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

Slides:

Advertisements

Similar presentations

Improved Joint Efficiencies in Aluminum Alloys

Advertisements

Chap.8 Mechanical Behavior of Composite

First EUREKA meeting Тhe activities of the EUREKA project DE_AMATECH in the year PROJECT Development of new actuators, materials and technology.

Euro-Zel th International Symposium Advanced Composite Materials for the Railroad cars Presented by Irina Garustovich Moscow State University of.

Materials for Automobiles CEEN0903 Summer 2011 Classes of Materials Metals Made of metallic elements: Sn, Cu, Fe Ceramics Compounds between metallic.

Experimental methods for material measurements at high strain-rate

ECO-PCCM Second Meeting, Belgrade, 7-8 April Eco-Houses Based on Eco-Friendly Polymer Composite Construction Materials ECO-PCCM ISO 9001:2000 PRODUCTION.

1 Characterization of kenaf/PLA composites ECO-PCCM Fourth Meeting, Sofia, Bulgaria, April 6-7, 2006 PROJECT Eco-Houses Based on Eco-Friendly Polymer Composite.

ME 240: Introduction to Engineering Materials Chapter 8. Failure 8.1 CHAPTER 8.

6-1 Chapter 6 Overview b Four major alloy groups most common: Aluminum, magnesium, zinc and ZA Aluminum, magnesium, zinc and ZA b These alloys have a range.

Manufacturing Technology

High Temperature Composites Rutgers University Federal Aviation Administration Advanced Materials Flammability Atlantic City, NJ October 24, 2001.

Engineering materials lecture #14

Chapter 6: Mechanical Properties

R.Valbuena NBI March 2002 CNGS Decay Pipe Entrance Window Structural and Thermal Analysis A.Benechet, P.Cupial, R.Valbuena CERN-EST-ME.

Identified Company (CompositeX) to manufacture Custom Composite Pressure Vessel ● Working pressure 1000psi ● Holds 8 kg Nitrous Oxide ● 700 cubic inch.

Characterization, applications

Connie King /14/05 Side-Release Buckle. Materials Selection Economical Fatigue resistance Temperature & weather resistance MaterialPPHDPENylon.

EBB 220/3 PRINCIPLE OF VISCO-ELASTICITY

ENGR 225 Section

MECHANICAL PROPERTIES OF MATERIALS

1 lectures accompanying the book: Solid State Physics: An Introduction, by Philip Hofmann (2nd edition 2015, ISBN- 10: , ISBN-13: ,

Fluoropolymers Teflon ® / Tefzel ® are DuPont registered trademarks FH 8 Oct 02 / page 1 TYPICAL PROPERTIES MOLECULAR WEIGHT COMONOMER CONTENT MELTING.

Engineering Practicum Baltimore Polytechnic Institute M. Scott (Pass in Remote Measurement Lab Report) 1.What is the relationship between a)Tensile Strength.

The E.O. Paton Welding Institute 1 NEW TECHNIQUE FOR EXPLOSION WELDING OF HIGH-STRENGTH ALUMINUM ALLOYS OF SERIES 7xxx S.Yu. Illarionov*, L.D. Dobrushin**,

Objective Aluminium Alloy.

Chapter 6: Mechanical Properties

Mechanical Properties

CHAPTER 6: MECHANICAL PROPERTIES

11O105 BASICS OF CIVIL AND MECHANICAL ENGINEERING Prepared by Mr. C. Ayyasamy Assistant Professor Department of Mechanical Engineering Bannari Amman Institute.

Selection Criteria Properties Availability Cost Manufacturability

STRUCTURAL TRANSFORMATIONS IN Al-Cu COMPOSITE I. S. Los', A. V. Khorin, G. V. Kozlov, and A. V. Pryshchak Penza State University XII International Symposium.

Classification of Metals

Aluminum 6061-T6 Christian Bushnell Christian Bushnell Joshua Higgins Joshua Higgins Eric Lemont Eric Lemont Harold Mason Harold Mason Christopher Michaud.

Materials PHYA2. MATERIALS DENSITY, SPRINGS, STRESS AND STRAIN Topics 11, pp.162–173.

Design of Concrete Structure I Dr. Ali Tayeh First Semester 2009 Dr. Ali Tayeh First Semester 2009.

ENGR-45_Lec-14_Metal_MechProp-1.ppt 1 Bruce Mayer, PE Engineering-45: Materials of Engineering Bruce Mayer, PE Registered Electrical.

Mix design of fiber reinforced concretes Exercise 9.

Welding Design 1998/MJ1/MatJoin2/1 Design. Lesson Objectives When you finish this lesson you will understand: Mechanical and Physical Properties (structure.

Welding Inspection and Metallurgy

Chapter 3 Micromechanical Analysis of a Lamina Volume Fractions, Weight Fractions, Density, and Void Content Dr. Autar Kaw Department of Mechanical Engineering.

ME Manufacturing Systems Introduction To Manufacturing Systems by Ed Red Introduction To Manufacturing Systems by Ed Red.

Chapter 2 Properties of Metals.

Properties of materials. The behaviour of a given material is characterised by the response to a stimulus. Mechanical properties (behaviour under a set.

Chapter 9: Mechanical Properties of Matter

1) Metal wires after cold work are usually sold in markets. Why? Increase yield strength This is called cold work strengthening. Tutorial (2)

Resistance welding. Conti…… Resistance Welding is a welding process, in which work pieces are welded due to a combination of a pressure applied to them.

Bachelor of Technology Mechanical Industrial Material UOG Lecture # 04 By: Jahangir Rana.

UNIT-01. SIMPLE STRESSES & STRAINS Lecture Number - 06 Prof. S.C.SADDU MECHANICAL DEPARTMENT SIT LONAVALA Strength of Materials.

Properties of Concrete Design and Control of Concrete Mixtures – Chapter 9.

The Wonderful World of… TECHNOLOGY. MATERIALS External forces produce various effects inside a material. EXAMPLE: *Consider what would happen if an elephant.

Week 4 Fracture, Toughness, Fatigue, and Creep

Epoxy (Polyepoxide) Gerardo De Leon MEEN Epoxy ( Polyepoxide)

Aluminum Alloy 6061 – Composition, Properties, Temper and Applications of 6061 Aluminum.

Dr. Owen Clarkin School of Mechanical & Manufacturing Engineering Summary of Material Science Chapter 1: Science of Materials Chapter 2: Properties of.

Mechanical properties of dental biomaterials 2

Physical properties Enrollment numbers Government engineering collage,Palanpur sub:- Applied.

Epoxy Infusion System – Hardener SIN B17 Polynt’s SIN B17 is the world’s first Epoxy resin hardener based on anhydride chemistrythat has been specially.

Strain Hardening Concrete – Applications in Underground Coal Mines.

BY ADITYA RAMAKRISHNAN

Tensile strength (MPa) Length (m) of fibers/kg

Mechanical Properties of Metals

Chapter 3 Mechanical Properties of Materials

Poisons Ratio Poisons ratio = . w0 w Usually poisons ratio ranges from

بسم الله الرحمن الرحيم.

Tutorial in Mechanical Properties

Strain Hardening & Annealing

Mechanical Properties of Metals

Mechanical Properties Of Metals - I

Presentation transcript:

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

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

3 Appearance

4 Flight performance Beriev aircraft company

5 Patent

6 Sial (glare) Beriev aircraft company

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 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 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 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