Kenneth C. Cheung - Boston MA, US Ara Knaian - Newton MA, US Neil Gershenfeld - Somerville MA, US
Assignee:
Massachusetts Institute of Technology - Cambridge MA
International Classification:
G06F 19/00 B25J 17/00
US Classification:
700245, 7449005
Abstract:
Cellular automotion digital material is useable for rapid prototyping and fabrication of continuous string conformations and two- or three-dimensional shapes through actuation of a string, surface, or volume composed of identical discrete units. Each unit is an actuated joint having a single degree of freedom. The actuated joint includes a two-part actuator having an inner active portion and an outer passive portion that are controllably rotatable relative to each other, the outer portion being configured to fit within the housing of an adjacent cellular automotion unit, and a linkage element that includes a main strut and a housing and is connected to the actuator by a pin connector. The housing is configured to house the actuator of an adjacent cellular automation unit, and the opening in the strut is rotated about the axis of symmetry of the cellular automotion unit relative to the opening in the housing so that the alignment of the cellular automotion unit will be rotated with respect to the alignment of any adjacent unit. The cellular automotion unit may include an on-board processor for controlling actuation of the cellular automotion unit.
Neil Gershenfeld - Somerville MA, US Kenneth Cheung - Boston MA, US
Assignee:
MASSACHUSETTS INSTITUTE OF TECHNOLOGY - Cambridge MA
International Classification:
B32B 3/06 B23P 11/00 B32B 5/02
US Classification:
428 99, 29428
Abstract:
In exemplary implementations of this invention, a digital material comprising many discrete units is used to fabricate a sparse structure. The units are reversibly joined by elastic connections. Each unit comprises fiber-reinforced composite material. Each unit is small compared to the sparse structure as a whole. Likewise, in a sparse structure made from this digital material, the number of types of units is small compared to the total number of units. The digital material is anisotropic. This anisotropy may be due to different fiber orientations within each unit. Furthermore, different units in a single sparse structure may be oriented in different directions and in different, non-parallel planes. In some cases, the digital material is reinforced with carbon fibers, and connections between units are stronger than the units themselves. The small discrete units may be assembled into a strong, lightweight sparse structure, such as an airframe.
Neil Gershenfeld - Somerville MA, US Nadya Peek - Cambridge MA, US Kenneth Cheung - Boston MA, US David Watson - Newtownabbey, GB
Assignee:
MASSACHUSETTS INSTITUTE OF TECHNOLOGY - Cambridge MA
International Classification:
B29C 39/00
US Classification:
700198
Abstract:
In exemplary implementations of this invention, a network of nodes controls and senses the cure of a thermosetting plastic in a component that is made of fiber composite material. The network comprises multiple nodes, which are separated spatially from each other. Each of the nodes, respectively, comprises a heat transfer device for actively transferring thermal energy, a temperature sensor for taking local temperature measurements, and a processor. In each of the nodes, respectively: (a) the processor locally performs closed loop control over the temperature of the heat transfer device, and (b) the closed loop control is based at least in part on the local temperature measurements and on estimated or measured input current to the heat transfer device.
Charles Fracchia - Cambridge MA, US Neil Gershenfeld - Cambridge MA, US Kenneth Cheung - Freehold NJ, US
International Classification:
C07H 21/04
US Classification:
514777, 536 231, 530395, 5303911, 422149
Abstract:
In exemplary implementations of this invention, hierarchical, nanometer-precise assembly is performed: A first structural unit is attached to a solid substrate in a first fluidic flow. A second structural unit is attached to the first structural unit in a second fluidic flow, a third structural unit is attached to the second structural unit in a third fluidic flow, and so on, until a target structure comprising the structural units is assembled. The first, second, third and so on fluidic flows are separate and occur in order in a temporal sequence. During the temporal sequence, a specific permutation of nucleobases is used repeatedly, in separate fluidic flows which occur at different times, to form multiple attachments between structural units in an assembly. The assembled target structure is removed from the solid substrate. Attachments between the structural units may be formed by nucleobase pairing.
Kenneth C. Cheung - Boston MA, US Neil Adam Gershenfeld - Somerville MA, US
Assignee:
MASSACHUSETTS INSTITUTE OF TECHNOLOGY - Cambridge MA
International Classification:
B32B 3/06 E04B 1/02 B64C 1/00
US Classification:
428 341, 428 99, 29428
Abstract:
Digital flexural materials are kits of discrete parts that can be assembled into a lattice structure to produce functionally useful assemblies. Digital flexural materials enable design of materials with many small and inexpensive flexures that combine in a lattice geometry that permits deformation without compromising the strength of the assembly. The number of types of parts in a kit is small compared to the total number of parts. A product constructed from digital flexural materials comprises a set of discrete units that are assembled into the structure according to a lattice geometry, with a majority of the units being reversibly connected to at least two other units in the set according to the lattice geometry, and wherein, in response to loading of the structure, a reversible deformation of at least part of the structure occurs. An automated process may be employed for constructing a product from digital flexural materials.
