Setting D-26 in materials, Bauman Moscow State Technical University
Sold <10
                                0 000 X
                                
                            
                            
                        
        
        
            
            
                There are no such quantities in stock
            
        
        
    
                    
                            By clicking the button, you agree to
                            
                                terms for buyers
                            
                        
                    
                
                
                    Secure deal
                
            
            
            
                
                    
                    
                        Instant delivery
                    
                
            
        Product description
                        
        
            
        
    Setting №D-26 
For load-bearing elements of the aircraft (chassis parts and plating, stringers, frames, spars, etc..) Are widely used wrought aluminum alloys brands: D1, D16, V93, V95 and others.
1. Select a deformable aluminum alloy for the production of power de¬taley landing gear section 50 mm. Assign the mode of heat treatment, provides the highest resistance to fatigue crack propagation alloy, yield strength σ0,2> 500 MPa, elongation δ> 9%. Plot the heat treatment temperature-time indicating: the heating temperature, holding time, cooling medium.
2. Describe the structural changes taking place in parts at all stages of heat treatment
3. Provide basic information on the alloy chemical composition according to GOST, the scope, the requirements for this type of product, mehaniche¬skie and technological properties, the influence of alloying elements and others.
References 6
                    
        
            For load-bearing elements of the aircraft (chassis parts and plating, stringers, frames, spars, etc..) Are widely used wrought aluminum alloys brands: D1, D16, V93, V95 and others.
1. Select a deformable aluminum alloy for the production of power de¬taley landing gear section 50 mm. Assign the mode of heat treatment, provides the highest resistance to fatigue crack propagation alloy, yield strength σ0,2> 500 MPa, elongation δ> 9%. Plot the heat treatment temperature-time indicating: the heating temperature, holding time, cooling medium.
2. Describe the structural changes taking place in parts at all stages of heat treatment
3. Provide basic information on the alloy chemical composition according to GOST, the scope, the requirements for this type of product, mehaniche¬skie and technological properties, the influence of alloying elements and others.
References 6
Main features
- Content type File
- Content description 57,98 kB
- Updated on the site 10.05.2013
Reviews
No reviews yet
                                0 000 X
                                
                            
                            
                        
        
        
            
            
                There are no such quantities in stock
            
        
        
    
                    
                            By clicking the button, you agree to
                            
                                terms for buyers
                            
                        
                    
                
                
                    Secure deal
                
            
            
            
                
                    
                    
                        Instant delivery
                    
                
            
        