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AIR6037
Aircraft Exhaust Nonvolatile Particle Matter Measurement Method Development
Aircraft Exhaust Nonvolatile Particle Matter Measurement Method Development
有效
【范围】 This report provides current practice measurement methods for quantifying nonvolatile particle matter at the exit plane of aircraft gas turbine engines. This document contains detailed information for many instruments and techniques, described in AIR5892A, that have been applied in aircraft engine field tests since AIR5892A was first issued in April 2003. There are four sections, identified as Technical Appendices (TA), presenting measurement techniques, sampling, and quantification of nonvolatile particles. The sections are written in the format of Aerospace Recommended Practice (ARP) documents and intended to progress to recommended practices upon overcoming existing technical challenges. Many important technical advances have been accomplished that comprise the Aircraft Engine Exhaust Nonvolatile Particle Matter Measurement Method Development techniques described in TA A: Particle Mass,TA B: particle Number and Size,TA C: Particle Sampling, and TA D: Calculation of Particle Number and particle Mass Emission Indices. Various measurement methodologies and operability and compatibility issues are described within the TAs. The TAs briefly discuss degrees of sensitivity, accuracy, repeatability, and test operations acceptability for each measurement discipline. They reflect that many important technical advances have been accomplished for measurement techniques of nonvolatile particles. Additional research is required to transition the TAs to Aerospace Recommended Practices.strRefField
【与前一版的变化】

包含缩略语

BC
cfm
cm
CO2
EC
g
m
mg
μg
μm
nm
OC
P
PM
V
L
slpm
SN
T
t
TC

引用文件/被引文件

Nonvolatile Exhaust Particle Measurement Techniques
Aircraft Gas Turbine Engine Smoke Measurement Practice

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包含图表

AVAILABLE METHODS FO
SELECTED METHODS FOR
SCHEMATIC OF THE GRA
CARBON MASS (TEMPERA
REPRESENTATIVE GRAVI
THERMO SCIENTIFIC SE
SEMTECH-QCM INSTRUME
MODEL 5012 MAAP FROM
MODEL 5012 MAAP FLOW
SCHEMATIC OF THE MAA
FORMULA 1
FORMULA 2
ARTIUM TECHNOLOGIES
SCHEMATIC OF LII 200
FORMULA 3
LII SYSTEM MOUNTED I
PARTICLE MASS CONCEN
LII PARTICLE MASS PR
THE LII CONCEPT INVO
IMAGE OF LII FROM SO
GEOMETRY OF THE LII
RAW DATA IMAGE OF A
SOOT GENERATOR TO CR
INSTRUMENT CALIBRATI
FORMULA 1
FORMULA 2
FORMULA 3
FORMULA 4
FORMULA 5
FORMULA 6
SIZE DISTRIBUTION RE
FORMULA 7
IDEALIZED AIRCRAFT D
SCHEMATIC OF A SATUR
FORMULA 8
SCHEMATIC OF AN SMPS
SCHEMATIC OF A RMPS
EXAMPLE SAMPLING CON
EARLY PARTICLE SAMPL
CURRENT PARTICLE SAM
FORMULA 8
FORMULA 9
FORMULA 10
FORMULA 11
FORMULA 12
FORMULA 13
PENETRATION EFFICIEN
PENETRATION EFFICIEN
MEASURED SIZE DEPEND
ILLUSTRATION OF THE
FORMULA 14
FORMULA 15
FORMULA 16
FORMULA 17
FORMULA 18
FORMULA 19
FORMULA 20
FORMULA 21
FORMULA 22
FORMULA 23
FORMULA 24

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