The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 01, 2024

Filed:

Mar. 09, 2020
Applicant:

United States of America As Represented BY the Administrator of Nasa, Washington, DC (US);

Inventors:

Benjamin Eric Jenett, Cambridge, MA (US);

Neil Gershenfeld, Cambridge, MA (US);

Sean Swei, Moffett Field, CA (US);

Nicholas Cramer, Moffett Field, CA (US);

Kenneth Cheung, Moffett Field, CA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/48 (2006.01); B64C 3/26 (2006.01); B64C 3/52 (2006.01); C08K 7/14 (2006.01); C08L 79/08 (2006.01); B64C 3/54 (2006.01);
U.S. Cl.
CPC ...
B64C 3/48 (2013.01); B64C 3/26 (2013.01); B64C 3/52 (2013.01); C08K 7/14 (2013.01); C08L 79/08 (2013.01); B64C 2003/543 (2013.01);
Abstract

A shape-morphing ultralight structure using materials that dramatically increase the efficiency of load-bearing aerostructures that includes a programmable material system applied as a large-scale, ultralight, and conformable (shape-morphing) aeroelastic structure. The use of a modular, lattice-based, ultralight material results in stiffness and density typical of an elastomer. This, combined with a building block-based manufacturing and configuration strategy, enables the rapid realization of new adaptive structures and mechanisms. The heterogeneous design with programmable anisotropy allows for enhanced elastic and global shape deformation in response to external loading, making it useful for tuned fluid-structure interaction. The present invention demonstrates an example application experiment using two building block types for the primary structure of a 4.27 m wingspan aircraft with spatially programed elastic shape morphing to increase aerodynamic efficiency.


Find Patent Forward Citations

Loading…