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Programmable controller system for wind tunnel diversion vanesA programmable controller (PC) system automatic sequence control, which acts as a supervisory controller for the servos, selects the proper drives, and automatically sequences the vanes, was developed for use in a subsonic wind tunnel. Tunnel modifications include a new second test section (80 ft x 100 ft with a maximum air speed capability of 110 knots) and an increase in maximum velocity flow from 200 knots to 300 knots. A completely automatic sequence control is necessary in order to allow intricate motion of the 14 triangularly arranged vanes which can be as large as 70 ft high x 35 ft wide and which require precise acceleration and deceleration control. Rate servos on each drive aid in this control, and servo cost was minimized by using four silicon controlled rectifier controllers to control the 20 dc drives. The PC has a programming capacity which facilitated the implementation of extensive logic design. A series of diagrams sequencing the vanes and a block diagram of the system are included.
Document ID
19820058311
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
King, R. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Research And Support Facilities (Air)
Meeting Information
Meeting: International Instrumentation Symposium
Location: Las Vegas, NV
Start Date: May 3, 1982
End Date: May 6, 1982
Accession Number
82A41846
Distribution Limits
Public
Copyright
Other

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