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1. 发明授权

US07286287B1 Visual aid in the form of telescopic spectacles with an automated focusing device 失效
标题翻译：具有自动对焦装置的伸缩眼镜形式的视觉辅助
公开(公告)号：US07286287B1
公开(公告)日：2007-10-23
申请号：US09889895
申请日：2000-11-23
申请人： Anton Gerald Ofner
发明人： Anton Gerald Ofner
IPC分类号： G02B23/00
CPC分类号： G02B7/002 , G02B5/30 , G02B25/004 , G02B27/017 , G02B27/0172 , G02B27/0176 , G02B2027/0132 , G02C7/088
摘要： A vision aid in the form of telescopic spectacles has two lens systems, which each comprise at least one objective lens (70) and one eyepiece (71). An autofocussing element which changes the focal length of the lens systems for sharp focussing thereof according to the distance of the telescopic spectacle from the object is assigned to the lens systems. Furthermore, an element for changing the magnification factor by changing the focal length of the lens systems (“zoom”) and finally an element for matching the parallax between the lens systems of the vision aid to the focal length which has been set according to the distance of the telescopic spectacles from the object are assigned to the lens systems. The parallax is adapted using adjustable optical elements (11) which are located in the beam path of the lens systems, with which elements the angle (13) between the beam paths (14) running from the lens systems (1) to the object can be changed.
摘要翻译：伸缩眼镜形式的视力援助具有两个透镜系统，每个透镜系统包括至少一个物镜（70）和一个目镜（71）。将透镜系统的焦距改变为根据伸缩眼镜与物体的距离进行锐利聚焦的自动聚焦元件被分配给透镜系统。此外，通过改变透镜系统的焦距（“缩放”）以及最后将视觉辅助的透镜系统之间的视差匹配的元件与根据将伸缩眼镜与物体的距离分配给透镜系统。使用位于透镜系统的光束路径中的可调节光学元件（11）来适应视差，利用该元件，从透镜系统（1）延伸到物体的光束路径（14）之间的角度（13）可以改变。

2. 发明授权

US5971540A Magnifying spectacles with variable focus, variable magnification factor and automatic parallax compensation 失效
标题翻译：放大眼镜具有可变焦距，可变放大倍率和自动视差补偿
公开(公告)号：US5971540A
公开(公告)日：1999-10-26
申请号：US36335
申请日：1998-03-06
申请人： Anton Gerald Ofner
发明人： Anton Gerald Ofner
IPC分类号： A61B19/00 , G02C7/08 , G02C1/00
CPC分类号： G02C7/088 , A61B90/20
摘要： Magnifying spectacles for surgical use have an automatic focusing device, a device for automatically altering the magnification factor and a device for automatic parallax compensation corresponding to the current focal length. During surgical operations, alteration of the working distance is commonly necessary due to the positions of different operating sites. Automatic adaptation of the focal length and the parallax angle allows optimum optical configuration to be reached without the need for the surgeon to use his hands. Focusing can be adjusted using a foot switch.
摘要翻译：用于外科手术的放大镜具有自动对焦装置，用于自动改变放大倍数的装置和与当前焦距相对应的用于自动视差补偿的装置。在外科手术中，由于不同操作部位的位置，通常需要改变工作距离。自动调整焦距和视差角度可以实现最佳的光学配置，无需外科医生使用他的手。可以使用脚踏开关调节对焦。

3. 发明授权

US06910662B1 Aircraft wing and wing parts movable adjacent to the aircraft wing 有权
标题翻译：飞机机翼和机翼部件可在飞机机翼附近移动
公开(公告)号：US06910662B1
公开(公告)日：2005-06-28
申请号：US09959707
申请日：2000-05-02
申请人： Anton Gerald Ofner
发明人： Anton Gerald Ofner
IPC分类号： B64B1/20 , B64C3/48 , B64C3/44
CPC分类号： B64B1/20 , B64C3/48 , Y02T50/14
摘要： Wing parts (20, 21) which influence the lift of aircraft wings (1), especially wings (1) with a cross section and an angle of attack which is suitable for high-speed flight, which parts can be moved out of an aerodynamically inactive servicing position within the aircraft fuselage (30) or out of chambers (40) mounted on the wings (1) into an aerodynamically efficient active position and from the active position back into the servicing position, are assigned to the wings (1). These wing parts (20, 21) in their active position are located on the top (3) and optionally also on the bottom (4) of the wings (1) and are shaped for example such that the wing parts (21) located in their active position on the bottom (4) of the wings (1) jointly with the wing parts (20) located in their active position on the top (3) of the wings (1) increase the lift and optionally at the same time change the angle of attack of the wing.
摘要翻译：影响飞机机翼（1）的升力的翼部件（20,21），特别是适用于高速飞行的横截面和迎角的翼（1），这些部件可以从空气动力学中移出将安装在机翼（1）上的飞行器机身（30）内或室外（40）内的不正常的维修位置分配成空气动力学有效的主动位置并从主动位置返回维修位置。这些翼部件（20,21）处于其主动位置，位于机翼（1）的顶部（3）上并且任选地位于底部（4）上，并且成形为例如使翼部件（21）位于它们与翼（1）的底部（4）的主动位置与位于机翼（1）的顶部（3）上的主动位置的翼部件（20）共同增加升力并且可选地同时改变机翼的攻角。

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