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Design and Control of a Proof-of-Concept Active Jet Engine Intake Using Shape Memory Alloy ActuatorsThe design and control of a novel proof-of-concept active jet engine intake using Nickel-Titanium (Ni-Ti or Nitinol) shape memory alloy (SMA) wire actuators is used to demonstrate the potential of an adaptive intake to improve the fuel efficiency of a jet engine. The Nitinol SMA material is selected for this research due to the material's ability to generate large strains of up to 5 percent for repeated operations, a high power-to-weight ratio, electrical resistive actuation, and easy fabrication into a variety of shapes. The proof-of-concept engine intake employs an overlapping leaf design arranged in a concentric configuration. Each leaf is mounted on a supporting bar that rotates upon actuation by SMA wires electrical resistive heating. Feedback control is enabled through the use of a laser range sensor to detect the movement of a leaf and determine the radius of the intake area. Due to the hysteresis behavior inherent in SMAs, a nonlinear robust controller is used to direct the SMA wire actuation. The controller design utilizes the sliding-mode approach to compensate for the nonlinearities associated with the SMA actuator. Feedback control experiments conducted on a fabricated proof-of-concept model have demonstrated the capability to precisely control the intake area and achieve up to a 25 percent reduction in intake area. The experiments demonstrate the feasibility of engine intake area control using the proposed design.
Document ID
20040082466
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Song, Gangbing
(Houston Univ. TX, United States)
Ma, Ning
(Houston Univ. TX, United States)
Penney, Nicholas
(Ohio Aerospace Inst. Brook Park, OH, United States)
Barr, Todd
(Jackson and Tull, Inc. Cleveland, OH, United States)
Lee, Ho-Jun
(NASA Glenn Research Center Cleveland, OH, United States)
Arnold, Steven M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2004
Subject Category
Structural Mechanics
Report/Patent Number
E-14618
NASA/TM-2004-213124
Funding Number(s)
CONTRACT_GRANT: NSF 00-93737
CONTRACT_GRANT: NAG3-2827
WBS: WBS 22-708-01-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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