Grant: Discovery Grants Program - Individual
Ryerson University
$55,000.00
Paneled Morphing Skins for A Full Shape Adaptive System
FY 2021-22
Summary
A full shape adaptive system, such as morphing wings, should contain a morphing structure covered by a morphing skin. In my last DG research, a methodology for designing a morphing structure has been developed. In this proposed DG research, the goal is to develop a morphing skin that must fulfill motion requirement by morphing it along with a morphing structure yet withstand a surface load. The objective of this program is to spearhead a research into a new panel morphing skin that is made of segmented panels, inspired by fish scales. This research program is proposed under three pillars to investigate three types of new panel skins and develop associated design and analysis methodologies. The first pillar is to design, model and analyze a sliding panel skin that is devised as a set of small panels through loose connections joined by a telescopic interlock system allowing them to move relative to each other. Further, smart materials, such as shape memory polymer (SMP), are used to join these panels. A new method will be developed to model this skin system considering a morphing structure as a driving system and a morphing skin as a driven system. The key is to provide a proper constraint model that can truly represent the connections among adjacent panels. An effective numerical method will be developed to solve the panel motions because the computational complexity increases as the number of panels increase. The second pillar is to design, model and analyze a multi-stable panel morphing skin. Through special treatment metallic/composite materials would exhibit bi-stable configurations, which have been used for shape morphing but focusing on a single patch. Our research is to develop a multiple-patch system to form a morphing skin with multi-stable configurations. Different from the first pillar design, this pillar design has all the patches closely connected. Though each patch has two definite stable principal axes, they will behave differently after connection. The key is how to model the boundary conditions among adjacent patches and predict the overall skin shape. The third pillar is to design, model and analyze a continuum panel morphing skin. Currently continuum robots have been researched by utilizing long and slender rods to form for example a snake robot. Our research is to use large, thin and flexible panels that can be deformed to fulfill shape morphing requirement. Though this pillar design may be the best among the three for practical use, it has some limitations. The key is to model the entire skin system that is statically indeterminate and coupled with rigid motion. At the end of this program, all three designs will be summarized in terms of pros and cons that can be used to guide panel morphing skin designs for different applications. The proposed research program will help train a number of graduate students in this emerging area and strengthen collaborations with the Canadian aerospace manufacturing industry.
Program
Discovery Grants Program - Individual
Recipient
Location
Ontario, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
RGPIN-2020-04355
Name nom
Xi, Fengfeng
Department département
Aerospace Engineering - Aerospace Engineering
Organization id
43
Institution établissement
Ryerson University
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2021
Competition year année de concours
2020
Award amount
55000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
Discovery grants programs
Group fr
Programmes de subventions à la découverte
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Installment
inst:2
Partie
1
Nb partie
5
Application title
Paneled Morphing Skins for A Full Shape Adaptive System
Keyword
NSERC
Application summary
A full shape adaptive system, such as morphing wings, should contain a morphing structure covered by a morphing skin. In my last DG research, a methodology for designing a morphing structure has been developed. In this proposed DG research, the goal is to develop a morphing skin that must fulfill motion requirement by morphing it along with a morphing structure yet withstand a surface load. The objective of this program is to spearhead a research into a new panel morphing skin that is made of segmented panels, inspired by fish scales. This research program is proposed under three pillars to investigate three types of new panel skins and develop associated design and analysis methodologies. The first pillar is to design, model and analyze a sliding panel skin that is devised as a set of small panels through loose connections joined by a telescopic interlock system allowing them to move relative to each other. Further, smart materials, such as shape memory polymer (SMP), are used to join these panels. A new method will be developed to model this skin system considering a morphing structure as a driving system and a morphing skin as a driven system. The key is to provide a proper constraint model that can truly represent the connections among adjacent panels. An effective numerical method will be developed to solve the panel motions because the computational complexity increases as the number of panels increase. The second pillar is to design, model and analyze a multi-stable panel morphing skin. Through special treatment metallic/composite materials would exhibit bi-stable configurations, which have been used for shape morphing but focusing on a single patch. Our research is to develop a multiple-patch system to form a morphing skin with multi-stable configurations. Different from the first pillar design, this pillar design has all the patches closely connected. Though each patch has two definite stable principal axes, they will behave differently after connection. The key is how to model the boundary conditions among adjacent patches and predict the overall skin shape. The third pillar is to design, model and analyze a continuum panel morphing skin. Currently continuum robots have been researched by utilizing long and slender rods to form for example a snake robot. Our research is to use large, thin and flexible panels that can be deformed to fulfill shape morphing requirement. Though this pillar design may be the best among the three for practical use, it has some limitations. The key is to model the entire skin system that is statically indeterminate and coupled with rigid motion. At the end of this program, all three designs will be summarized in terms of pros and cons that can be used to guide panel morphing skin designs for different applications. The proposed research program will help train a number of graduate students in this emerging area and strengthen collaborations with the Canadian aerospace manufacturing industry.