ELECTRIC CIRCUIT BOARD WITH POWER CONNECTOR
A power connector (8) for an aircraft solid state power controller (2) comprises a first portion (81) including a socket (84) configured for receiving an electric plug (9), which is inserted into the socket (84) in a receiving direction (R); and a second portion (82) comprising a connection surface...
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| Hauptverfasser: | , |
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Zusammenfassung: | A power connector (8) for an aircraft solid state power controller (2) comprises a first portion (81) including a socket (84) configured for receiving an electric plug (9), which is inserted into the socket (84) in a receiving direction (R); and a second portion (82) comprising a connection surface (82a) configured for mating with a complementary connection surface (102) of a complementary connection element (10). At least one opening (89) is formed within the connection surface (82a). |
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