RESUMO
The CBL family of E3 ubiquitin ligases regulates cell signaling in a number of tissues by promoting degradation of tyrosine kinase receptors such as epidermal growth factor receptor. CBLC, the third member of the CBL family, is expressed in epithelial tissues, including the mammary gland. A transgenic mouse strain expressing a tetracyclin-inducible CBLC in the mammary gland was derived. It was found that CBLC transgene expression reduces the number and length of ducts during the development of the gland. In vivo results support the concept of CBLs as negative regulators of cell proliferation. Alternatively, the phenotype may be due to increased apoptosis. This mouse model may be used to further study regulatory components of the CBL pathway and may be crossed with mice susceptible to develop mammary tumors.
Assuntos
Regulação da Expressão Gênica no Desenvolvimento , Glândulas Mamárias Animais/metabolismo , Vírus do Tumor Mamário do Camundongo/genética , Proteínas Proto-Oncogênicas c-cbl/genética , Animais , Proliferação de Células , Epitélio/metabolismo , Genótipo , Glândulas Mamárias Animais/embriologia , Camundongos , Camundongos Transgênicos , Modelos Biológicos , Modelos Genéticos , Fenótipo , Tetraciclina/farmacologia , TransgenesRESUMO
Based on a phenomenological methodology, a three dimensional (3D) thermochemical model was developed to predict the temperature profile, the mass loss and the decomposition front of a carbon-reinforced epoxy composite laminate (T700/M21 composite) exposed to fire conditions. This 3D model takes into account the energy accumulation by the solid material, the anisotropic heat conduction, the thermal decomposition of the material, the gas mass flow into the composite, and the internal pressure. Thermophysical properties defined as temperature dependant properties were characterised using existing as well as innovative methodologies in order to use them as inputs into our physical model. The 3D thermochemical model accurately predicts the measured mass loss and observed decomposition front when the carbon fibre/epoxy composite is directly impacted by a propane flame. In short, the model shows its capability to predict the fire behaviour of a carbon fibre reinforced composite for fire safety engineering.
RESUMO
Thermophysical properties of a carbon-reinforced epoxy composite laminate (T700/M21 composite for aircraft structures) were evaluated using different innovative characterisation methods. Thermogravimetric Analysis (TGA), Simultaneous Thermal analysis (STA), Laser Flash analysis (LFA), and Fourier Transform Infrared (FTIR) analysis were used for measuring the thermal decomposition, the specific heat capacity, the anisotropic thermal conductivity of the composite, the heats of decomposition and the specific heat capacity of released gases. It permits to get input data to feed a three-dimensional (3D) model given the temperature profile and the mass loss obtained during well-defined fire scenarios (model presented in Part II of this paper). The measurements were optimised to get accurate data. The data also permit to create a public database on an aeronautical carbon fibre/epoxy composite for fire safety engineering.