Provided are a flat plate pulsating heat pipe having flexibility and having an improved sealing ability so as not to leak a working fluid therein, and a manufacturing method thereof. The flat plate pulsating heat pipe includes a base part having an upper surface or a lower surface which is plasma-treated, wherein the base part has a plurality of channels formed therein and both end portions of each of the channels are bent and connected to each other to form a closed-loop type or a closed type; and a pair of surface films bonded to an upper portion and a lower portion of the base part and bonded to each other at an outer portion of the base part to seal the channels.

Systems, methods, and apparatus for dual condenser loop heat pipes for satellites with sun-normal radiators are disclosed. In one or more embodiments, a disclosed method for a satellite thermal management system comprises heating, in an evaporator, a liquid to convert the liquid to a vapor. The method further comprises passively circulating within tubing, from the evaporator, the vapor to a first radiator not illuminated by a sun and to a second radiator illuminated by the sun. Also, the method comprises converting the vapor to the liquid when the vapor is within the first radiator not illuminated by the sun. Further, the method comprises passively circulating within the tubing, from the first radiator not illuminated by the sun, the liquid to the evaporator.

Methods, apparatuses, and systems are disclosed for flexible thermal ground planes. A flexible thermal ground plane may include a support member. The flexible thermal ground plane may include an evaporator region or multiple evaporator regions configured to couple with the support member. The flexible thermal ground plane may include a condenser region or multiple condenser regions configured to couple with the support member. The evaporator and condenser region may include a microwicking structure. The evaporator and condenser region may include a nanowicking structure coupled with the micro-wicking structure, where the nanowicking structure includes nanorods. The evaporator and condenser region may include a nanomesh coupled with the nanorods and/or the microwicking structure. Some embodiments may include a micromesh coupled with the nanorods and/or the microwicking structure.

Thermal management systems and corresponding use methods are described herein. A thermal management system includes components of a computing device. The computing device includes a housing. The housing includes an outer surface and an inner surface. The computing device also includes a heat generating component supported by the housing. The computing device includes a phase change device adjacent or physically connected to the heat generating component. The phase change device includes a first side and a second side. The first side is closer to the heat generating component than the second side. The second side is opposite the first side. The phase change device is compressible, such that when a force is applied to the outer surface of the housing, the inner surface of the housing flexes towards the second side of the phase change device and the phase change device is compressed.

Embodiments described herein may include apparatuses, systems and/or processes to provide a cooling apparatus that includes a first heatsink, a second movable heatsink and a flexible thermal conductor physically and thermally coupled with the first and second heatsinks, where the flexible thermal conductor is to flex and remain thermally coupled with the first heatsink and the second heatsink, when the second heatsink is moved relative to the first heatsink. The first heatsink may be coupled to a heat source such as a processor that may be coupled with a PCB. Also, the movable heatsink may allow access to components, such as dual in-line memory modules (DIMMs) that are next to the first heatsink and under the movable second heatsink. Other embodiments may be described and/or claimed.

Methods, apparatuses, and systems are disclosed for flexible thermal ground planes. A flexible thermal ground plane may include a support member. The flexible thermal ground plane may include an evaporator region or multiple evaporator regions configured to couple with the support member. The flexible thermal ground plane may include a condenser region or multiple condenser regions configured to couple with the support member. The evaporator and condenser region may include a microwicking structure. The evaporator and condenser region may include a nanowicking structure coupled with the micro-wicking structure, where the nanowicking structure includes nanorods. The evaporator and condenser region may include a nanomesh coupled with the nanorods and/or the microwicking structure. Some embodiments may include a micromesh coupled with the nanorods and/or the microwicking structure.

A heat spreader apparatus, testing system, method may be used to test an electronic device. The heat spreader may include a hollow housing. The hollow housing may define an interior chamber. The hollow housing may include a contact surface. The heat spreader may include a working fluid. The working fluid may be included in the interior chamber. The hollow housing may be configured to be physically compliant. The hollow housing may be physically compliant such that the hollow housing conforms to the shape of a testing surface in response to an applied pressure. The testing surface may be a top surface of a semiconductor. The testing surface may be curved or otherwise lack uniformity. The hollow housing may conform to the curvature or lack of uniformity of the testing surface such that minimal gaps exist between the hollow housing and the surface.

A heat pipe has an evaporator portion, a condenser portion, and at least one flexible portion that is sealingly coupled between the evaporator portion and the condenser portion. The flexible portion has a flexible tube and a flexible separator plate held in place within the flexible tube so as to divide the flexible tube into a gas-phase passage and a liquid-phase artery. The separator plate and flexible tube are configured such that the flexible portion is flexible in a plane that is perpendicular to the separator plate.

Methods, apparatuses, and systems are disclosed for flexible thermal ground planes. A flexible thermal ground plane may include a support member. The flexible thermal ground plane may include an evaporator region or multiple evaporator regions configured to couple with the support member. The flexible thermal ground plane may include a condenser region or multiple condenser regions configured to couple with the support member. The evaporator and condenser region may include a microwicking structure. The evaporator and condenser region may include a nanowicking structure coupled with the micro-wicking structure, where the nanowicking structure includes nanorods. The evaporator and condenser region may include a nanomesh coupled with the nanorods and/or the microwicking structure. Some embodiments may include a micromesh coupled with the nanorods and/or the microwicking structure.

An apparatus includes a structure configured to receive and transport thermal energy. The structure includes one or more materials configured to undergo a solid-solid phase transformation at a specified temperature or in a specified temperature range. The one or more materials form a heat input region configured to receive the thermal energy and a cold sink interface region configured to reject the thermal energy. The structure also includes one or more thermal energy transfer devices embedded in at least part of the one or more materials. The one or more thermal energy transfer devices are configured to transfer the thermal energy throughout the one or more materials and at least partially between the heat input region and the cold sink interface region. The one or more materials are also configured to absorb and store excess thermal energy in response to a temperature excursion associated with a thermal transient event and to release the stored thermal energy after the thermal transient event.