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General Industry (2) Spotlight on Design (2)

Power Quality Test Data Analysis for Aircraft Subsystem

  • UTC Aerospace Systems-Shobha Ramanjani
  • Technical Paper
  • 2018-01-1932
To be published on 2018-10-30 by SAE International in United States
Aircraft subsystem development involves various combinations of testing and qualification activities to realize a flight worthy system. The subsystem needs to be verified for a massive number of customer requirements. Power Quality (PQ) testing is also an important testing activity carried out as a part of the environmental qualification test. It is intended to verify the functionality of subsystem with various power disturbances, to determine the ability of a subsystem to withstand power quality disturbances. The subsystem being designed should be reliable enough to handle power quality anomalies. Power quality test generates an enormous amount of test result data for analysis with millions of data samples depending on the test, and can be identified as Big Data. The engineer needs to analyze each set of test data as a part of post processing to ensure the power disturbances during testing are as per the standard requirements and functional performance of the subsystem is met. Manually analyzing the test data with classical methods and generating the report requires more time and effort, as it needs analysis of millions of test data samples, also leading to the possibility of errors. Hence it is required to have automated methods to perform unsupervised data analysis in a faster way and generate the post processed report as required by the end user. This paper presents the testing of aircraft subsystem, for power quality with various power input disturbances involved, mainly focusing on test data analysis techniques using script based analysis tools. Also, it discusses on the utilization of options available in various tools for automation of test data analysis and presentation.

Novel Framework Approach for Model-Based Process Integration from Requirements to Verification Demonstrated on a Complex, Cyber-Physical Aircraft System

  • ESI ITI GmbH-Marcel Gottschall, Bastian Binder
  • United Technologies Research Center-Hajer Saada, Luis Diogo Couto, Fabio Cremona, Gilberto Burgio
  • Show More
  • Technical Paper
  • 2018-01-1947
To be published on 2018-10-30 by SAE International in United States
This paper presents a demonstrator developed in the European CleanSky2 project MISSION (Modelling and Simulation Tools for Systems Integration on Aircraft). Its scope is the development towards a seamless integrated, interconnected toolchain enabling more efficient processes with less rework time in todays, highly collaborative aerospace domain design applications.

ED-247 (VISTAS) Gateway for Hybrid Test Systems

  • dSPACE France SARL-Yannick Hildenbrand
  • Technical Paper
  • 2018-01-1949
To be published on 2018-10-30 by SAE International in United States
Testing a full Aircraft System that includes several on-board computers, physical I/O, and communication buses requires connecting the system to adequate test benches to stimulate or monitor the I/O in a suitable manner. Next generation benches are controlled by test scenarios that reproduce flight situations that occur in a real aircraft.

Highly Efficient Civil Aviation, Now via Operations: AAR & Challenges

  • Independent Contractor-R K Nangia
  • Technical Paper
  • 2018-01-1925
To be published on 2018-10-30 by SAE International in United States
No Abstract Available.
new

Oxygen System and Component Cleaning

  • A-10 Aircraft Oxygen Equipment Committee
  • Aerospace Standard
  • ARP1176A
  • Current
Published 2018-10-18 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces, parts (including regulator and valve parts), cylinders and ground-based equipment that may be used to support aircraft oxygen systems. This revision introduces a cleanliness coding scheme that can be referenced as a requirement, and/or referenced to identify compliance to meeting such a requirement. These methods may apply to gaseous and liquid oxygen equipment. This document specifies work area details, methods to select suitable cleaning agents, cleaning methods, test methods to verify cleanliness level, and methods of packaging the components and parts after cleaning. Technicians designated to clean oxygen equipment must be qualified and trained to clean oxygen equipment. This ARP is applicable to metallic and non-metallic parts.
new

Liquid Oxygen Systems

  • A-10 Aircraft Oxygen Equipment Committee
  • Aerospace Standard
  • AIR825/5A
  • Current
Published 2018-10-18 by SAE International in United States
This Aerospace Information Report provides general information to aircraft designers and engineers, regarding LOX, its properties, its storage and its conversion to gas. Much useful information is included herein for aircraft designers regarding important design considerations for a safe and effective installation to an aircraft. The associated ground support equipment needed to support operations of LOX equipped aircraft is also discussed. It is important to realize that LOX equipped aircraft cannot be supported unless this support infrastructure is also available. A significant part of this document will address the specific advantages, disadvantages and precautions relating to LOX systems. These are important issues that must be considered in deciding which oxygen system to install to the aircraft. Also, many commercial and military aircraft use aeromedical LOX equipment that is mostly portable equipment. Aeromedical LOX equipment is not addressed herein as it is beyond the scope of this document.
new

Guide for Evaluating Combustion Hazards in Aircraft Oxygen Systems

  • A-10 Aircraft Oxygen Equipment Committee
  • Aerospace Standard
  • AIR825/13
  • Current
Published 2018-10-18 by SAE International in United States
This guide is intended to promote safe designs, operations and maintenance on aircraft and ground support oxygen systems. This is also a summary of some work by the ASTM G 4 Committee related to oxygen fire investigations and design concerns to reduce the risk of an oxygen fire. There have been many recent technological advances and additional test data is available for evaluating and controlling combustion hazards in oxygen equipment. Standards that use this new information are rapidly evolving. A guide is needed to assist organizations and persons not completely familiar with this process to provide oxygen systems with minimum risks of combustion. This guide does not necessarily address all the detailed issues and provide all data that will be needed. For a complete analysis, supplemental publications need to be consulted. This guide does discuss the basics of oxygen systems fire hazards. The hazard analysis process is discussed and a simple example to explain this process. Also, this guide does not address the overall system safety issues normally evaluated in aircraft programs. This guide does provide some important background and observations about combustion in oxygen systems. Information is given describing how to accomplish a hazard analysis. Furthermore, background is provided to explain critical locations in oxygen systems that need to be evaluated and other locations that do not require hazard analysis.
new

Disinfectant, Aircraft, for Use in Cargo Compartments

  • AMS J Aircraft Maintenance Chemicals and Materials Committee
  • Aerospace Material Specification
  • AMS1451C
  • Current
Published 2018-10-16 by SAE International in United States
This specification covers disinfectants or chemicals for use in disinfecting aircraft after carrying livestock.
new

TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDBACK TYPE, SERIES II

  • AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81714/67A
  • Current
Published 2018-10-10 by SAE International in United States
No Abstract Available.
new

INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE I, CLASS 1, COMPOSITION C

  • AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81969/18
  • Current
Published 2018-10-10 by SAE International in United States
No Abstract Available.