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    • 3. 发明授权
    • Double-mirror combining glass for head-up display
    • 双镜组合玻璃用于平视显示
    • US06751025B2
    • 2004-06-15
    • US10168386
    • 2002-06-21
    • Jean-Marc DarrieuxYannick ChevreauJean-François Gomme
    • Jean-Marc DarrieuxYannick ChevreauJean-François Gomme
    • G02B2714
    • G02B27/0101
    • A double-plate combiner for a head-up visor, including two substantially flat plates substantially parallel to each other, and held fixedly together by a holding structure that includes a central baseplate, two side flanks connected to the central baseplate, and two spacers respectively connected to the side flanks and tightly holding the two plates between them. An outer plate is tightly held between free ends of the spacers and an inner plate is tightly held between the free ends, connected to the side flanks, of the spacers. An assembly of the plates, the side flanks, and the spacers has a plane of symmetry substantially orthogonal to the mid-plane of the plates. A first dimension from one spacer to the other of the outer plate is greater than a second dimension from one spacer to the other of the inner plate. The mid-plane of each spacer is not orthogonal to the mid-plane of the plates. Such a double-plate combiner can especially be applied to a head-up visor mounted in the cockpit of an aircraft, preferably of the airplane type.
    • 一种用于平顶遮阳板的双板组合器,包括基本上彼此平行的两个基本平坦的板,并且通过保持结构固定地保持在一起,该保持结构包括中央基板,连接到中心基板的两个侧面侧面和两个间隔件 连接到侧面,并将两个板紧紧地保持在它们之间。 外板紧紧地保持在间隔件的自由端之间,并且内板牢固地保持在间隔件的连接到侧面的自由端之间。 板,侧面和间隔件的组件具有与板的中间平面基本正交的对称平面。 从一个间隔件到外板的另一个的第一尺寸大于从一个隔离件到另一个内板的第二尺寸。 每个间隔物的中间平面不与板的中间平面正交。 这种双板组合器可以特别适用于安装在飞行器的驾驶舱中,优选为飞机型的俯视遮阳板。
    • 4. 发明授权
    • Device for the mechanical hooking of a display system to a helmet
    • 将显示系统机械挂接到头盔的装置
    • US5581806A
    • 1996-12-10
    • US400866
    • 1995-03-08
    • Pascal CapdepuyJean-Marc Darrieux
    • Pascal CapdepuyJean-Marc Darrieux
    • A42B3/04G02B27/00G02B27/01G02B27/02H04N5/64G02B7/00
    • A42B3/04G02B27/0176G02B2027/0143G02B2027/0154G02B2027/0156
    • A device for the mechanical hooking of a display system to a helmet which includes a sheath that surrounds the body of the display system except for elbowed optical elements leading to the combiner forming the eye-piece of the display system and that has a projecting longitudinal ridge acting as a guiding shaft for the hooking and as a fastening lug, and also includes a hooking stud. The device also has a stage that is interposed between the side wall of the helmet and the sheath. This stage is provided with a channel designed to receive the longitudinal ridge of the sheath and a hook jaw designed to grasp the hooking stud. The device is fixed to the side wall of the helmet by mechanism enabling the adjustment of its position both vertically and laterally, to enable the adjusting of the position of the eye-piece of the display system in the alignment of the helmet wearer's eye.
    • 一种用于将显示系统机械挂接到头盔的装置,其包括围绕显示系统的主体的护套,除了通过组合器形成显示系统的眼睛的弯头光学元件,并且具有突出的纵向脊 作为用于钩的引导轴和紧固凸耳,并且还包括钩挂螺柱。 该装置还具有介于头盔的侧壁和护套之间的台阶。 该台设置有用于容纳护套的纵向脊的通道和设计成抓住钩钉的钩夹。 该装置通过机构固定到头盔的侧壁,能够垂直和横向地调节其位置,以便能够调整戴头戴用者的眼睛对齐的显示系统的眼部的位置。
    • 5. 发明授权
    • Head-up display adaptable to given type of equipment
    • 平视显示适应给定类型的设备
    • US06813086B2
    • 2004-11-02
    • US10013690
    • 2001-12-13
    • Laurent BignollesJean-Marc DarrieuxYannick Chevreau
    • Laurent BignollesJean-Marc DarrieuxYannick Chevreau
    • G02B2714
    • G02B27/0101
    • A head-up display including a combiner and a relay optics formed from a combination of optical elements and forming an intermediate image projected to infinity by the combiner of a symbology emitted in a given spectral band by an image source. The combiner forms an off-axis convergent mirror in the spectral band, and an angle of inclination of the off-axis convergent mirror is adjustable for a given type of equipment as a function of a position of the image source and in a given angular range that depends on the type of equipment. The relay optics is modular and includes a first module with at least one optical element fixed regardless of the type of equipment and a second module with at least one optical element for which a position is predefined as a function of an angular position of the combiner.
