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Aerospace Instrument-Making

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REPAIR RATIONAL DESIGN OF FLAT STRUCTURE OF THE AIRCRAFT
V.S. Safronov

One of the problems in the design of aircraft structures reusable is to assess the recoverability and maintainability of the damaged structure. Questions develop ways to restore the original strength and stiffness are today highly relevant.
This is explained as follows. Aviation and rocket design due to the relatively high technological complexity, have a high cost. This applies particularly to the honeycomb structure, the volume of which in modern aircraft makes up 40-50% of the mass. In view of this, in order to save material resources
and needs a quick recovery of aircraft and rocket park, great importance is the restoration of the damaged aircraft structures in the military and hospi tals. The paper developed a method of rational design of repair elements of different structures for planar structures aircraft of various structural and
power schemes on the basis of analytical mathematical models to assess their bearing capacity.
Key words: panel, bearing capacity, repair paste, optimal design, analytical model.

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

Pp. 44-48.

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