Presentation is loading. Please wait.

Presentation is loading. Please wait.

1 Beriev aircraft company Light multirole amphibian aircraft Be-103 Be-103 while running at full speed at taking-off water.

Similar presentations


Presentation on theme: "1 Beriev aircraft company Light multirole amphibian aircraft Be-103 Be-103 while running at full speed at taking-off water."— Presentation transcript:

1 1 Beriev aircraft company Light multirole amphibian aircraft Be-103 Be-103 while running at full speed at taking-off water

2 2 Fuel tanks allocation at Be-103 amphibian Beriev aircraft company

3 3 Appearance

4 4 Flight performance Beriev aircraft company

5 5 Patent

6 6 Sial (glare) Beriev aircraft company

7 7 Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Beriev aircraft company CharacteristicsVersion 1Version 2Version 3Version 4 Aluminum Alloy 2024T3 Alloy Lithium Percentage Elastic tensile modulus, GPa ,5 Compression tensile, GPa ,5 Density (d, kg/m 3 ) Tensile ultimate strength, MPa

8 8 Comparative characteristics of Light-resistant Polymeric Materials Structure and Properties Beriev aircraft company CharacteristicsVersion 1Version 2Version 3Version 4 Glass-fiber Cloth Roving Base: Threads density (thread/cm) Glass fibers: diameter (mm) ,5 Ultimate strength MPa Elastic tensile modulus, GPa ,5 Density (d, kg/m 3 ) Weft: fusion temperature (ºC) Threads density (thread/cm) 456- Bonding Material: Hardening Temperature (ºC)

9 9 Mechanical and physical properties of the new designed material Beriev aircraft company Characteristics Version 1Version 2Version 3Version 4 Tensile ultimate strength, MPa Elastic tensile modulus, GPa Elastic pressure modulus, GPa727375,568 Density (d, kg/m 3 ) Fatigue crack extension rate (dI/dN, mcm/cycle at ΔK = 1 0,080,09 0,1

10 10 ТАНТК им. Г.М. Бердиева 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 1.8T10) 0,80,5 Melting of external layer. Size of destroyed zone 8-13 mm. No specimens are deformed SIAL 2/1 – 2 th. (1441+KMKS 1.8T10) 0,5 Melting of external layer. Size of melted zone 12 mm. Specimen is deformed at discharge filament contact Shet 1441 – 2th.2,5 Cissing, paint charring on the reverse of the panel S=60mm² Shet ST-69N – 2th. 0,56 Through-thickness charring of sheet at discharge contact, sheet delaminating (1200 mm²)

11 11


Download ppt "1 Beriev aircraft company Light multirole amphibian aircraft Be-103 Be-103 while running at full speed at taking-off water."

Similar presentations


Ads by Google