Toyota Motor Engineering & Manufacturing North America, Inc.

University of Illinois

University of Connecticut

Toyota Jidosha Kabushiki Kaisha

Purdue Research Foundation

University System of Maryland

Vanderbilt University

The Ohio State University

Ohio State Innovation Foundation

Toyota Motor North America, Inc.

North America, Inc.

Toyota Manufacturing Engineering & Manufacturing North America, Inc.

Shailesh N Joshi

Ercan Mehmet Dede

Feng Zhou

Ercan Mehment Dede

Danny J Lohan

Yanghe Liu

Naoya Take

Paul Vannest Braun

Masao Noguchi

Umesh N Gandhi

Hitoshi Fujioka

Ali M Bazzi

Gaurav Singhal

Hiroshi Ukegawa

Weiqiang Chen

Lingyi Zhang

Julia Kohanek

Shohei Suenaga

Matthew Joseph Rau

Krishna R Pattipati

Krishna Pattipatti

Kai-Wei Lan

Donald Mcmenemy

Debasish Banerjee

Brian J Pinkelman

Yuyang Song

Suresh V Garimella

Yuji Fukuoka

Vishnu Baba Sundaresan

Mayur Prakash Gaikwad

Vijay Venkatesh

Danil V Prokhorov

Ryohei Tsuruta

Songtao Wu

Chi-Ming Wang

Tianzhu Fan

Shohei Nagai

Jaewook Lee

F Patrick McCluskey

John Kaminski

Hannes Martin Hinrich Greve

Srivatsava Krishnan

Joshua Sean Kuhlmann

Jae Seung Lee

Taehwa Lee

Masanori Ishigaki

Ravi Rajamani

Jongwon Shin

Ziqi Yu

Muhamed K Farooq

Nenad Miljkovic

Khoa Vo

Piran Ravichandran Kidambi

Kyosuke N Miyagi

Fa Chen

Srivathsan Sudhakar

Hiroshi N Ukegawa

Peifu Cheng

Shashi Honnikoppa

Srivathsan Sudhaker

Dajie Xie

Krishna Pattipati

Qian Yang

Raymond P Viviano

The present disclosure is directed to systems and methods for cooling electronic devices. The system comprises a pump, a distribution manifold fluidly coupled to the pump, one or more capillary coolers fluidly coupled to the distribution manifold, one or more electronic devices coupled to the one or more capillary coolers, a vapor line fluidly coupled to the one or more capillary coolers, and a condenser comprising an inlet and an outlet, wherein the inlet is fluidly coupled to the vapor line and the outlet is fluidly coupled to the pump.

Systems and methods for cooling electronic devices

The present disclosure is directed to systems and methods for cooling an electric aircraft. The system comprises an electronic device, a casing, a fin, and at least one PHP. The casing comprises an inner surface. A PHP may be coupled to the inner surface. The fin comprises a fin interior cavity. A PHP may be embedded within the fin interior cavity. The same PHP may be both coupled to the casing inner surface and embedded within the fin interior cavity, or there may be a plurality of fins such that at least one fin is coupled to the casing inner surface and at least one fin is embedded within the fin interior cavity. The portion of the PHP closest to the electronic device comprises an evaporator section and the portion of the PHP furthest from the electronic device comprises a condenser section.

Systems and methods for cooling an electric aircraft

The present disclosure is directed to systems and methods for cooling an electric aircraft. The system comprises an electronic device, a casing, at least one fin, and at least one PHP. The electronic device can generate heat. The electronic device can be housed within the casing. The fin can be attached to the outer wall of the casing. The PHP can be embedded within the fin, such that an evaporator section of the PHP is closest to the heat source and the condenser section of the PHP is furthest from the heat source. The PHP can also be placed within the casing. In some embodiments, the casing can have a plurality of slots. The fin can be shaped such that a single fin may slide into a pair of slots and come to rest adjacent to the casing, wherein a PHP can be embedded within the fin.

Methods, apparatuses and systems provide technology that includes a first transistor, a second transistor stacked on the first transistor, at least one electrical conductor that is positioned between the first and second transistors and electrically connected to the first and second transistors, and a busbar that is electrically connected to the first and second transistors through the at least one electrical conductor.

Power electronics assembly having vertically stacked transistors

A morphing structure includes a deployable aerodynamic origami structure with an outer covering having a plurality of creases, a tether attached to the deployable origami structure, and a light-responsive polymer disposed on one or more of the creases of the outer covering. The light-responsive polymer is configured to change shape when activated by a light and the deployable origami structure configured to change from a first shape to a second shape different than the first shape when the light-responsive polymer is activated. In some variations, the morphing structure also includes at least one heating element disposed on one or more of the creases of the outer covering and the at least one heating element is configured to heat the light-responsive polymer such that the shape of the deployable aerodynamic origami structure moves from the second shape to the first shape.

Morphing origami structures with light-responsive polymers

Systems, methods, and other embodiments described herein relate to predicting anomalous operation of a device and an associated remaining useful life (RUL) estimation. In one embodiment, a method includes acquiring usage information about the operation of an electronic device. The method includes determining whether the usage information indicates the presence of an anomaly in the operation of the electronic device according to an anomaly model. The method includes, responsive to detecting the anomaly, determining a remaining useful life (RUL) for the electronic device according to a RUL model. The method includes providing the RUL estimate.

