Aircraft Maintenance and Aircraft Reliability Engineering Software System (ARESS)
Safety is a key technical issue in aviation industry. This patent provides a comprehensive assessment and evaluation of safety level of aircraft subsystems through generating a comprehensive Reliability Report for each aircraft in fleet of an airline (also helicopter fleet and General Aviation). It also assists maintenance units of airlines to maintain technical failure data and monitor subsystems through generating a great number of plots based on very complex reliability computations for all subsystems of each aircraft in an airline's fleet.
A brief description of the capabilities of the patent
This invention (and the developed software system) is a comprehensive and advanced package designed and developed specifically for comprehensive reliability analysis of aircraft subsystems. This patent in fact presents for the first time some comprehensive methods, ideas and a comprehensive and complete software system for numerical assessment and evaluation of reliability of all aircraft subsystems.
This invention presents methods, ideas and software system named “ARESS”, short for Aircraft Reliability Engineering Software System. This advanced innovative Windows software utilizes the modern software technologies and it is a state-of-the-art integrated environment and world-level solution that can provide for the first time a comprehensive reliability analysis for all subsystems of all aircraft models existing in a fleet of an airline. All types of aircraft and subsystems can be analyzed by the software system.
Determining and knowing reliability estimations of each subsystem of an aircraft is very important and essential task.
The software with its powerful and DYNAMIC algorithm is designed to provide comprehensive reliability analysis computations for any airplane model; several examples with data for some modern passenger airplane models show that how the software works by using real and simulated data sets for their subsystems.
The powerful computational engine of the software includes two computational modes: non-automatic mode (MRDA) and automatic mode (ARDA). In the MRDA mode, all processes and analyses are controlled and intervened by the user through selection of the relevant options. In the ARDA mode, all the computational steps and processes are controlled and executed automatically by the ROBUST, POWERFUL and DYNAMIC algorithms of the software system.
The monitoring section of the patent/software is also a very important tool for finding possible problematic subsystems through generating a great number of plots for all aircraft systems.
A business model has also been provided for implementing the project.
The comprehensive methods and ideas of the patent are ALL thoroughly introduced, developed, and implemented by the inventor for the first time.
As a conclusion, the invention is in fact a key solution and product for aviation safety and aircraft maintenance in airline industry, helicopter maintenance, General Aviation industry, and etc.
US 10,861,252 issued 2020-12-08 [MORE INFO
Type of Offer:
« More Aeronautics Patents« More Software Patents