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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Применить Всего найдено 3. Отображено 3.
25-02-2021 дата публикации

Electrical Connector And Bonding System

Номер: US20210057832A1
Автор: Kolarich Roberta A., Kramer Michael I., Myles Andrea M.
Принадлежит:

An electrical connection system includes a mounting stud having a base configured for mounting to a conductive surface. One or more one ring-shaped lugs, formed of an electrically conductive material, are configured for being positioned on the mounting stud for surrounding the mounting stud. The ring-shaped lug includes one or a plurality of interior channels extending around the inside diameter thereof. A contact spring is seated within a respective interior channel and is electrically conductive and dimensioned to extend radially inwardly from the channel and contact the mounting stud when the ring-shaped lug is positioned thereon. The contact spring is configured to at least partially collapse in the radial direction and to provide a spring bias against the mounting stud for providing an electrical connection between the ring-shaped lug and mounting stud. A locking cap is positioned on the mounting stud over the at least one ring-shaped lug for locking with the mounting stud and securing the ring-shaped lugs on the mounting stud for a secure electrical connection. 1. An electrical connection system comprising:a mounting stud having a base configured for mounting to a conductive surface;at least one ring-shaped lug configured for being positioned on the mounting stud for surrounding the mounting stud, the ring-shaped lug being formed of an electrically conductive material and including an interior channel extending around the inside diameter thereof;a contact spring seated within the interior channel, the contact spring being electrically conductive and dimensioned to extend radially inwardly from the channel and contact the mounting stud when the ring-shaped lug is positioned thereon, the contact spring configured to at least partially collapse in the radial direction and to provide a spring bias against the mounting stud for providing an electrical connection between the ring-shaped lug and mounting stud; anda locking cap configured for positioning on the ...

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Номер записи: 1
13-07-2022 дата публикации

Mounting system for mounting an element to an aircraft surface

Номер: EP4026410A1
Автор: Bradley J. PURPUS, Michael I. Kramer
Принадлежит: Carlisle Interconnect Technologies Inc

An electronics system (10) for an aircraft includes a mounting structure (12) and a generally planar plate element (40) mounted to the mounting structure (12) which has opposing face surfaces (41, 43) and includes a central region (50) and side edge regions (52). A serpentine passage (100) is formed in the plate element (40) between the face surfaces and contains alternating liquid slugs and vapor plugs along its length. The plate element 40 is configured for gathering heat proximate the central region (50) and moving the heat to the side edge regions (52) through interaction with the liquid slugs and vapor plugs of the serpentine passage. An electronic system (30, 32) is mounted on a face surface of the plate element proximate the central region (50). A heat dissipating structure, such as a heat sink or an integral portion (120) of the mounting structure (12) is thermally coupled with the plate element and positioned along the side edge regions thereof for dissipating heat of the electronic system (30, 32) moved to the side edge regions (50). A cover structure (14) covers the plate element and electronic system. In one version, the cover (14) has apertures (16, 18) in ends thereof positioned for directing air over the heat sinks.

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Номер записи: 2
03-11-2022 дата публикации

Mounting System For Mounting An Element To An Aircraft Surface

Номер: US20220354020A1
Автор: Bradley J. PURPUS, Michael I. Kramer
Принадлежит: Carlisle Interconnect Technologies Inc

An electronics system for an aircraft includes a mounting structure and a plate element mounted to the mounting structure with opposing face surfaces, a central region and side edge regions. A serpentine passage in the plate element contains alternating liquid slugs and vapor plugs along its length. The plate element is configured for gathering heat proximate the central region and moving the heat to the side edge regions. An electronic system is mounted on a face surface of the plate element and a heat dissipating structure is thermally coupled with the plate element and positioned along the side edge regions thereof for dissipating heat moved to the side edge regions. A cover structure covers the plate element and electronic system.

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Номер записи: 3