1. "Beriev Be 103: The Versatile Light Multirole Amphibian Aircraft"


The Be 103 is a light amphibian aircraft manufactured by Beriev Aircraft Company. It is capable of operating on both water and land
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About 1. "Beriev Be 103: The Versatile Light Multirole Amphibian Aircraft"
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Slide11Beriev aircraft company Beriev aircraft company Light multirole amphibian aircraft Be-103 Light multirole amphibian aircraft Be-103 Be-103 while running at full speed at tak ing -off water
Slide22Fuel tanks allocation at Be-103 amphibian Fuel tanks allocation at Be-103 amphibian Beriev aircraft company Beriev aircraft company
Slide33Appearance Appearance Beriev aircraft company Beriev aircraft company
Slide44Flight performance Flight performance Beriev aircraft company Beriev aircraft company
Slide55Patent Patent Beriev aircraft company Beriev aircraft company
Slide66Sial (glare) Sial (glare) Beriev aircraft company Beriev aircraft company
Slide77Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Beriev aircraft company Beriev aircraft company Characteristics Version 1 Version 2 Version 3 Version 4 Aluminum Alloy 2024T3 Alloy Lithium Percentage 1.5 1.7 2.0 - Elastic tensile modulus, GPa 77 79 81 71,5 Compression tensile, GPa 79 81 83 73,5 Density (d, kg/m 3 ) 2600 2590 2580 2780 Tensile ultimate strength, MPa 400 440 460 440
Slide88Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Beriev aircraft company Beriev aircraft company Characteristics Version 1 Version 2 Version 3 Version 4 Glass-fiber Cloth Roving Base : Threads density (thread/cm) 30 25 20 Glass fibers : diameter (mm) 79 81 83 73,5 Ultimate strength MPa 500 470 400 470 Elastic tensile modulus, GPa 85 90 100 85,5 Density (d, kg/m 3 ) 2500 2550 2580 2500 Weft : fusion temperature ( ºC) 150 140 120 - Threads d ensity (thread/cm) 4 5 6 - Bonding Material : Hardening Temperature ( ºC) 180 150 120 120
Slide99Mechanical and physical properties of the new designed material Mechanical and physical properties of the new designed material Beriev aircraft company Beriev aircraft company Characteristics Version 1 Version 2 Version 3 Version 4 Tensile ultimate strength, MPa 870 875 865 850 Elastic tensile modulus, GPa 70 71 73 66 Elastic pressure modulus, GPa 72 73 75,5 68 Density (d, kg/m 3 ) 2350 2380 2340 2500 Fatigue crack extension rate (dI/dN, mcm/cycle at ΔK = 1 0,08 0,09 0,09 0,1
Slide1010ТАНТК им. Г.М. Бердиева ТАНТК им. Г.М. Бердиева Be-103 aircraft integral fuel tanks panels lightning resistance test results Be-103 aircraft integral fuel tanks panels lightning resistance test results Panel Specimen (quantity) Metal thickness 1441 mm Impact results Layer 1 Layer 3 SIAL 2/1 – 2 th. (1441+ KMKS 1.8 T 10) 0,8 0,5 Melting of external layer. Size of destroyed zone 8-13 mm. No specimens are deformed SIAL 2/1 – 2 th. (1441+ KMKS 1.8 T 10) 0, 5 0,5 Melting of external layer. Size of melted zone 12 mm. Specimen is deformed at discharge filament contact Shet 1441 – 2 th . 2,5 Cissing, paint charring on the reverse of the panel S=60mm ² Shet ST -69 N – 2th. 0,56 Through-thickness charring of sheet at discharge contact, sheet delaminating (1200 mm ² )
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