Agilis测量系统 - 探针优化的考虑事项.pdf

Optical Probe Considerations Confidentiality Statement The information contained in this document and referenced material is confidential and proprietary business information of Agilis Measurement Systems, Inc.TM This information cannot be disclosed to any third party, and must be secured and maintained as confidential at all times. © 2012 Agilis Measurement Systems, Inc. TM Export Controlled This document contains information within the purview of the Export Administration Regulations (EAR), 15 CFR 730-774, and is export controlled. Transfer or export contrary to U.S. law is prohibited. ECCN: 9E990 / No License Required 2014 Agilis Measurement Systems, Inc. Proprietary and Confidential. Use or disclosure of the data contained in this page is subject to the restrictions on the first page of this document 1 Estimated Noise Floor from Case, Rotor and Low Stress, Random Blade Motion ‣ Compressor, ~40” radius: 3.0 mils p-p ‣ Compressor, ~12” radius: 0.5mils p-p ‣ Turbo Compressor, ~2” radius: 0.1 p-p ‣ Turbine, ~40” radius: ~3.0 mils p-p ‣ Turbine, ~12” radius: ~1.0 mils p-p ‣ Turbo Turbine, ~2” radius: ~0.3 mils p-p 2014 Agilis Measurement Systems, Inc. Proprietary and Confidential. Use or disclosure of the data contained in this page is subject to the restrictions on the first page of this document 2 Event Area Characteristics ‣ Surface texture should be small relative to expected noise floor. ‣ Edge radii should be small relative to expected noise floor ‣ Edge nicks should be small relative to expected noise floor ‣ Minimize Blade to Blade variability