Published July 2014 | Version v1
Journal article

Biomimetic FAA-certifiable, artificial muscle structures for commercial aircraft wings

  • 1. University of Kansas Aerospace Engineering Department (United States)
  • 2. College of Biological Sciences, University of Minnesota, Minneapolis (United States)

Description

This paper is centered on a new form of adaptive material which functions much in the same way as skeletal muscle tissue, is structurally modeled on plant actuator cells and capable of rapidly expanding or shrinking by as much as an order of magnitude in prescribed directions. Rapid changes of plant cell shape and sizes are often initiated via ion-transport driven fluid migration and resulting turgor pressure variation. Certain plant cellular structures like those in Mimosa pudica (sensitive plant), Albizia julibrissin (Mimosa tree), or Dionaea muscipula (Venus Flytrap) all exhibit actuation physiology which employs such turgor pressure manipulation. The paper begins with dynamic micrographs of a sectioned basal articulation joint from A. julibrissin. These figures show large cellular dimensional changes as the structure undergoes foliage articulation. By mimicking such structures in aircraft flight control mechanisms, extremely lightweight pneumatic control surface actuators can be designed. This paper shows several fundamental layouts of such surfaces with actuator elements made exclusively from FAA-certifiable materials, summarizes their structural mechanics and shows actuator power and energy densities that are higher than nearly all classes of conventional adaptive materials available today. A sample flap structure is shown to possess the ability to change its shape and structural stiffness as its cell pressures are manipulated, which in turn changes the surface lift-curve slope when exposed to airflows. Because the structural stiffness can be altered, it is also shown that the commanded section lift-curve slope can be similarly controlled between 1.2 and 6.2 rad−1. Several aircraft weight reduction principles are also shown to come into play as the need to concentrate loads to pass through point actuators is eliminated. The paper concludes with a summary of interrelated performance and airframe-level improvements including enhanced gust rejection, load alleviation, ride quality, fatigue life and flight safety. (papers)

Availability note (English)

Available from http://dx.doi.org/10.1088/0964-1726/23/7/074011

Additional details

Publishing Information

Journal Title
Smart Materials and Structures (Print)
Journal Volume
23
Journal Issue
7
Journal Page Range
[15 p.]
ISSN
0964-1726

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
47050873
Subject category
S42: ENGINEERING; S36: MATERIALS SCIENCE;
Descriptors DEI
ACTUATORS; AIRCRAFT; ANIMAL TISSUES; CONTROL SYSTEMS; ENERGY DENSITY; FATIGUE; FLEXIBILITY; IONS; MECHANICS; MUSCLES; PLANT CELLS; PLANT TISSUES; STRUCTURAL MODELS; SURFACES
Descriptors DEC
BODY; CHARGED PARTICLES; MECHANICAL PROPERTIES; TENSILE PROPERTIES