Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 2

Search results for: R. Doubrava

2 Classification of Impact Damages with Respect of Damage Tolerance Design Approach and Airworthiness Requirements

Authors: R. Doubrava, T. Mrna

Abstract:

This paper describes airworthiness requirements with respect damage tolerance. Damage tolerance determines the amount and magnitude of damage on parts of the airplane. Airworthiness requirements determine the amount of damage that can still be in flight capable of the condition. Component damage can be defined as barely visible impact damage, visible impact damage or clear visible impact damage. Damage is also distributed it according to the velocity. It is divided into low or high velocity impact damage. The severity of damage to the part of airplane divides the airworthiness requirements into several categories according to severity. Airworthiness requirements are determined by type airplane. All types of airplane do not have the same conditions for airworthiness requirements. This knowledge is important for designing and operating an airplane.

Keywords: Composite, Damage Tolerance, airworthiness requirements, low and high velocity impact

Procedia PDF Downloads 392
1 Development of a New Method for T-Joint Specimens Testing under Shear Loading

Authors: Radek Doubrava, Roman Růžek

Abstract:

Nonstandard tests are necessary for analyses and verification of new developed structural and technological solutions with application of composite materials. One of the most critical primary structural parts of a typical aerospace structure is T-joint. This structural element is loaded mainly in shear, bending, peel and tension. The paper is focused on the shear loading simulations. The aim of the work is to obtain a representative uniform distribution of shear loads along T-joint during the mechanical testing is. A new design of T-joint test procedure, numerical simulation and optimization of representative boundary conditions are presented. The different conditions and inaccuracies both in simulations and experiments are discussed. The influence of different parameters on stress and strain distributions is demonstrated on T-joint made of CFRP (carbon fiber reinforced plastic). A special test rig designed by VZLU (Aerospace Research and Test Establishment) for T-shear test procedure is presented.

Keywords: Finite Element Analysis, Methodology, Composite, Mechanical testing, shear, t-joint

Procedia PDF Downloads 306