Affiliation:
1. Aerospace Mechanics Division, University of Dayton Research Institute, Dayton, OH 45469-0013, USA,
2. Air Combat Command, Langley AFB, VA 23665, USA
Abstract
In this study, the optimal location of a distributed network of actuators within a morphing wing scissor mechanism is investigated. The analysis begins by developing a mechanical understanding of a single cell representation of the mechanism. This cell contains four linkages connected by pin joints, a single actuator, two springs to represent the bi-directional behavior of a flexible skin, and an external load. Equilibrium equations are developed using static analysis and the principle of virtual work equations. An objective function is developed to maximize the efficiency of the unit/multiple cell model. It is defined as useful work over input work. There are two constraints imposed on this problem. The first is placed on force transferred from the external source to the actuator. It should be less than the blocked actuator force to ensure the mechanism moves in the desired direction. The other is the requirement that the ratio of output displacement over input displacement, i.e., geometrical advantage (GA), of the cell is larger than a prescribed value. Sequential quadratic programming is used to solve the optimization problem. This process suggests a systematic approach to identify an optimum location of an actuator and to avoid the selection of location by trial and error. Preliminary results show that optimum locations of an actuator can be selected out of feasible regions according to the requirements of the problem, such as a higher GA, a higher efficiency, or a smaller transferred force from external force. Results include analysis of single and multiple cell wing structures and some experimental comparisons.
Subject
Mechanical Engineering,General Materials Science
Cited by
13 articles.
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