Turbine Engine Component
Air Flow Test System
Low Flow Configuration
Air Flow Test System
Low Flow Configuration
Ø Designed for Aircraft Components
Ø Up to 4 Flow Ports for Multi-path Fixtures
| Low Flow
Configuration Specifications: |
|
| (Refer to our brochure
and technical notes on this product for more information.) |
|
| Nozzle Set: Standard - 6 Sonic Nozzles with a
binary progression in throat area |
|
| (diameters range from 0.031” to 0.177”). |
|
| Option 1 - 7 Sonic Nozzles with a binary progression in throat
area |
|
| (diameters range from 0.022” to 0.177”). |
|
| Option 2 - 7 Sonic Nozzles with a binary progression in throat
area |
|
| (diameters range from 0.031” to 0.250”). |
|
| Air Mass Flow Range: Standard 0.0005 to 0.1 lbm/sec 200:1 Turndown |
|
| Option 1
0.0003 to 0.1 lbm/sec 333:1
Turndown |
|
| Option 2
0.0005 to 0.22 lbm/sec 440:1
Turndown |
|
| (Refer to FLOW SYSTEMS’
Technical Note “Flow Bench Capabilities” for detailed Test Measure ranges,
Effective Area, Flow Parameter, Reduced Mass Flow.) |
|
| Part Pressure Range: 0.5 to 50 psig (other, custom ranges available on request) |
|
| Part Pressure Ratio
Range: 1.04 to 4.4 psig (other, custom ranges available on request) |
|
| Accuracy: +/-0.48% of reading, traceable to NIST
Standards. |
|
| (Refer to FLOW SYSTEMS’
Technical Note “Low & High Flow Systems Uncertainty Analysis”.) |
|
| Repeatability:
Less than +/-0.25% as defined as 2 standard deviations divided by the mean |
|
| of 20 identical samples. |
|
| Cycle Time: 20 to 40 seconds depending on percentage of
maximum capacity. |
|
| Connections: Flow
Ports -12 Swagelok Full Flow Female Quick Connectors QF series; (-16 on
Option 2) |
|
| Pressure -4
Swagelok Instrumentation Female Quick Connectors QC series, color keyed. |
|