B23K20/18

SYSTEMS AND METHODS OF APPLYING THERMAL INTERFACE MATERIALS
20180009072 · 2018-01-11 ·

Disclosed are exemplary embodiments of systems and methods of applying thermal interface materials (TIMs). The thermal interface materials may be applied to a wide range of substrates and components, such as lids or integrated heat spreaders of integrated circuit (IC) packages, board level shields, heat sources (e.g., a central processing unit (CPU), etc.), heat removal/dissipation structures or components (e.g., a heat spreader, a heat sink, a heat pipe, a vapor chamber, a device exterior case or housing, etc.), etc.

TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS

The disclosure describes example techniques and assemblies for joining a first component and a second component. The techniques may include positioning the first and second component adjacent to each other to define a joint region between adjacent portions of the first component and the second component, the joint region being coated with an adhesion resistant coating. The techniques may also include positioning a braze material in the joint region, heating the braze material to form an at least softened material, and cooling the at least softened material to form a mechanical interlock including the braze material in the joint region joining the first and second components. The braze material does not metallurgically bond to the joint surface.

COLD SPRAY ADDITIVE MANUFACTURING OF MULTI-MATERIAL ELECTRICAL CONTACTS

The presently disclosed subject matter relates to multi-material electrical contacts, and methods of making multi-material electrical contacts.

Manufacture of a hollow aerofoil

A method of manufacturing a hollow aerofoil component 100 for a gas turbine engine 10 comprises joining a first panel 200 to a second panel 300 using bonding, and hot forming the panels into shape. The bonding step and the hot forming step are performed in the same rig, thereby optimizing process time and component quality.

Manufacture of a hollow aerofoil

A method of manufacturing a hollow aerofoil component 100 for a gas turbine engine 10 comprises joining a first panel 200 to a second panel 300 using bonding, and hot forming the panels into shape. The bonding step and the hot forming step are performed in the same rig, thereby optimizing process time and component quality.

Support structures for laminated metallic parts
20230166356 · 2023-06-01 ·

A method for the additive manufacturing of an object and a system for manufacturing an object. The method includes depositing a first foil layer, the first foil layer including a first body section, a first support section connected to the first body section, and a second support section connected to the first body section; depositing a second foil layer, the second foil layer comprising a second body section, a third support section, and a fourth support section; aligning the second foil layer and the first foil layer; and applying at least one of heat and pressure to the first foil layer and the second foil layer to form the object comprising the first body section and the second body section.

Techniques and assemblies for joining components

The disclosure describes example techniques and assemblies for joining a first component and a second component. The techniques may include positioning the first and second component adjacent to each other to define a joint region between adjacent portions of the first component and the second component, the joint region being coated with an adhesion resistant coating. The techniques may also include positioning a braze material in the joint region, heating the braze material to form an at least softened material, and cooling the at least softened material to form a mechanical interlock including the braze material in the joint region joining the first and second components. The braze material does not metallurgically bond to the joint surface.

ULTRASONIC METAL WELDING DEVICE

An ultrasonic metal welding device for welding electrical conductors using a compression chamber that is adjustable at least n height and that is delimited on opposite sides by a section of a sonotrode as a first delimiting surface and by at least one section of a counter electrode (156) as a second delimiting surface, wherein for welding, the counter electrode and the sonotrode are displaced relative to one another. The counter electrode used is one that comprises sections (152, 154) of geometrically different working surfaces or is composed of at least two sections that are displaceable relative to one another.

Method for welding electrical conductors by means of ultrasound and ultrasonic metal welding device

The invention relates to an ultrasonic metal welding device and a method for welding electrical conductors using a compression chamber that is adjustable at least in height and that is delimited on opposite sides by a section of a sonotrode as a first delimiting surface and by at least one section of a counter electrode (156) as a second delimiting surface, wherein for welding, the counter electrode and the sonotrode are displaced relative to one another. The counter electrode used is one that comprises sections (152, 154) of geometrically different working surfaces or is composed of at least two sections that are displaceable relative to one another.

Ultrasonic metal welding device

An ultrasonic metal welding device for welding electrical conductors using a compression chamber that is adjustable at least n height and that is delimited on opposite sides by a section of a sonotrode as a first delimiting surface and by at least one section of a counter electrode (156) as a second delimiting surface, wherein for welding, the counter electrode and the sonotrode are displaced relative to one another. The counter electrode used is one that comprises sections (152, 154) of geometrically different working surfaces or is composed of at least two sections that are displaceable relative to one another.