公开(公告)号：US5197695A

公开(公告)日：1993-03-30

申请号：US845421

申请日：1992-03-04

Applicant: Torbjorn Andersson ,  Ingvar Bengtsson ,  Orjan Arulf ,  Johan Ohlin

Inventor： Torbjorn Andersson ,  Ingvar Bengtsson ,  Orjan Arulf ,  Johan Ohlin

IPC: B64G1/64 ,  F16B2/10

CPC classification number: B64G1/645 ,  B64G1/641 ,  F16B2/10 ,  Y10S292/49 ,  Y10T24/1424 ,  Y10T24/2179 ,  Y10T292/0917

Abstract: A locking device for a band or the like comprising a housing having one end fastened to a first portion of the band. The housing extends in the direction of the prevailing tensile force and is formed with a guide for guiding a link means. This comprises a fastening element fastened at its first end to the second portion of the band and at its second end journally connected to a second link at a distance from its first end. The second link is, at its first end, journaled around an axis provided in the housing transverse to the longitudinal direction of the housing. The locking device also comprises a third link journaled at the first end of the housing and a dowel element which, l via the third link, is able to prevent the second link from being turned around the axis to a position where it is released from the axis so that the locking device is opened.

Abstract translation: 用于带状物或类似物的锁定装置包括具有固定到带的第一部分的一端的壳体。 壳体沿着主要拉伸力的方向延伸并且形成有用于引导连杆装置的引导件。 这包括紧固元件，该紧固元件在其第一端处固定到带的第二部分，并且在其第二端处与其第一端一定距离的时间连接到第二连杆。 第二连杆在其第一端处围绕设置在壳体中的轴线横向于壳体的纵向方向。 锁定装置还包括在壳体的第一端处轴颈的第三连杆和定位销元件，该定位销元件经由第三连杆能够防止第二连杆件绕轴线转动到从第二连杆释放的位置 使锁定装置打开。

公开(公告)号：US5890680A

公开(公告)日：1999-04-06

申请号：US796688

申请日：1997-03-04

Applicant: Orjan Arulf

Inventor： Orjan Arulf

IPC: B64G1/00 ,  B64G1/22 ,  B64G1/64

CPC classification number: B64G1/222 ,  B64G1/641 ,  B64G1/002 ,  B64G1/645

Abstract: A device for imparting rotational movement to a satellite during discharge from an adapter of a launcher. The satellite includes a first axis, a second axis, and a third axis passing through a center of gravity. The first axis, the second axis, and the third axis are mutually perpendicular. The device includes at least one line dismountably attached to a first point on the satellite and a first point on the adapter. The at least one line is attached to the satellite and the adapter such that the at least one line imparts a rotational movement to the satellite as the satellite is discharged and separates from the adapter with a discharge velocity in a direction along the first axis. A lock dismountably attaches the at least one line to the satellite.

Abstract translation: 一种用于在从发射器的适配器放电期间向卫星施加旋转运动的装置。 卫星包括第一轴线，第二轴线和穿过重心的第三轴线。 第一轴，第二轴和第三轴相互垂直。 该装置包括可拆卸地附接到卫星上的第一点和适配器上的第一点的至少一个线。 至少一条线连接到卫星和适配器，使得当卫星排出时，至少一条线向卫星施加旋转运动，并且沿着沿着第一轴线的方向以排出速度与适配器分离。 一个锁可拆卸地将至少一条线连接到卫星。