Browse Topic: Air pollution

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TEST https://wcm14-tst.cld.sae.org/site/binaries/content/gallery/mobilus-brx/digital-supplements/software-diagram.png/software-diagram.png/sae%3Amedium
This specification covers the requirements for a hard anodic coating on magnesium alloys.
AMS B Finishes Processes and Fluids Committee
There has been a recent upsurge in interest from the media concerning the quality of the environment within aircraft cabins and cockpits especially in the commercial world. This has included (although by no means been limited to) the air quality, with particular reference to the alleged effects of contamination from the aircraft turbine lubricant. Possible exposure to 'organophosphates' (OPs) from the oil has raised special concerns from cabin crew. Such is the concern that government organisations around the world, including Australia, USA and UK, have set up committees to investigate the cabin air quality issue. Concern was also voiced in the aviation lubricants world at the way in which OP additives in turbine lubricants were being blamed in some reports for the symptoms being experienced by air crew and passengers. SAE Committee E-34 therefore decided that it should gather as much available information on the subject as possible. This would then enable E-34 to participate in debates on the issue and help prevent a potentially erroneous decision regarding the future of OP based additives in turbine lubricants. It would also serve as an indicator of where any additional work may be necessary to properly gauge the role that turbine lubricants, and OP additives, play in cabin air quality. This report summarises recent documentation from the literature on this subject. The contents do not necessarily represent the views of the SAE or any of the members of the study group who produced this review. The literature falls into three categories: - Air quality (Section 5), which includes: future systems to improve air quality and research plans into investigating cabin air quality - Chemistry of turbine lubricants, phosphate esters (Section 6), including evaluation of products found in cabin air and thermal breakdown products of lubricants. - Toxicity evaluation of turbine oils and additives (Section 7).
E-34 Propulsion Lubricants Committee
AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 0 OVERVIEW OF ARINC 653ARINC653P0-3 (Current)11/15/2021
This document provides an overview of the entire set of documents collectively referred to as ARINC 653. As this set of documents evolves, Part 0 has been adjusted to reflect technical changes made in Supplements to Parts 1 through 5 in conjunction with the technical changes made in the evolution of ARINC 653. A summary of the ARINC 653 documents follows: Part 0 – Overview of ARINC 653 Part 1 – Required Services Part 2 – Extended Services Part 3A – Conformity Test Specification for ARINC 653 Required Services Part 3B – Conformity Test Specification for ARINC 653 Extended Services Part 4 – Subset Services Part 5 – Core Software Recommended Capabilities The term “this document” refers to Part 0 only, while the term “ARINC 653” or “the Specification” refers to the whole set of ARINC 653 documents, currently Parts 0 to 5. The primary objective of ARINC 653 is to define a general-purpose APplication/EXecutive (APEX) interface (API = Application Program Interface) between the Core Software (CSW) of an Avionics Computer Resource (ACR) and the application software. Included within ARINC 653 are the interface requirements between the application software and the CSW and the list of services which allow the application software to control the scheduling, communication, and status information of its internal processing elements.
Airlines Electronic Engineering Committee
This SAE Aerospace Recommended Practice (ARP) describes recommended sampling conditions, instrumentation, and procedures for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to estimate sampling system loss performance. This ARP is not intended for in-flight testing, nor does it apply to engines operating in the afterburning mode. This ARP is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances.
E-31P Particulate Matter Committee
Questions about Real Driving Emissions in BrazilSAE-PP-002272/2/2021
The motor vehicles are the main source of atmospheric pollution, especially carbon monoxide, hydrocarbons and nitrogen oxides (NOx). To reduce these emissions for environmentally acceptable levels, Europe and the United States have developed control programs, where are set emissions limits for new vehicles, which are gradually reduced over time and the compliance must be done through standardized tests in laboratories. However, Europe is facing a problem: NOx level in the cities is not being reduced in the same proportion of the homologation limits, due to two factors: the poor representativeness of the test procedures in comparison of the “real world” and the use of engine management software that produces low pollutants just in laboratory tests. Several studies about real world emissions have pointed to vehicles, approved in the laboratory, emitting in the streets about 7 up to 40 times more NOx than the homologation limit. To fix this problem, since September/2017 Europe will add to the vehicles type-approval process a real driving emissions test (Real Driving Emissions - RDE), where the vehicle must meet the limits when running in streets coupled to a portable measuring system. In order for the RDE procedure be applied effectively to the Brazilian reality, it is necessary to discuss three relevant points: the differences between the national and the European fleet, the procedure itself, focused on NOx control and the specific characteristics of Brazilian cities. This paper has the objective to discuss about RDE principles and how it can to be applied in the Brazilian reality.
Anthony, Lindsay
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode. This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320. Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.
E-31P Particulate Matter Committee
A Novel Solid Oxide Fuel Cell Based Catalytic Converter Replacement for Enhanced Emission Control and Power Generation in Automotive Exhaust2020-01-03534/14/2020
Increased concerns over climate change, limited fossil fuel resources, emissions, and poor air quality has created a greater need for sustainable energy systems. The need for increased sustainable energy systems has created largely two cooperative movements: 1) technologies that are considered renewable or more environmentally friendly and 2) higher efficiency. The automotive industry has long been a target for increasing efficiency and decreasing emissions. Current emission control systems rely heavily on the usage of precious metal based catalytic converters. Traditional catalytic converters convert incomplete combustion products into carbon dioxide and water vapor. During this conversion, any remaining chemical energy within the exhaust is lost to waste heat production. In order to achieve increased efficiency and reduced pollutant emission, the remaining chemical energy in the exhaust must be transformed into usable energy. A Solid Oxide Fuel Cell (SOFC) stack is therefore integrated into the exhaust system of a traditional internal combustion engine in place of the current upstream catalytic converter. A SOFC stack would eliminate the need to maintain stoichiometric exhaust conditions, and would allow the recovery of any remaining chemical energy in the exhaust stream. The SOFC stack creates the potential for electrical power generation from the exhaust, while significantly improving emission reduction in a lean environment when compared to the traditional catalytic converter. Initial testing indicates that a typical internal combustion engine operating at stoichiometric conditions results in an exhaust composition of ~2-3% H2 and CO and ~1% mixed hydrocarbons. These exhaust constituents may be used by the SOFC for electrical power generation. Simultaneously, the SOFC stack has demonstrated an ability to decrease hydrocarbon, carbon monoxide, and nitrogen oxide emission by up to 50% when compared to a traditional platinum foil based catalytic converter.
Welles, Thomas S.Ahn, Jeongmin
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