Les ressources de pouvoir et l’influence sur les politiques publiques : le cas des associations patronales de l’industrie aérospatiale au Québec.

Cette recherche vise à mieux comprendre la mobilisation des ressources de pouvoir, par les associations patronales, dans le but d’influencer les politiques publiques, plus précisément dans le secteur de l’aérospatiale. Dans un premier temps, cette recherche tente de répondre à notre première question de recherche qui s’attarde à l’impact de la logique de représentation sur la détermination du champ d’intervention en matière de politiques publiques. Dans un deuxième temps, notre seconde question de recherche tente de cerner comment les associations patronales utilisent leurs ressources de pouvoir dans le but d’influencer les politiques publiques. D’un angle théorique, cette recherche s’inscrit dans le courant des travaux néo-institutionnalistes. Tout d’abord, les associations patronales sont perçues comme étant des «entrepreneurs institutionnels» capables d’influencer leur environnement institutionnel (Campbell, 2004 ; Streeck et Thelen, 2005 ; Crouch, 2005). Plus précisément, nous constatons également que les employeurs et leurs associations sont en mesure de mobiliser plusieurs leviers de pouvoir pour influencer, à leur avantage, les développements politiques et économiques des sociétés capitalistes (Traxler et Huemer, 2007). D’un angle empirique, notre recherche vise trois objectifs : cerner les logiques de représentation des associations patronales; identifier quels types de ressources sont à la disposition des associations patronales; analyser comment s’exerce le lien entre les ressources de pouvoir (internes et externes) et l’influence potentielle sur les politiques publiques (commerciales et du travail). Afin de rencontrer nos objectifs de recherche, nous avons utilisé la technique de l’étude de cas. Cette méthode qualitative est l’un des meilleurs moyens pour analyser un phénomène inconnu car elle fournit des données en profondeur. Cette recherche suit les recommandations de Merriem (1998) qui propose de mener la recherche en trois grandes étapes : la préparation, la collecte des données et l’interprétation. Nous avons recueilli nos données à l’aide d’entrevues semi-dirigées, conduites à l’hiver 2012. Ces entrevues ont été menées auprès de représentants des associations patronales du secteur de l’aérospatiale. Nous avons effectué une analyse qualitative des données en fonction de notre revue de littérature et nos propositions de recherche. Dans cette perspective, nous avons utilisé la technique de l’appariement logique de Yin (1994) qui consistait à comparer nos observations avec nos propositions de recherche. Enfin, il faut mentionner que cette méthode de recherche (étude de cas) comporte une importante limite de recherche : la généralisation. Effectivement, nous pouvons difficilement généraliser les résultats de notre recherche à une autre population, considérant les nombreuses particularités du secteur de l’aérospatiale. Toutefois, cette recherche a tout de même contribué à enrichir les connaissances sur l’acteur patronal organisé au Canada.

Lean Enterprise Transformation: Measuring and Accelerating the transition to lean.

PowerPoint presentation that showcases: • Research Objectives • Strategic Value of the Lean Enterprise • Multi-Stakeholder Value Optimization • Lean Enterprise Self-Assessment Tool (LESAT) • Leading and Lagging Indicators of Lean Enterprise Transformation • Empirical Results in the Aerospace Industry • Accelerating the Lean Transformation - Linking LESAT to Strategic Objectives • Summary and Questions

Summary of Inventory Pilot Project March 1993 - December 1994

The Lean Aircraft Initiative began in the summer of 1992 as a “quick look” into the feasibility of applying manufacturing principles that had been pioneered in the automobile industry, most notably the Toyota Production System, to the U.S. defense aircraft industry. Once it was established that “lean principles” (the term coined to describe the new paradigm in automobile manufacturing) were indeed applicable to aircraft manufacturing as well, the Initiative was broadened to include other segments of the defense aerospace industry. These consisted of electronics/avionics, engines, electro-mechanical systems, missiles, and space systems manufacturers. In early 1993, a formal framework was established in which 21 defense firms and the Air Force formed a consortium to support and participate in the Initiative at M.I.T.

Summary of Research Conducted by the Manufacturing Systems Team 1994-2002

The Manufacturing Systems team was one of the research teams within the Lean Aerospace Initiative (LAI) whose goal was to document, analyze and communicate the design attributes and relationships that lead to significant performance improvements in manufacturing systems in the defense aerospace industry. This report will provide an integrated record of this research using the Production Operations Transition to Lean Roadmap as its organizing framework.

