FORMATION OF MASS CONSTRUCTION ELEMENTS HELICOPTER
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FORMATION OF MASS CONSTRUCTION ELEMENTS HELICOPTER

FORMATION OF MASS CONSTRUCTION ELEMENTS HELICOPTER

One of the main tasks is to design units meet the requirements of strength, aerodynamics, technology and operation of the helicopter.

Consider the basic methods of minimizing the weight of the power units design, providing static strength. For optimum test weight, with respect to static strength is taken equal to Strength designs.

Effective and practical way to create a structure approaching full-strength, the design is an understatement to load (0,9 the calculated) and the subsequent testing of the design to full load and hardening of the individual structural elements destroyed. Designer, consciously or unconsciously seeks to improve the reliability of more than minimizing the structural mass. Oversize square cross-sections takes place internally using standard profiles and standardized parts.

A very efficient to re-design method, i.e., partial revision already developed set of drawings in order to facilitate construction. Source for its justification are the following considerations: virtually any design when re-elaboration can be facilitated without radical changes it; in the design process is a periodic update of existing loads and safety margins based purging and laboratory tests and specified by various structural connection; relief may be carried out by increasing the depth of the design study.

Components for equipment

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