechanical coupling between 2 actuators for DM1... Mechanical coupling between 2 actuators for DM2... Figure 4 shows the influence functions of DM2. Deformations are generated on the activation of each actuator.... |
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| 8. | Active Control Principles - ONERA / DADS |
| | When applied to a structure, instead of creating an antinoise wave, the principle consists of locating vibration sensors on the structure or in the outside space and actuators capable of creating vibrations in the structure to achieve the minimization objective.... The sensors and actuators are coupled with an electronic control system, either an analog system or a digital computer, which calculates the signal to be applied to the actuators in real time.... |
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| 9. | No title |
| | The demonstrator equipped with the actuators... 6 actuators were manufactured and installed :... For excitation in the Z direction, only the vertical actuators are used.... In this configuration, the acceleration levels in the Z direction reach several g. The implementation of the active control with all 6 actuators operating reduces the peak levels, as the broadband contributions.... |
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| 10. | Microsoft Word - OneraPaper2006 29-01-06 doc |
| | Pulsed Plasma Actuators for Separation Flow Control... An experimental investigation of separation control using steady and pulsed plasma actuators was carried out on an Eppler E338 airfoil at typical micro air vehicle Reynolds numbers (20, 000Re140, 000). Pulsing was achieved by modulating the high frequency plasma excitation voltage.... |
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