Influence of support edge stiffness on the stress-strain state of shallow shells

1988 ◽  
Vol 24 (1) ◽  
pp. 52-56
Author(s):  
R. I. Nikulina ◽  
V. V. Zhitkov
Keyword(s):  
Strain State ◽  
Stress Strain ◽  
Shallow Shells ◽  
Stress Strain State ◽  
Edge Stiffness

Two-Layer Ferrocement Shells Stress-Strain State Modeling under the Fire Conditions

2019 ◽  
Vol 974 ◽  
pp. 515-520
Author(s):  
A.V. Zhurtov ◽  
T.A. Khezhev ◽  
Anton S. Chepurnenko ◽  
Angelica V. Saibel
Keyword(s):  
Strain State ◽  
Physical Nonlinearity ◽  
Strength Calculation ◽  
Stress Strain ◽  
Shallow Shells ◽  
Physicomechanical Characteristics ◽  
Stress Strain State ◽  
Double Curvature ◽  
Fire Conditions

The article deals with the issues of strength calculation of two-layer ferrocement shells under fire conditions, taking into account the physical nonlinearity of the material. The change in the physicomechanical characteristics of materials under the action of temperature is taken into account. The solution of model problems for shallow shells of double curvature is presented.

КОНСТРУКТИВНО-ТЕХНОЛОГІЧНІ ОСОБЛИВОСТІ ХВОСТО-ВИХ БАЛОК СІТЧАСТОГО ТИПУ З ПОЛІМЕРНИХ КОМПО-ЗИЦІЙНИХ МАТЕРІАЛІВ ВЕРТОЛЬОТІВ ТРАНСПОРТНОЇ КАТЕГОРІЇ

2020 ◽  
pp. 15-30
Author(s):  
А. Г. Гребеников ◽  
И. В. Малков ◽  
В. А. Урбанович ◽  
Н. И. Москаленко ◽  
Д. С. Колодийчик
Keyword(s):  
Finite Element ◽  
Strain State ◽  
Layer Structure ◽  
Metal Structure ◽  
Element Model ◽  
Stress Strain ◽  
Element Analysis ◽  
Mesh Structure ◽  
Stress Strain State ◽  
Mesh Structures

The analysis of the design and technological features of the tail boom (ТB) of a helicopter made of polymer composite materials (PCM) is carried out.Three structural and technological concepts are distinguished - semi-monocoque (reinforced metal structure), monocoque (three-layer structure) and mesh-type structure. The high weight and economic efficiency of mesh structures is shown, which allows them to be used in aerospace engineering. The physicomechanical characteristics of the network structures are estimated and their uniqueness is shown. The use of mesh structures can reduce the weight of the product by a factor of two or more.The stress-strain state (SSS) of the proposed tail boom design is determined. The analysis of methods for calculating the characteristics of the total SSS of conical mesh shells is carried out. The design of the tail boom is presented, the design diagram of the tail boom of the transport category rotorcraft is developed. A finite element model was created using the Siemens NX 7.5 system. The calculation of the stress-strain state (SSS) of the HC of the helicopter was carried out on the basis of the developed structural scheme using the Advanced Simulation module of the Siemens NX 7.5 system. The main zones of probable fatigue failure of tail booms are determined. Finite Element Analysis (FEA) provides a theoretical basis for design decisions.Shown is the effect of the type of technological process selected for the production of the tail boom on the strength of the HB structure. The stability of the characteristics of the PCM tail boom largely depends on the extent to which its design is suitable for the use of mechanized and automated production processes.A method for the manufacture of a helicopter tail boom from PCM by the automated winding method is proposed. A variant of computer modeling of the tail boom of a mesh structure made of PCM is shown.The automated winding technology can be recommended for implementation in the design of the composite tail boom of the Mi-2 and Mi-8 helicopters.

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