The Influence of Shm Techniques on Scheduled Maintenance of Aircraft Composite Structures

نویسنده

  • Xi Chen
چکیده

Scheduled maintenance procedures for civil aircraft structures went through decades of evolution from hard time replacement to timebased inspection. Currently, different inspection tasks are carried out at predetermined intervals to check the condition of structural components. If the condition of the structure exceeds a certain threshold, repair activities are initiated. The two key parameters in scheduled maintenance are the inspection interval and the repair threshold. The development of new materials such as composites and the introduction of advanced Structural Health Monitoring (SHM) techniques, will have a profound effect on scheduled maintenance. Considering the current level of maturity of SHM technologies, several combinations of SHM and scheduled maintenance are proposed in this paper and a probabilistic analysis is performed to quantify the savings on maintenance cost.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Composite Panel Damage Detection using Ultrasonic Testing and Neural Networks

For modern aircraft, wind turbines, and other aerospace structures composites are replacing metal components. These aerospace structures will be designed and expected to perform well for many years ahead. Therefore, structural health monitoring (SHM) systems are being designed to monitor these structures to improve maintenance, repairing or replacing composites components when the need arises. ...

متن کامل

Experimental characterisation of Lamb wave propagation through thermoplastic composite ultrasonic welds

Ultrasonic welding is a very promising technique for joining thermoplastic composite (TpC) components in aircraft primary structures [1, 2]. The potential introduction of new lightweight structures in civil aviation has been driving the change towards condition-based maintenance (CBM) as an alternative to the regular inspection interval approach [3]. In turn, CBM has been pushing forward the de...

متن کامل

On-Line Multi-Damage Scanning Spatial-Wavenumber Filter Based Imaging Method for Aircraft Composite Structure

Structural health monitoring (SHM) of aircraft composite structure is helpful to increase reliability and reduce maintenance costs. Due to the great effectiveness in distinguishing particular guided wave modes and identifying the propagation direction, the spatial-wavenumber filter technique has emerged as an interesting SHM topic. In this paper, a new scanning spatial-wavenumber filter (SSWF) ...

متن کامل

Classification and Quantification of Matrix Micro-cracks in Composite Structures

Fiber reinforced composites have been widely used in aerospace applications due to their functional properties such as high strength-to-weight ratios. But many challenges are yet to be overcome in order to have more confidence on the performance of composites structures. Particularly, composites have different failures types and modes that make the damage prediction and propagation a very chall...

متن کامل

A phase reconstruction algorithm for Lamb wave based structural health monitoring of anisotropic multilayered composite plates

Platelike structures, made of composites, are being increasingly used for fabricating aircraft wings and other aircraft substructures. Continuous monitoring of the health of these structures would aid the reliable operation of aircrafts. This paper considers the use of a Lamb wave based structural health monitoring SHM system to identify and locate defects in large multilayered composite plates...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2014