公开(公告)号：WO1986006217A1

公开(公告)日：1986-10-23

申请号：PCT/US1986000590

申请日：1986-03-24

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  REED, Elmer, E.

IPC: H01R13/73

CPC classification number: H01R13/73

Abstract: An electrical interconnection assembly (12) for use with a high voltage device such as a traveling-wave tube (10). The assembly (12) includes an electrically insulating housing (32) having a plurality of recesses (36, 38, 40, 41) formed in its outer and inner surfaces. Leads (24, 28) from the high voltage device (10) can be connected directly to respective conductive pins (70, 72) mounted in recesses (40, 41) in the housing inner surface, and electrical conductors (48, 49) from a power supply can be connected directly to respective conductive pins (66, 68) mounted in recesses in the outer surface of the housing (32) and which are electrically connected to respective conductive pins (70, 72) on the inner surface. Protruding staggered gripping elements (60) on the housing outer surface and on a removable cover plate (80) for the housing (32) minimize the possibility of separation of electrical conductors (48, 49) from the conductive pins (66, 68).

公开(公告)号：WO1986004730A1

公开(公告)日：1986-08-14

申请号：PCT/US1985002394

申请日：1985-12-05

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  REED, Elmer, E. ,  MANOLY, Arthur, E.

IPC: H01B11/18

CPC classification number: H01B11/1834 ,  H01R24/545 ,  H01R2103/00

Abstract: A high-power coaxial cable (10) comprising an inner conductor (14), an outer conductor (16) coaxially disposed about and spaced from the inner conductor (14), and insulating fittings (20, 52) disposed between the inner and outer conductors (14, 16) near opposite ends of the cable (10) to maintain a desired spacing between the inner and outer conductors (14, 16). The insulating fitting (26) at one end of the cable has a plurality of longitudinal holes (30) therethrough to reduce the dielectric constant and the impedance of the fitting (20). The fitting (20) is formed in two like sections (22) joined at right angles to one another along a substantially 45o interface (28), thereby defining a short 90o turn for the inner conductor (14) near the end of the cable (10). The fitting sections (22) are retained in position by a surrounding mounting block (34), the opposite ends of which respectively receive a conductive sleeve (38) and an end (42) of the outer coaxial conductor (16) in press-fit relationship.

公开(公告)号：EP0214150B1

公开(公告)日：1989-10-11

申请号：EP86900430.9

申请日：1985-12-05

Applicant: Hughes Aircraft Company

Inventor： REED, Elmer, E. ,  MANOLY, Arthur, E.

IPC: H01B11/18 ,  H01R17/12

CPC classification number: H01B11/1834 ,  H01R24/545 ,  H01R2103/00

Abstract: A high-power coaxial cable (10) comprising an inner conductor (14), an outer conductor (16) coaxially disposed about and spaced from the inner conductor (14), and insulating fittings (20, 52) disposed between the inner and outer conductors (14, 16) near opposite ends of the cable (10) to maintain a desired spacing between the inner and outer conductors (14, 16). The insulating fitting (26) at one end of the cable has a plurality of longitudinal holes (30) therethrough to reduce the dielectric constant and the impedance of the fitting (20). The fitting (20) is formed in two like sections (22) joined at right angles to one another along a substantially 45o interface (28), thereby defining a short 90o turn for the inner conductor (14) near the end of the cable (10). The fitting sections (22) are retained in position by a surrounding mounting block (34), the opposite ends of which respectively receive a conductive sleeve (38) and an end (42) of the outer coaxial conductor (16) in press-fit relationship.

公开(公告)号：EP0214150A1

公开(公告)日：1987-03-18

申请号：EP86900430.0

申请日：1985-12-05

Applicant: Hughes Aircraft Company

Inventor： REED, Elmer, E. ,  MANOLY, Arthur, E.

IPC: H01B11 ,  H01P3 ,  H01R13

CPC classification number: H01B11/1834 ,  H01R24/545 ,  H01R2103/00

Abstract: Câble coaxial de grande puissance (10) comprenant un conducteur interne (14), un conducteur externe (16) disposé de manière coaxiale autour du conducteur interne (14) mais écarté de celui-ci, et des éléments isolants (20, 52) disposés entre les conducteurs interne et externe (14, 16) à proximité des extrémités opposées du câble pour maintenir un écartement désiré entre les conducteurs interne et externe (14, 16). L'élément isolant (26) présente à une extrémité du câble une pluralité de trous longitudinaux (30) traversants, servant à réduire la constante diélectrique et l'impédance de l'élément (20). Celui-ci se compose de deux sections identiques (22) reliées au droit l'une de l'autre le long d'une interface (28) essentiellement à 45o, définissant ainsi un court coude à 90o du conducteur interne (154) à proximité de l'extrémité du câble (10). Les sections de l'élément (22) sont retenues en position par un bloc de montage qui les entoure (34), dont les extrémités opposées reçoivent respectivement un manchon conducteur (38) et une extrémité (42) du conducteur coaxial externe (16) par un montage à pression.

公开(公告)号：EP0217868B1

公开(公告)日：1989-05-31

申请号：EP86902228.5

申请日：1986-03-24

Applicant: Hughes Aircraft Company

Inventor： REED, Elmer, E.

IPC: H01R13/73

CPC classification number: H01R13/73

Abstract: An electrical interconnection assembly (12) for use with a high voltage device such as a traveling-wave tube (10). The assembly (12) includes an electrically insulating housing (32) having a plurality of recesses (36, 38, 40, 41) formed in its outer and inner surfaces. Leads (24, 28) from the high voltage device (10) can be connected directly to respective conductive pins (70, 72) mounted in recesses (40, 41) in the housing inner surface, and electrical conductors (48, 49) from a power supply can be connected directly to respective conductive pins (66, 68) mounted in recesses in the outer surface of the housing (32) and which are electrically connected to respective conductive pins (70, 72) on the inner surface. Protruding staggered gripping elements (60) on the housing outer surface and on a removable cover plate (80) for the housing (32) minimize the possibility of separation of electrical conductors (48, 49) from the conductive pins (66, 68).

公开(公告)号：EP0217868A1

公开(公告)日：1987-04-15

申请号：EP86902228.0

申请日：1986-03-24

Applicant: Hughes Aircraft Company

Inventor： REED, Elmer, E.

IPC: H01R ,  H01R4 ,  H01J23 ,  H01R13

CPC classification number: H01R13/73

Abstract: Un ensemble d'interconnexion électrique (12) est utilisé avec un dispositif de haute tension tel qu'un tube à ondes progressives (10). L'ensemble (12) comprend une enceinte d'isolation électrique (32) ayant une pluralité d'évidements (36, 38, 40, 41) formés dans ses surfaces externe et interne. Des conducteurs (24, 28) partant du dispositif de haute tension (10) peuvent être connectés directement aux broches conductrices respectives (70, 72) montées dans les évidements (40, 41) de la surface interne de l'enceinte, et des conducteurs électriques (48, 49) d'une alimentation électrique peuvent être connectés directement aux broches conductrices respectives (66, 68) montées dans les évidements de la surface externe de l'enceinte (32) et qui sont connectés électriquement aux broches conductrices respectives (70, 72) sur la surface interne. Des éléments saillant en quinconce de prise (60) sur la surface externe de l'enceinte et sur une plaque de couverture amovible (80) pour l'enceinte (32) réduisent au minimum les possibilités de séparation des conducteurs électriques (48, 49) provenant des broches conductrices (66, 68).