    • 一种平视显示器,包括由光学元件的组合形成的组合器和中继光学器件,并且通过由图像源在给定光谱带中发射的符号系统的组合器形成投影到无限远的中间图像。 组合器在光谱带中形成离轴会聚反射镜,并且对于给定类型的设备,离轴会聚反射镜的倾斜角度可根据图像源的位置和给定的角度范围而变化 这取决于设备的类型。 中继光学器件是模块化的,并且包括具有固定的至少一个光学元件的第一模块,而不管设备的类型如何,以及具有至少一个光学元件的第二模块,其中位置被预先定义为组合器的角位置的函数。
    • 6. 发明授权
    • Fastening of a support for on-board equipment
    • 紧固对车载设备的支持
    • US6078428A
    • 2000-06-20
    • US209757
    • 1998-12-11
    • Thierry RambertJean-Marc Darrieux
    • Thierry RambertJean-Marc Darrieux
    • B64D43/00G02B27/01G02B27/14
    • B64D43/00G02B27/0149
    • Disclosed is a removable device for the supporting of equipment in an aircraft, especially to fasten the support of a head-up collimator with its projection system, above the seat of the pilot of the aircraft. To enable the support to be dismounted (for maintenance for example), and to be put back in place at its exact position, the fastening device is made as follows: it is hinged on the aircraft by a hinge and it is fastened by bolts enabling the fastening of the support according to an angle that is variable about a rotation axis. The device furthermore comprises a centering block that cooperates with a centering pawl, one of the two elements being part of the aircraft while the other is part of the support, the pawl being housed in a removable way in a positioning aperture formed in the centering block, the block comprising a cup filled with resin, the resin being used to define and maintain the position of the aperture with respect to the cup.
    • 公开了一种用于在飞行器中支撑设备的可移除装置,特别是将其具有其投影系统的平视准直器的支撑件紧固在飞行器飞行员的座位之上。 为了使支撑件能够被拆卸(例如用于维护),并且在其精确位置被放回到位,紧固装置制成如下:它通过铰链铰接在飞机上,并且通过螺栓固定 根据围绕旋转轴线变化的角度来固定支撑件。 该装置还包括与定心爪配合的定心块,两个元件中的一个是飞行器的一部分,而另一个是支撑件的一部分,棘爪以可移除的方式容纳在形成在定心块中的定位孔中 ,所述块包括填充有树脂的杯,所述树脂用于限定和保持所述孔相对于所述杯的位置。
    • 7. 发明授权
    • Collimator support and guidance device
    • 准直仪支撑和导向装置
    • US5479294A
    • 1995-12-26
    • US160914
    • 1993-12-03
    • Jean-Marc DarrieuxPatrick Nicolo
    • Jean-Marc DarrieuxPatrick Nicolo
    • B64D45/08G02B27/00G02B27/01G02B27/30G02B27/14
    • G02B27/0149G02B2027/0156G02B27/30
    • A device for supporting and guiding a collimator, particularly for a collimator designed to be installed on the ceiling of an aircraft. A collimator follows a complex predefined trajectory in a three-dimensional space (X, Y, Z ) with up to six degrees of freedom, between a given operational position and a stored position. The device includes a first structure (3) attached to the aircraft having three guiding grooves, a first central groove (30) following a plane trajectory in a first plane (X, Y), and two lateral grooves (31, 32) on opposite sides of the central groove which follow second and third trajectories located in two planes perpendicular to the first plane. A second structure (4) rigidly attached to the collimator (1) moves along grooves by means of rollers (8a, 8b, 9a, 9b, 10), the number and shape of which enable the second structure to have six degrees of freedom along the complex trajectory.
    • 一种用于支撑和引导准直器的装置,特别是用于设计成安装在飞行器的天花板上的准直器。 准直器遵循在给定操作位置和存储位置之间具有高达六个自由度的三维空间(X,Y,Z)中的复杂预定轨迹。 该装置包括附接到具有三个引导槽的飞行器的第一结构(3),在第一平面(X,Y)中的平面轨迹之后的第一中心凹槽(30)和相对的两个横向凹槽(31,32) 沿着位于垂直于第一平面的两个平面中的第二和第三轨迹的中心凹槽的侧面。 刚性地附接到准直器(1)的第二结构(4)通过辊(8a,8b,9a,9b,10)沿着凹槽移动,其数量和形状使得第二结构能够沿着六个自由度 复杂的轨迹。