A heat exchanger which may be used in an engine, such as a vehicle engine for an aircraft or orbital launch vehicle. is provided. The heat exchanger may be configured as generally drum-shaped with a multitude of spiral sections, each containing numerous small diameter tubes. The spiral sections may spiral inside one another. The heat exchanger may include a support structure with a plurality of mutually axially spaced hoop supports, and may incorporate an intermediate header. The heat exchanger may incorporate recycling of methanol or other antifreeze used to prevent blocking of the heat exchanger due to frost or ice formation.

A header (10) for a heat exchanger, in particular for a charge air cooler, comprising an opening plane (12) with plurality of openings (14) for attachment of tubes, a collar (13) encircling the perimeter of the opening plane (12) and protruding at least partially above the opening plane (12), wherein the header (10) further comprises guiding protrusions (11a, 11b) located along inner perimeter of the collar (13) adjacent to said openings (14) and configured to guide the tubes into the openings (14) upon insertion, wherein the openings (14) have substantially rectangular shape with longer sides (14a) and shorter sides (14b) and are arranged in series along their longer sides (14a), wherein a first group of guiding protrusions (11a) is located adjacent the longer sides (14a) of the openings (14), while a second group of guiding protrusions (11b) is located adjacent the shorter sides (14b) of the openings (14).

In one instance, an isolator for a heating, ventilating, and cooling (HVAC) system is provided that is a formed plastic member that is disposed between dissimilar metals of the bottom of the condenser and a base pan that supports the condenser or between two dissimilar metals of another HVAC heat exchanger. The isolator separates the two dissimilar metals involved from each of those components and also provides gaps or apertures to drain any water that otherwise might become standing water that potentially causes oxidation or increased oxidation. Other aspects are disclosed.

An air-cooled heat exchanger is connectable between an upstream fluid source and a downstream fluid destination by a plurality of external pipes having connection ends arranged in one or more external pipe connection configurations. The air-cooled heat exchanger has a cooling tubes assembly that includes a plurality of headers, a plurality of intermediate pipes connected to the plurality of headers, and a modular manifold system that connects the plurality of intermediate pipes to the plurality of external pipes. The modular manifold system includes a plurality of pipe elbows each connected to a corresponding one of the plurality of intermediate pipes, and one or more trays. Each of the plurality of pipe elbows is retained within the one or more trays in a configuration that matches the one or more external pipe connection configurations.

A heat transfer element is disclosed. The heat transfer element can be configured to directly bond to a metal surface of an element. The heat transfer element can include a chamber that is defined at least in part by a housing that has a metal portion. The heat transfer element can also include a phase change material disposed in the chamber. The phase change material can be in thermal communication with the metal portion. The Heat transfer element can be bonded to the element to define a bonded structure.

The present invention relates to a plate heat exchanger system with a plate heat exchanger (10) comprising an inlet (11) and an outlet (12) of a primary circuit (13), an inlet (14) and an outlet (15) of a secondary circuit (16), at least one plate (17) separating the two circuits in a housing of the plate heat exchanger from each other, and preferably a pipe which connects the primary circuit to a heating device. For improving heat transfer between the primary circuit (13) and the secondary circuit (16), the plate heat exchanger (10) is according to the invention in the direction of gravity (G) arranged such that the plane (E), in which the plate (17) is located, is inclined relative to the gravity vector (G) and the horizontal (H).

Phased array antennas, such as a multi-function aperture, are limited in performance and reliability by traditional air-cooled thermal management systems. A fuel-cooled multi-function aperture passes engine fuel through heat exchangers that surround the multi-function aperture to provide better heat transfer than can be achieved through air cooling systems. The increased heat transfer and thermal management results in a multi-function aperture with improved performance and reliability.

A heat exchanger assembly has a frame including: a plurality of legs; first and second lower transversal members extending perpendicular to and interconnecting the legs; a plurality of upstanding members extending upwardly from respective ones of the legs, a lower end of each upstanding member being connected to a corresponding leg at a junction therebetween; an upper transversal member interconnecting upper ends of the upstanding members; and an upper frame assembly. The frame components are weldlessly connected to one another. First and second heat exchanger panels exchange heat with air pulled into the heat exchanger assembly and are disposed in a V-configuration. An upper end of each heat exchanger panel is connected to upper retaining members of the upper frame assembly. A fan pulls air into the enclosed space of the heat exchanger assembly via at least one of the heat exchanger panels.

A component, and a method of forming a component, including a plurality of representative volume elements, each of the representative volume elements abutting at least one other representative volume element to form the component. Each of the representative volume elements includes at least one dividing structure bound by surfaces offset from a parting surface. The shape and contour of the parting surface defined by a mathematical expression that equals a non-zero constant, the mathematical expression selected to define a triply periodic surface when the expression equals zero.

A method of constructing a coil wound heat exchange module and transporting and installing the coil wound heat exchange module at a plant site, such as an natural gas liquefaction plant. A module frame is constructed and attached to a heat exchanger shell prior to telescoping of a coil wound mandrel into the shell. The module frame includes a lug and two saddles that remain attached to the shell throughout the process and when the heat exchanger is operated. The lug and saddles are constructed and located to stabilize the shell during construction, telescoping and transport (when in a horizontal orientation), and when the shell is installed at the plant site (in a vertical orientation). The lugs and saddles are adapted to allow for thermal expansion and contraction of the shell when it is transitioned from ambient to operating temperature and vice versa.