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A fast acting electrical servo for the actuation of full span, Fowler-type wing flaps in DLC applications: A detail design studyThe philosophy and detail design of an electro-mechanical actuator for Fowler-type wing flaps which have a response time constant of 0.025 seconds are described. A conventional electrical servomotor with a power rating twice the maximum power delivered to the load is employed along with adaptive, gain-scheduled feedback and various logic circuits, including one to remove electrical excitation from the motor during extended periods when no motion of the flap is desired.
Document ID
19720020377
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smetana, F. O.
(North Carolina State Univ. Raleigh, NC, United States)
Montoya, R. J.
(North Carolina State Univ. Raleigh, NC, United States)
Carden, R. K.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publisher: NASA
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-CR-2059
Report Number: NASA-CR-2059
Accession Number
72N28027
Funding Number(s)
PROJECT: RTOP 736-05-10-01
CONTRACT_GRANT: NGR-34-002-086
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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