T/ACEF 081-2023 Active Group standards

T/ACEF 081-2023 Fixed-wing general aviation platform and guidelines for in-situ measurement of atmospheric particulate matter by aerial technology

T/ACEF 081-2023 Fixed-wing general aviation platform and guidelines for in-situ measurement of atmospheric particulate matter by aerial technology

Publish Date: 2023-05-31 Implement Date: 2023-06-01 For services related to genuine standard inquiry, procurement, translation, and other related services in China, please Contact Us
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Basic Information

Standard Code: T/ACEF 081-2023
Standard Type: Group standards
Standard Status: Active
is_force_gb: no
CCS Name: Environmental protection sampling and analysis testing methods
ICS Name: Environmental air
Publish Date: 2023-05-31
Implement Date: 2023-06-01
Pages: 17 pages

Scope

Scope: This document provides guidance on the composition and functionalities of the aerial in-situ measurement system for atmospheric particulate matter on fixed-wing general aviation platforms, including technical content, quality assurance, and quality control. This document is applicable to high-altitude observations of atmospheric particulate matter using aerial in-situ measurement methods on fixed-wing general aviation platforms, and can also be used for the design, modification, integration, testing, and application of aerial in-situ measurement systems for atmospheric particulate matter. Note: This document does not include unmanned aerial vehicles as fixed-wing general aviation platforms for aerial in-situ measurement systems. **Main Technical Content**: 4. System Composition and Functionalities 4.1 General Principles 4.1.1 Measurement System 4.1.2 Measurement Process 4.2 System Composition 4.3 Functionalities 4.3.1 Atmospheric Observation Aircraft 4.3.2 Isokinetic Sampler 4.3.3 Atmospheric Particulate Matter Sampling System 4.3.4 Aerial Atmospheric Particulate Matter Measurement System 4.3.5 Pressure Control and Flow Diversion System 4.3.6 Calibration System 4.3.7 Data Acquisition, Storage, and Processing System 5. Technical Content 5.1 Atmospheric Observation Aircraft 5.1.1 Fixed-Wing Aircraft 5.1.2 Network Communication Module 5.1.3 Power Supply Module 5.1.4 Environmental Control Module 5.1.5 Auxiliary Integration Module 5.2 Atmospheric Particulate Matter Sampling System 5.2.1 Atmospheric Particulate Matter Sampling Pipe 5.2.2 Multi-Branch Particulate Pipeline in the Cabin 5.3 Aerial Atmospheric Particulate Matter Measurement System 5.3.1 Instrument Appearance 5.3.2 Environmental Adaptability 5.3.3 Safety 5.3.4 Instrument Performance 5.3.4.1 Passive Chamber Particulate Probe 5.3.4.2 Particle Number Spectrometer 5.3.4.3 High-Resolution Mass Spectrometer 5.3.4.4 Single Particle Black

Development Information

Pages: 17 pages

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