Lean Transition of Emerging Industrial Capability (LeanTEC)

Lean Transition of Emerging Industrial Capability (LeanTEC) program was a cooperative agreement between the Boeing Company and AFRL conducted from January 1998 to January 2002. The results of this program are documented in the Manual for Effective Technology Transition Processes included as an attachment to this report. This manual provides processes, procedures, and tools for greatly improving technology transition in the aerospace industry. Methodology for the implementation of these improvements is given along with methods for customizing the various processes, procedures, and tools for a given company or business unit. The indicated methodology was tested by the LeanTEC team and results are documented in the report.

Simulation of interlaminar and intralaminar damage in polymer-based composites for aeronautical applications under impact loading

La aplicación de materiales compuestos de matriz polimérica reforzados mediante fibras largas (FRP, Fiber Reinforced Plastic), está en gradual crecimiento debido a las buenas propiedades específicas y a la flexibilidad en el diseño. Uno de los mayores consumidores es la industria aeroespacial, dado que la aplicación de estos materiales tiene claros beneficios económicos y medioambientales. Cuando los materiales compuestos se aplican en componentes estructurales, se inicia un programa de diseño donde se combinan ensayos reales y técnicas de análisis. El desarrollo de herramientas de análisis fiables que permiten comprender el comportamiento mecánico de la estructura, así como reemplazar muchos, pero no todos, los ensayos reales, es de claro interés. Susceptibilidad al daño debido a cargas de impacto fuera del plano es uno de los aspectos de más importancia que se tienen en cuenta durante el proceso de diseño de estructuras de material compuesto. La falta de conocimiento de los efectos del impacto en estas estructuras es un factor que limita el uso de estos materiales. Por lo tanto, el desarrollo de modelos de ensayo virtual mecánico para analizar la resistencia a impacto de una estructura es de gran interés, pero aún más, la predicción de la resistencia residual después del impacto. En este sentido, el presente trabajo abarca un amplio rango de análisis de eventos de impacto a baja velocidad en placas laminadas de material compuesto, monolíticas, planas, rectangulares, y con secuencias de apilamiento convencionales. Teniendo en cuenta que el principal objetivo del presente trabajo es la predicción de la resistencia residual a compresión, diferentes tareas se llevan a cabo para favorecer el adecuado análisis del problema. Los temas que se desarrollan son: la descripción analítica del impacto, el diseño y la realización de un plan de ensayos experimentales, la formulación e implementación de modelos constitutivos para la descripción del comportamiento del material, y el desarrollo de ensayos virtuales basados en modelos de elementos finitos en los que se usan los modelos constitutivos implementados.

Gestão de parcerias na administração pública: uma experiência no setor de telecomunicações

O tema parceria vem sendo objeto de estudo em todo o mundo. Ganhando força, com as Joint-venture Internacionais, nas áreas de telecomunicações, informática, automobilística, aeroespacial etc., o elemento inovador passou a ser a constituição de alianças estratégicas com potenciais concorrentes, seja na exploração de novos nichos de mercado, seja em atividades de pesquisa e desenvolvimento de novos serviços e produtos. Considerando como normal esta troca ou sinergia entre parceiros, o trabalho apresenta e analisa os dados relativos ao estudo de campo realizado (pesquisa seletiva) junto a profissionais envolvidos com o dia-a-dia do processo de parceria de empresas líderes dos setores de Telecomunicações (Empresa Estatal) e do setor de serviços de Rede e Informática ( Empresa Privada). As considerações estão estruturadas nas seguintes partes: a caracterização e segmentação da amostra utilizada (caracterização dos respondentes); a análise descritiva e avaliação das variáveis representativas dos fatores inibidores e facilitadores; as percepções diferenciadas face aos elementos dependendo da experiência profissional e grau de envolvimento com os processos da parceria; os elementos inibidores e facilitadores apontados como de maior relevância; e os resultados obtidos a partir do uso da técnica de análise fatorial.

