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    BUOY DEPLOYMENT SYSTEM
    2.
    发明专利
    BUOY DEPLOYMENT SYSTEM 未知

    公开(公告)号：AU4154889A

    公开(公告)日：1990-04-05

    申请号：AU4154889

    申请日：1989-09-19

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： FERRARO JOHN ROBERT ,  FOERSTER PHILIP PAUL ,  GREENSTREET PETER THOMAS ,  SCHWARZ STEVEN RICHARD ,  TURGEON MILTON ROBERT

    IPC: B63B22/00 ,  B64D1/02

    Abstract: A buoy deployment system for an aircraft is disclosed which includes a multi-store gravity launching system which allows for discharge of different lengths and types of buoys. The gravity launch system includes a plurality of launch tubes, each including a spring biased door at the discharge end thereof, with the doors being either electrically actuated from the pilot cockpit via electrical controls, or, in the event of an electrical malfunction, being manually operable by an operator. Each buoy loaded therein is accessible for reconfiguration in flight, with each tube similarly being reloadable in flight. Also disclosed is a rotatable storage carousel including a plurality of semi-cylindrical tube section/latch assemblies, sized to restrain a plurality of buoys, which form storage stations on the carousel. The storage carousel maximizes the number and type of buoys which may be carried in a given space, being manually rotatable to allows access for setting the operational functions of the buoys contained therein. Utilizing the gravity launcher and storage carousel provides maximum mission flexibility while minimizing aircraft space requirements.

    BUOY DEPLOYMENT SYSTEM
    7.
    发明专利
    BUOY DEPLOYMENT SYSTEM 未知

    公开(公告)号：AU1709192A

    公开(公告)日：1992-07-16

    申请号：AU1709192

    申请日：1992-05-21

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： FERRARO JOHN ROBERT ,  FOERSTER PHILIP PAUL ,  GREENSTREET PETER THOMAS ,  SCHWARZ STEVEN RICHARD ,  TURGEON MILTON ROBERT

    IPC: B63B22/00 ,  B64D1/02 ,  B64D1/10

    Abstract: A buoy deployment system for an aircraft is disclosed which includes a multi-store gravity launching system which allows for discharge of different lengths and types of buoys. The gravity launch system includes a plurality of launch tubes, each including a spring biased door at the discharge end thereof, with the doors being either electrically actuated from the pilot cockpit via electrical controls, or, in the event of an electrical malfunction, being manually operable by an operator. Each buoy loaded therein is accessible for reconfiguration in flight, with each tube similarly being reloadable in flight. Also disclosed is a rotatable storage carousel including a plurality of semi-cylindrical tube section/latch assemblies, sized to restrain a plurality of buoys, which form storage stations on the carousel. The storage carousel maximizes the number and type of buoys which may be carried in a given space, being manually rotatable to allows access for setting the operational functions of the buoys contained therein. Utilizing the gravity launcher and storage carousel provides maximum mission flexibility while minimizing aircraft space requirements.

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