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Aerospace Instrument-Making

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ACCOUNTING REQUIREMENTS FOR THE DESIGN SURVIVABILITY OF SHELL STRUCTURES AIRCRAFT
V.S. Safronov

High cost, complexity of developing aircraft necessitate the use of such design techniques that would allow a greater or lesser extent taken into account quantitatively and are interrelated main factors that determine the effectiveness of the developed aircraft. These factors include not only the flight technical and technological characteristics, complexity of production, flue technology, consumption of materials, cost of production, affecting the overall economic efficiency, but also the vitality of the design of the machine. Under the survivability design we mean the ability of the unit after receiving the calculated maximum – damage tolerance to continue the job or return to home base with less (specified in the formation of the requirements for survivability design) overloads. The paper presents a model and algorithm of optimal design of shell structures of various structural and power circuits of the aircraft taking into account the basic requirements of survivability design based on an analytical assessment of the bearing capacity, the results of the design.
Key words: shells, survivability of a design, optimum designing, analytical model.

Contacts: E-mail: v.s.safronov@mail.ru

Pp. 17-25.

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