scholarly journals Strength, Fatigue Strength and Stiffness of High-Tech Bamboo/Epoxy Composites

2014 ◽  
Vol 05 (13) ◽  
pp. 1281-1290 ◽  
Author(s):  
Michael James Platts
Author(s):  
Ricarda Berger ◽  
Benedikt Hofmeister ◽  
Cristian G. Gebhardt ◽  
Raimund Rolfes

Abstract Advanced repair techniques intended for jet engine parts are continuously under development and improvement. Patching is a high-tech approach towards reduced scrap rates and an extended life of high pressure compressor blisks. In this work, we contribute to the structural design of patches for compressor blisks with improved high cycle fatigue behaviour. A fully parameterised patch model is developed, which allows the accurate description of the patch geometry. High cycle fatigue is assessed for welding seam positions specified by the patch model. On the basis of this automated process, a multi-objective optimisation is carried out. The fatigue strength and the length of the welding seam are defined as conflicting targets. Pareto-optimal solutions are calculated using a generalised pattern search algorithm. The engineer’s decision for a specific patch geometry can thus be made based on the optimisation results. The application of the new approach to a compressor blisk demonstrates the influence of vibration modes on fatigue strength. We identify sets of optimal suited patch geometries in accordance to the specified damage pattern.


2009 ◽  
Vol 18 (5) ◽  
pp. 096369350901800
Author(s):  
A.M. Amaro ◽  
F.V. Antunes ◽  
A. Ramalho

Composite materials are mostly submitted to dynamic loads, because of their excellent specific strength and stiffness, therefore the resonant technique is adequate for the determination of stiffness properties. Three plates of similar carbon-epoxy composites with distinct fibre orientations were studied with this technique. The effect of stacking sequence on the rigidity of laminated composites was investigated A significant influence of this material parameter on in-plane elastic properties was found, allowing optimization of stiffness for a particular application.


1989 ◽  
Vol 38 (434) ◽  
pp. 1329-1335 ◽  
Author(s):  
Kenjiro KOMAI ◽  
Sohei SHIROSHITA ◽  
Sadamu KINOSHITA ◽  
J. GRENESTEDT

Alloy Digest ◽  
1990 ◽  
Vol 39 (4) ◽  

Abstract KEVLAR 49 is a high-modulus para-aramid reinforcing fiber. It is the dominant organic reinforcing fiber in advanced composites today. It has exceptional strength and stiffness and it is a low density material. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as creep. It also includes information on machining. Filing Code: Cp-7. Producer or source: E. I. Dupont de Nemours & Company Inc..


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