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R. A. Newley – One of the best experts on this subject based on the ideXlab platform.

  • Polymer composite applications to Aerospace Equipment
    Composites Manufacturing, 1994
    Co-Authors: R. F J Mccarthy, George H. Haines, R. A. Newley

    Abstract:

    This paper describes Dowty’s experience in the composite technology areas of designing in composites, materials development, manufacturing using the resin transfer moulding process, quality assurance and certification which has underpinned the highly successful application of composites in advanced propeller blades. Additional design considerations which must be satisfied to extend the use of composites in other product areas such as multiaxial loading on structural components in landing gear are also addressed. ?? 1994.

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R. F J Mccarthy – One of the best experts on this subject based on the ideXlab platform.

  • Polymer composite applications to Aerospace Equipment
    Composites Manufacturing, 1994
    Co-Authors: R. F J Mccarthy, George H. Haines, R. A. Newley

    Abstract:

    This paper describes Dowty’s experience in the composite technology areas of designing in composites, materials development, manufacturing using the resin transfer moulding process, quality assurance and certification which has underpinned the highly successful application of composites in advanced propeller blades. Additional design considerations which must be satisfied to extend the use of composites in other product areas such as multiaxial loading on structural components in landing gear are also addressed. ?? 1994.

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S. A. Chernyavsky – One of the best experts on this subject based on the ideXlab platform.

  • Optimum Design of Erosion-Stable Heatshield Composite Materials
    Applied Composite Materials, 1997
    Co-Authors: Yu. I. Dimitrienko, G. A. Efremov, S. A. Chernyavsky

    Abstract:

    The present paper describes the development of multilayered heatshield composite materials. These methods permit us to design an optimum composition of heatshield composite materials for Aerospace Equipment under different heat and mechanical influences.

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  • Optimum design of erosion-stable heatshield composite materials
    Applied Composite Materials, 1997
    Co-Authors: Yu. I. Dimitrienko, G. A. Efremov, S. A. Chernyavsky

    Abstract:

    The present paper describes the development of multilayered heatshield composite materials. These methods permit us to design an optimum composition of heatshield composite materials for Aerospace Equipment under different heat and mechanical influences. In accordance with the theory developed, an erosion-stable heatshield three-layered composite material was synthesized, consisting of the upper erosion-stable layer based on the fabric reinforcing filler, the middle high-temperature heatshield layer and the lower low-temperature heatshield layer. Thicknesses of the layers and compositions of the fillers are selected by the methods of optimum design. Specimens were manufactured and gas-dynamical testing was conducted on an erosion-stable composite revealing its very suitable properties and verifing the adequacy of the model developed for the optimum design of heatshield composites.

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