Remaining useful life determination for power electronic devices

Systems, methods, and other embodiments described herein relate to charging a battery of an electric vehicle while the electric vehicle is hovering. In one embodiment, a method includes, responsive to determining that an electric vehicle does not include a receiver pad, inserting the receiver pad into the electric vehicle that is hovering in the air at a charging station. The method includes determining a space above a transmitter pad for the electric vehicle to hover based, at least in part, on a location and a size of the transmitter pad. The method includes charging a battery to a threshold value through the receiver pad.

Charging a battery of an electric vehicle hovering in the air

A dynamic wireless power transfer system can include a dynamic wireless power transfer transmission system and a dynamic wireless power transfer reception system. The dynamic wireless power transfer transmission system can include a signal receiver, an array of coils of conductors, an array of switches, and a controller. The dynamic wireless power transfer reception system can include a signal transmitter and an array of coils of conductors. The signal transmitter can be configured to transmit, to the signal receiver, a signal. The signal can include information indicative of a size of the array of coils of conductors of the dynamic wireless power transfer reception system. The array of switches can be configured to connect an alternating current source to the array of coils of conductors of the dynamic wireless power transfer transmission system. The controller can control, according to the information, positions of switches of the array of switches.

Configurable dynamic wireless power transfer transmission system

A light apparatus includes an optical member, composed of an elastically deformable material, having a reflective surface to reflect light. The optical member moveable between a first state in which the reflective surface has a first structural shape, and a plurality of second states in which the reflective surface has a second structural shape different than the first structural shape. Elastically deformable position adjustment members are operable to move the optical member between the first state and the plurality of second states. The elastically deformable position adjustment members have one or more photochromatic regions that are moveable in response to exposure to UV light. Light sources are operable to selectively emit illuminating UV light in a direction that contacts the one or more photochromatic regions to thereby adjust an orientation of the optical member in a manner which changes a direction of light reflected by the optical member.

Dynamic adjustment of flexible mirror using photochromatic material

A morphing aerodynamic structure includes a body with an outer covering, a bridle attached to the body, and a light-response polymer disposed on at least one of the outer covering and the bridle. The light-responsive polymer is configured to change shape when illuminated with a laser such that at least one of an angle of attack, roll, pitch and yaw of the morphing aerodynamic structure is at least partially controlled without the use of a mechanical or pneumatic control unit.

Morphing structures with light-responsive polymers

A louvre system controls a flow of cooling air to a heat-generating element mounting inside a wing of an aircraft. The louvre system includes a louvre operably connected to the wing and structured to be rotatable to control airflow through an air intake of the wing into an interior of the wing. A louvre actuation mechanism is operably connected to the louvre and configured to control rotation of the louvre. A memory is communicably coupled to a processor and stores a louvre control module configured to autonomously control operation of the louvre actuation mechanism to control rotation of the louvre responsive to a temperature of a heat-generating element mounted in the wing interior.

Cooling system for aircraft components

Systems and methods for adjusting one or more properties of a deformable lens are described herein. The deformable lens includes a photoswitch material that, when irradiated by a radiation, causes a curvature of a surface of the deformable lens to change from a first curvature to a second curvature based on the intensity of the radiation.

System and method for adjusting one or more properties of a deformable lens

A transient liquid phase (TLP) composition includes a plurality of first high melting temperature (HMT) particles, a plurality of second HMT particles, and a plurality of low melting temperature (LMT) particles. Each of the plurality of first HMT particles have a core-shell structure with a core formed from a first high HMT material and a shell formed from a second HMT material that is different than the first HMT material. The plurality of second HMT particles are formed from a third HMT material that is different than the second HMT material and the plurality of LMT particles are formed from a LMT material. The LMT particles have a melting temperature less than a TLP sintering temperature of the TLP composition and the first, second, and third HMT materials have a melting point greater than the TLP sintering temperature.

Transient liquid phase bonding compositions and power electronics assemblies incorporating the same

A two-phase cold plate that includes a manifold body having a fluid inlet and a fluid outlet each fluidly coupled to a fluid pathway housed within the manifold body and a vaporization structure housed within the manifold body such that the fluid pathway is disposed over the vaporization structure. The vaporization structure includes a cavity cover, a porous surface, a vapor cavity disposed between the cavity cover and the porous surface, and one or more porous feeding posts extending between the cavity cover and the porous surface. The one or more porous feeding posts fluidly coupled the fluid pathway with the porous surface of the vaporization structure and the porous surface includes a plurality of nucleation sites configured to induce vaporization of a cooling fluid and facilitate vapor flow into the vapor cavity of the vaporization structure.

Power electronics systems comprising a two-phase cold plate housing a vaporization structure

Evaporator assemblies, vapor chamber assemblies, and methods for fabricating a vapor chamber are disclosed. In one embodiment, an evaporator assembly for a vapor chamber includes an evaporator surface, an array of posts extending from the evaporator surface, and an array of vapor vents within the evaporator surface. Each vapor vent of the array of vapor vents is configured as a depression within the evaporator surface. The evaporator assembly further includes a porous layer disposed on the evaporator surface, the array of posts, and the array of vapor vents.

Evaporator assemblies, vapor chambers, and methods for fabricating vapor chambers

Growing community of inventors

Ann Arbor, MI, United States of America

Shailesh N Joshi