Biased Atmospheric, Sub-Atmospheric, and Low-Pressure Air Plasmas for Material Surface Improvements

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Análise do efeito higrotérmico no comportamento em fadiga de compósitos de PPS/fibras de carbono

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Evaluation of fatigue behavior on repaired carbon fiber/epoxy composites

The continuous use of structural polymer composites in aeronautical industry has required the development of repairing techniques of damages found in different types of laminates. The most usually adopted procedure to investigate the repair of composite laminates has been by repairing damages simulated in laminated composite specimens. This work shows the influence of structural repair technique on mechanical properties of a typical carbon fiber/epoxy laminate used in aerospace industry. When analyzed by tensile test, the laminates with and without repair present tensile strength values of 670 and 892 MPa, respectively, and tensile modulus of 53.0 and 67.2 GPa, respectively. By this result, it is possible to observe a decrease of the measured mechanical properties of the repaired composites. When submitted to fatigue test, it is observed that in loads higher than 250 MPa, this laminate presents a low life cycle (lower than 400,000 cycles). The fatigue performance of both laminates is comparable, but the non-repaired laminate presented higher tensile and fatigue resistance when compared with the repaired laminate.

Análise crítica do processo de auditoria de sistema de gestão da qualidade no setor aeroespacial

A auditoria de sistema de gestão da qualidade é utilizada pelas organizações para melhorar o seu desempenho por meio de avaliações sistemáticas dos processos. Ao mesmo tempo, a atividade de auditoria vem sendo questionada quanto à sua capacidade de promover essa melhoria. Diante deste cenário, este artigo objetiva analisar fatores que afetam o processo de auditoria de certificação do sistema de gestão da qualidade, de modo a indicar oportunidades de melhoria das auditorias. A pesquisa é delimitada a auditorias no setor aeroespacial, que são orientadas pela NBR 15100. Foi realizada uma survey com auditores experientes nos anos de 2009 e 2010. São identificados fatores como comunicação, seleção da equipe, conhecimento do setor e os resultados mostram a existência de discrepâncias consideráveis entre o nível de importância e de aplicação desses fatores nas organizações auditadas.

Avaliação da resistência ao desgaste de aços inoxidáveis endurecíveis por precipitação nitretados

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

Investigation of the corrosion behaviour of AA 2024-T3 in low concentrated chloride media

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Active flutter suppression in a 2-D airfoil using linear matrix inequalities techniques

Flutter is an in-flight vibration of flexible structures caused by energy in the airstream absorbed by the lifting surface. This aeroelastic phenomenon is a problem of considerable interest in the aeronautic industry, because flutter is a potentially destructive instability resulting from an interaction between aerodynamic, inertial, and elastic forces. To overcome this effect, it is possible to use passive or active methodologies, but passive control adds mass to the structure and it is, therefore, undesirable. Thus, in this paper, the goal is to use linear matrix inequalities (LMIs) techniques to design an active state-feedback control to suppress flutter. Due to unmeasurable aerodynamic-lag states, one needs to use a dynamic observer. So, LMIs also were applied to design a state-estimator. The simulated model, consists of a classical flat plate in a two-dimensional flow. Two regulators were designed, the first one is a non-robust design for parametric variation and the second one is a robust control design, both designed by using LMIs. The parametric uncertainties are modeled through polytopic uncertainties. The paper concludes with numerical simulations for each controller. The open-loop and closed-loop responses are also compared and the results show the flutter suppression. The perfomance for both controllers are compared and discussed. Copyright © 2006 by ABCM.

The role of coarse intermetallics in the localized corrosion behaviour of AA 2024-T3 in low concentrated chloride media

Aluminium alloy (AA) 2024-T3 is an important engineering material due to its widespread use in the aerospace industry. However, it is very prone to localized corrosion attack in chloride containing media, which has been mainly associated to the presence of coarse intermetallics (IMs). In this work the corrosion behaviour of aluminium alloy 2024-T3 in low concentrated chloride media was investigated using microscopy and electrochemical methods. SEM observations have shown that intermetallics with the same nominal composition present heterogeneous reaction rates, and that both types of coarse IMs normally found in the AA 2024-T3 microstructure corrode. Moreover, EDS analyses have shown important compositional changes in the corroded IMs, evidencing the selective corrosion of their more active constituents and the onset of an intense oxygen peak, irrespective to the IM nature. TEM/EDS observations on non-corroded samples have evidenced the heterogeneous composition within the IMs. On the other hand, the results of the electrochemical investigations, in accordance with the SEM/EDS observations, have evidenced that IMs corrosion dominates the electrochemical response of the alloy during the first hours of immersion in the test electrolyte. © 2009 by NACE International.