Method For Discrete Assembly Of Cuboctahedron Lattice Materials
- 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
Assignee:
Massachusetts Institute of Technology - Cambridge MA
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.
Sarah Hovsepian - Cambridge MA, US Neil Adam Gershenfeld - Somerville MA, US Kenneth Cheung - Boston MA, US
Assignee:
MASSACHUSETTS INSTITUTE OF TECHNOLOGY - Cambridge MA
International Classification:
G05B 19/4097
Abstract:
A digital material skin is made of a set of discrete units with a finite set of parts and joints. The discrete units are assembled into a layer according to a regular geometry, with each of the discrete units being reversibly connected to at least one other unit in the set. The reversibly connected set of units forms an exterior structure surface that is larger than the individual discrete units. Digital material skins may be used to construct any shape or interior volume, whether regular or amorphous. The skin surface may be enclosed or open. The skin may rely on an interior digital material structure for support or may be self-supported. The skin may be part of a larger assembly or apparatus, enclosing an interior volume or structure.
Massachusetts Institute of Technology (Mit) Sep 2012 - Sep 2013
Post-Doctoral Associate
Nasa Sep 2012 - Sep 2013
Research Scientist and Engineer and Designer
Massachusetts Institute of Technology (Mit) Jun 2007 - Aug 2012
Ph.d Student and Research Assistant
Massachusetts Institute of Technology (Mit) Jun 2005 - May 2007
Master's Student and Research Assistant
Fablab Jun 2005 - May 2007
Fab Lab Helper
Education:
Massachusetts Institute of Technology 2007 - 2012
Doctorates, Doctor of Philosophy, Philosophy
Massachusetts Institute of Technology 2005 - 2007
Master of Science, Masters
Cornell University 2000 - 2005
Bachelor of Architecture, Bachelors
Apr 2014 to 2000 Online Sales PersonUnited Accounting & Tax
Nov 2009 to 2000 Accounting/ BookkeeperMillion Dollar Baby Montebello, CA Mar 2013 to Apr 2014 IT SpecialistMillion Dollar Baby Montebello, CA Aug 2010 to Mar 2013 Accounts Receivable SpecialistVaco Technology Services Torrance, CA Aug 2009 to Nov 2009 Helpdesk EngineerTurner Techtronics Burbank, CA Aug 2007 to Aug 2009 Helpdesk AnalystMechanized Propulsion Systems Rosamond, CA Jul 2007 to Dec 2008 Web Page DeveloperTransportation Security Administration San Jose, CA Aug 2005 to Mar 2007 Transportation Security Officer
Education:
East Los Angeles College Monterey Park, CA 2009 to 2011 AccountingSan Jos State University San Jose, CA 2003 to 2006 BS in Computer SciencePasadena City College Pasadena, CA 2001 to 2003 AA in Computer Science
Youtube
The Motion of Life | Lai Chi-wai & Kenneth Ch...
As a world-leading spine surgeon, Prof. Kenneth Cheung has spent years...
In tandem, although such changes do bring about a certain degree of uncertainty, the naming of former company vice president of finance, Kenneth Cheung as the new chief accounting officer, as well as the announced intention to name new personnel to the positions of general counsel, chief compliance
Date: Dec 11, 2024
Category: Business
Source: Google
MIT and NASA engineers demonstrate a new kind of airplane wing
in the design and manufacturing of future aircraft. The new wing design was tested in a NASA wind tunnel and is described today in a paper in the journal Smart Materials and Structures, co-authored by research engineer Nicholas Cramer at NASA Ames in California; MIT alumnus Kenneth Cheung SM '07 Ph.
Date: Apr 01, 2019
Category: Science
Source: Google
MIT and NASA engineers demonstrate a new kind of airplane wing
The new wing design was tested in a NASA wind tunnel and is described today in a paper in the journal Smart Materials and Structures, co-authored by research engineer Nicholas Cramer at NASA Ames in California; MIT alumnus Kenneth Cheung SM 07 PhD 12, now at NASA Ames; Benjamin Jenett, a graduate
Date: Apr 01, 2019
Category: Science
Source: Google
Researchers invent a new approach to assembling big structures out of LEGO ...
According to MITnews, the small blocks can be mass-produced. In fact, Gershenfeld andpostdoc Kenneth Cheung are creating a robotic system to turn them into airplane parts and other components of large structures. A robot will likely move very slowly over the surface of a forming structure, snapping
Date: Aug 17, 2013
Category: Sci/Tech
Source: Google
A Tiny Transforming Robot Inspired by Protein (and Junkyard Magnets)
Knaian and his co-designers, Neil Gershenfeld, head of MITs Center for Bits and Atoms, and Kenneth Cheung, call their invention the electropermanent motor, and its already getting attention from industry. Theyre working with the precision device maker Moog (MOG/A) to design airplane flap contro
The device was conceived by Neil Gershenfeld, head of MITs Center for Bits and Atoms, visiting scientist Ara Knaian and postdoctoral associate Kenneth Cheung, and is described in a paper presented recently at the 2012 Intelligent Robots and Systems conference. Its key feature, Gershenfeld says: It