Controlled-luminance lighting device
    3.
    发明申请
    Controlled-luminance lighting device 失效
    受控亮度照明装置

    公开(公告)号:US20020172046A1

    公开(公告)日:2002-11-21

    申请号:US10145885

    申请日:2002-05-16

    Abstract: A controlled-luminance lighting device comprising a fluorescent lamp (1), which extends longitudinally between a primary reflector (2) and a secondary reflector (3). The primary reflector (2) is formed by a plurality of cup-like elements (4) set alongside one another, having a generally parabolic shape, through which there extends the lamp (1), and the secondary reflector (3) is constituted by a tray-like element with a curved surface. The primary reflector (2) further includes a tile (9), which extends longitudinally between each pair of cup-like elements (4).

    Abstract translation: 一种受控亮度照明装置,包括在主反射器(2)和次反射器(3)之间纵向延伸的荧光灯(1)。 主反射器(2)由多个彼此并排设置的杯状元件(4)形成,具有大致抛物线形状,通过该形状延伸灯(1),并且次级反射器(3)由 具有弯曲表面的托盘状元件。 主反射器(2)还包括在每对杯形元件(4)之间纵向延伸的瓷砖(9)。

    Controlled-luminance lighting device
    4.
    发明申请
    Controlled-luminance lighting device 有权
    受控亮度照明装置

    公开(公告)号:US20020172044A1

    公开(公告)日:2002-11-21

    申请号:US10145886

    申请日:2002-05-16

    Abstract: A controlled-luminance lighting device comprising a fluorescent light source of a linear type (5), which extends longitudinally between a reflector (1) that is formed by an elongated body having a curved surface, and a set of transverse fins (3), which are set at a distance apart from one another and which define a grill for directional control of the light emitted by the light source (5). The reflector (1) defines, together with the transverse fins (3), a plurality of elements (2) set alongside one another of a generally parabolic shape.

    Abstract translation: 一种受控亮度照明装置,包括直线型(5)的荧光光源,其在由具有弯曲表面的细长主体形成的反射器(1)和一组横向翅片(3)之间纵向延伸, 它们被设置在彼此间隔开的距离处,并且限定用于由光源(5)发射的光的方向控制的格栅。 反射器(1)与横向散热片(3)一起限定多个沿大体抛物线形状彼此并列设置的元件(2)。

    VTOL aircraft
    5.
    发明申请
    VTOL aircraft 失效
    垂直起落飞机

    公开(公告)号:US20040129827A1

    公开(公告)日:2004-07-08

    申请号:US10626704

    申请日:2003-07-25

    CPC classification number: B64C39/026 B64C29/02

    Abstract: VTOL aircraft comprising a first and a second ducted rotor positioned at the ends of a vertical fuselage and whose propellers are driven to rotate in mutually opposite directions. Control flaps for orientation and transverse flight are operatively associated at least to the lower ducted rotor.

    Abstract translation: VTOL飞机包括位于垂直机身的端部的第一和第二导管转子,并且其螺旋桨被驱动以沿彼此相反的方向旋转。 用于定向和横向飞行的控制翼片至少可操作地连接到下部管道转子。

    Lighting device, particularly a motor vehicle light
    6.
    发明申请
    Lighting device, particularly a motor vehicle light 失效
    照明装置,特别是汽车灯

    公开(公告)号:US20020172045A1

    公开(公告)日:2002-11-21

    申请号:US10145759

    申请日:2002-05-16

    CPC classification number: B60Q1/302 F21S43/13 F21S43/31

    Abstract: A lighting device, particularly a motor vehicle light, comprising a primary reflector (2) composed of a hollow body that defines a pair of pointed elements (4,5), which face opposite directions, between which a luminous source (1) is placed; and a secondary reflector composed of an elongated element (3) with steps (6), at whose centre the primary reflector (2) is placed with its relative pointed elements (4,5) facing the steps (6).

    Abstract translation: 一种照明装置,特别是机动车灯,包括由限定一对相对方向的一对尖锐元件(4,5)构成的初级反射器(2),所述中空体位于其间放置发光源(1) ; 以及由具有台阶(6)的细长元件(3)组成的次级反射器,其主要反射器(2)的中心位于其相对尖的元件(4,5)的与台阶(6)相对的位置。

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