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On Shaft Data Acquisition System (OSDAS)On Shaft Data Acquisition System (OSDAS) is a rugged, compact, multiple-channel data acquisition computer system that is designed to record data from instrumentation while operating under extreme rotational centrifugal or gravitational acceleration forces. This system, which was developed for the Heritage Fuel Air Turbine Test (HFATT) program, addresses the problem of recording multiple channels of high-sample-rate data on most any rotating test article by mounting the entire acquisition computer onboard with the turbine test article. With the limited availability of slip ring wires for power and communication, OSDAS utilizes its own resources to provide independent power and amplification for each instrument. Since OSDAS utilizes standard PC technology as well as shared code interfaces with the next-generation, real-time health monitoring system (SPARTAA Scalable Parallel Architecture for Real Time Analysis and Acquisition), this system could be expanded beyond its current capabilities, such as providing advanced health monitoring capabilities for the test article. High-conductor-count slip rings are expensive to purchase and maintain, yet only provide a limited number of conductors for routing instrumentation off the article and to a stationary data acquisition system. In addition to being limited to a small number of instruments, slip rings are prone to wear quickly, and introduce noise and other undesirable characteristics to the signal data. This led to the development of a system capable of recording high-density instrumentation, at high sample rates, on the test article itself, all while under extreme rotational stress. OSDAS is a fully functional PC-based system with 48 channels of 24-bit, high-sample-rate input channels, phase synchronized, with an onboard storage capacity of over 1/2-terabyte of solid-state storage. This recording system takes a novel approach to the problem of recording multiple channels of instrumentation, integrated with the test article itself, packaged in a compact/rugged form factor, consuming limited power, all while rotating at high turbine speeds.
Document ID
20120014092
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Pedings, Marc
(Optical Sciences Corp. Huntsville, AL, United States)
DeHart, Shawn
(Optical Sciences Corp. Huntsville, AL, United States)
Formby, Jason
(Optical Sciences Corp. Huntsville, AL, United States)
Naumann, Charles
(Optical Sciences Corp. Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
September 1, 2012
Publication Information
Publication: NASA Tech Briefs, September 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32908-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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