Abstract: An assembly for shielding an aircraft from electromagnetic energy may include a window mounting configured to be conductively coupled to an aperture in a fuselage of an aircraft. The window mounting may include a window pane having an electromagnetically-reflective coating for reflecting electromagnetic energy. The window pane may remain electrically isolated from the fuselage prior to the electromagnetic energy exceeding a frequency of approximately 1 GHz. The window mounting may further include a capacitive gasket capacitively coupling the window pane to the fuselage after the frequency of the electromagnetic energy reflected by the window pane exceeds approximately 1 GHz.

Abstract: A hybrid coating composition including an organosilane component, a metal alkoxide component and a surfactant component, with the metal alkoxide component present in the composition at a molar ratio of about 75:1 with respect to the surfactant component. The hybrid coating composition once cured on a transparent substrate has an initial clarity greater than 98. Transparent members are also disclosed that include a transparent substrate having the hybrid coating composition cured on a first major surface thereof.

Abstract: An assembly for shielding an aircraft from electromagnetic energy may include a window mounting configured to be conductively coupled to an aperture in a fuselage of an aircraft. The window mounting may include a window pane having an electromagnetically-reflective coating for reflecting electromagnetic energy. The window pane may remain electrically isolated from the fuselage prior to the electromagnetic energy exceeding a frequency of approximately 1 GHz. The window mounting may further include a capacitive gasket capcaitively coupling the window pane to the fuselage after the frequency of the electromagnetic energy reflected by the window pane exceeds approximately 1 GHz.

Abstract: A system for shielding an aircraft from electromagnetic energy includes a fuselage, aperture, window mounting, and window plug. The fuselage provides an electrically conductive envelope. The aperture is disposed in the fuselage. The window mounting spans the aperture. The window plug spans the aperture. The window mounting and the window plug are electrically coupled to the fuselage and provide an electrical path spanning the aperture.

Abstract: A hybrid coating composition including an organosilane component, a metal alkoxide component and a surfactant component, with the metal alkoxide component present in the composition at a molar ratio of about 75:1 with respect to the surfactant component. The hybrid coating composition once cured on a transparent substrate has an initial clarity greater than 98. Transparent members are also disclosed that include a transparent substrate having the hybrid coating composition cured on a first major surface thereof.

Abstract: A hybrid coating including a mixture of an organosilane component, a metal alkoxide component and a surfactant component. A method for coating a substrate including cleaning a substrate surface, treating the surface with oxygen plasma, applying an adhesion promoter to the surface, then applying a hybrid coating to the surface and curing the hybrid coating. A method for making a hybrid coating includes preparing a mixture comprising an organosilane, a metal alkoxide and a surfactant, heating the mixture; and filtering the mixture.

Abstract: A method for applying an abrasion-resistant coating to a substrate including the steps of generating an atmospheric plasma, introducing a precursor to the atmospheric plasma, the precursor being selected to form the abrasion-resistant coating, and positioning the substrate relative to the atmospheric plasma such that the atmospheric plasma deposits the abrasion-resistant coating onto the substrate.

Abstract: A method for applying an abrasion-resistant coating to a substrate including the steps of generating an atmospheric plasma, introducing a precursor to the atmospheric plasma, the precursor being selected to form the abrasion-resistant coating, and positioning the substrate relative to the atmospheric plasma such that the atmospheric plasma deposits the abrasion-resistant coating onto the substrate.

Abstract: A hybrid coating including a mixture of an organosilane component, a metal alkoxide component and a surfactant component.

Abstract: A system for shielding an aircraft from electromagnetic energy includes a fuselage, aperture, window mounting, and window plug. The fuselage provides an electrically conductive envelope. The aperture is disposed in the fuselage. The window mounting spans the aperture. The window plug spans the aperture. The window mounting and the window plug are electrically coupled to the fuselage and provide an electrical path spanning the aperture.