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DEVELOPMENT OF DESIGN METHODS OF GASKETS WITH SHELL MEMBER FOR AIRCRAFT ENGINES

By Alexey Mitrofanovich Dolotov

Abstract

There the purposes are to develop the methods of design and choice of rational sizes of shell members under the conditions of impact loading, to control the energy of collisions, to develop the outlook gasket constructions. The design methodology of gaskets with the shell member with regard to the necessary life, of driving gears for them has been developed. The choice procedure of rational sizes of shell members has been developed; the new constructions of sealing joints with the shell member, the new constructions of driving gears for the valve gaskets with the shell member have been offered. The introduction efficiencies are the decrease of force to seal, the increase of sealing reliability, the reduction of dimensions and mass. The application fields are the aircraft engines, the pneumohydraulic apparatus of aircraft, of chemical, oil and gas productionsAvailable from VNTIC / VNTIC - Scientific & Technical Information Centre of RussiaSIGLERURussian Federatio

Topics: 13E - Couplings, fittings, fasteners, joints, 01C - Aircraft, aircraft components, MECHANICAL ENGINEERING
Year: 1995
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Provided by: OpenGrey Repository
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