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    • 21. 发明申请
    • A DEVICE FOR STRAIGHTENING OF A PROFILE
    • 配置文件的设备
    • WO1995026238A1
    • 1995-10-05
    • PCT/SE1994000276
    • 1994-03-28
    • SAAB-SCANIA AKTIEBOLAGSERRANDER, Per
    • SAAB-SCANIA AKTIEBOLAG
    • B21D03/02
    • B21D3/05
    • A device is described for straightening the plane of an elongated profile to restore its linearity in the longitudinal direction, through mechanical machining of the plane in question for evening mechanical tensions, which cause deviations from said linearity. The device is primarily characterized by guide means (14-19) for controlling the profile in its longitudinal direction to straightening means, comprising a first and a second roll (8, 11), rotatable about axles (6, 10) substantially perpendicular to the longitudinal direction of the profile, each of which rolls (8, 11) contacts the plane from its side by means of a controlled contact pressure, the device being arranged to feed the profile between the rolls and at least one roll being arranged to perform an axial oscillating movement.
    • 描述了一种装置,用于矫正细长轮廓的平面,以通过对所述平面的机械加工来恢复其在纵向方向上的线性,以产生与所述线性的偏差的晚间机械张力。 该装置主要特征在于用于将纵向方向上的轮廓控制到矫直装置的引导装置(14-19),包括可绕轴线(6,10)旋转的第一和第二辊(8,11),其基本上垂直于 轮廓的纵向方向,其中每一个辊(8,11)通过受控的接触压力从其侧面接触平面,该装置被布置成在辊之间供给轮廓,并且至少一个辊布置成执行 轴向振荡运动。
    • 22. 发明申请
    • DEICING MEANS DEVICE
    • 检测手段
    • WO1994016944A1
    • 1994-08-04
    • PCT/SE1994000049
    • 1994-01-25
    • SAAB-SCANIA AKTIEBOLAGBOMGREN, TomasBÄCKGREN, Karl-JohanEJDEHAGE, KjellJONSSON, SörenNEIGLICK, Bengt
    • SAAB-SCANIA AKTIEBOLAG
    • B64D15/16
    • B64D15/166
    • A device for checking the function of deicing means (2, 5) for aircraft leading edges of wing and horizontal tail is described. The deicing means consists of at least one container, so-called "boot" whose volume can be increased through the supply of gas with overpressure relative to the surrounding atmosphere whose pressure is the same as in the aircraft wings and horizontal tails. The device consists according to the invention of an opening (8) in the external wall (16) of the wing or horizontal tail, covered with an at least somewhat elastic part (15) of the container wall. A sensor (10, 11) is arranged to sense occurring pressure difference between the internal cavity (13) of the container and the interior (14) of the wing and the horizontal tail, respectively, and to emit a corresponding signal.
    • 描述了用于检查机翼和水平尾翼飞机前缘的除冰装置(2,5)功能的装置。 除冰装置包括至少一个容器,所谓的“靴子”,其体积可以通过相对于与飞机机翼和水平尾部相同的压力的周围空气的超压供应而增加。 根据本发明,该装置由翼或水平尾部的外壁(16)中的开口(8)组成,覆盖有容器壁的至少稍微弹性的部分(15)。 传感器(10,11)被布置成分别检测容器的内腔(13)和机翼的内部(14)与水平尾部之间的压力差,并发出相应的信号。
    • 26. 发明申请
    • ARRANGEMENT FOR SEMI-ACTIVE OR ACTIVE CONTROL OF DAMPING MEMBERS IN A VEHICLE SUSPENSION SYSTEM
    • 车辆悬挂系统中阻尼构件的半主动或主动控制的安排
    • WO1991007607A1
    • 1991-05-30
    • PCT/SE1990000727
    • 1990-11-09
    • SAAB-SCANIA AKTIEBOLAGHULT, Olle
    • SAAB-SCANIA AKTIEBOLAG
    • F16F09/50
    • B60G17/01933B60G2400/25B60G2401/14
    • In a vehicle suspension system, there is an arrangement for controlling damping members as a function of the movement between an undamped and damped mass. For the purpose of obtaining a position indicator (9) which is simple and takes up little space between the undamped and damped mass, use is made of a rotating optical pulse transmitter (24) which is coupled to a spring-loaded (23) wire pully (20). The wire pulley (20) has a wire (10) wound round it, which can be drawn out counter to the action of the spring (23) and coupled via coupling members (11, 12) to the second mass. This simple construction permits a protected position of the pulse transmitter itself and simple assembly on different types of spring systems.
    • 在车辆悬架系统中,存在用于控制阻尼构件作为​​无阻尼和阻尼质量块之间的运动的函数的装置。 为了获得简单的位置指示器(9),并且在无阻尼和阻尼的质量块之间占据很小的空间,使用旋转的光学脉冲发射器(24),该旋转光学脉冲发射器(24)耦合到弹簧加载的(23)线 (20)。 线滑轮(20)具有缠绕在其上的线(10),其可以与弹簧(23)的作用相反地拉出并且经由联接构件(11,12)耦合到第二质量块。 这种简单的结构允许脉冲发射器本身的保护位置和在不同类型的弹簧系统上的简单组装。