Abstract: A method and device are discussed for determining quantitative parameters of a bond between two elements, for example an adhesive bond between two aluminium plates of an aircraft. A pulsed wave is provided to a first element. The elements, including the bonded region, act as a waveguide. Any discontinuities, an end of the bonded region or imperfections, result in a change of parameters of the waveguide. This results in reflections. By analysing characteristics of the reflections, along with the actual bond length and a signal expected from a good quality bond, an equivalent bond length may be determined.

Abstract: A method is presented for making a composite material from strips comprising longitudinal fibers and a binder or resin, which material comprises a number of layer assemblies one on top of the other. Each layer assembly comprises m sets (with m at least 2) of parallel strips each extending in a different direction, Each layer assembly is manufactured by successive steps of depositing groups of parallel strips according to a well defined pattern (without longitudinally interweaving strips with previously deposited strips). Before completing a layer assembly, with the exception of the last layer assembly, by depositing its last group of parallel strips, the first group of parallel strips of the following layer assembly is already deposited. A composite material manufactured with such a method is presented too.

Abstract: A method is presented for making a composite material from strips comprising longitudinal fibres and a binder or resin, which material comprises a number of layer assemblies one on top of the other. Each layer assembly comprises m sets (with m at least 2) of parallel strips each extending in a different direction, Each layer assembly is manufactured by successive steps of depositing groups of parallel strips according to a well defined pattern (without longitudinally interweaving strips with previously deposited strips). Before completing a layer assembly, with the exception of the last layer assembly, by depositing its last group of parallel strips, the first group of parallel strips of the following layer assembly is already deposited. A composite material manufactured with such a method is presented too.

Abstract: A method of selecting the optimum mix of resources for achieving an outcome while minimizing risk is presented. In one embodiment, the method is applied to selecting the optimum mix of manufacturing technologies and amount of use of each technology for fabricating a helicopter fuselage structure in order to minimize the recurring cost and keep the risk below a pre-selected value. The method involves selecting a plurality of resources which can be used to achieve the desired outcome. Determining an associated outcome for each resource. Establishing at least one target risk level for the desired outcome. Calculating an associated outcome and risk for a plurality of combinations of the resources at a plurality of percentage applications of each resource. Then determining an optimum mix of resources and percentage of application of each resource which maximizes the outcome while maintaining the risk below the at least one target risk level.

Abstract: A main rotor support structure assembly includes a support housing which transmits loads developed by the main rotor assembly into the airframe. Integral main rotor servo attachment lugs extend from the cylindrical body member to provide lower attachment points for the rotor servo actuators which are operable to articulate a rotor swash plate or the like. The servo attachment lugs are integrally formed as part of the cylindrical body member and spaced thereabout. A substantially L-shaped metallic insert is sandwiched and bonded within each servo attachment lug to resist axial and transverse tension of the rather high forces exerted by the rotor servo actuators.