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    • 1. 发明申请
    • A DEVICE FOR TREATING THE OUTER SIDE OF AIRCRAFTS
    • 用于处理航空器外侧的装置
    • WO1998005554A1
    • 1998-02-12
    • PCT/NL1997000450
    • 1997-07-31
    • MAATSCHAPPIJ VOOR BEHEER EN INNOVATIE PRINS B.V.PRINS, Willem, Frederik
    • MAATSCHAPPIJ VOOR BEHEER EN INNOVATIE PRINS B.V.
    • B64F05/00
    • B64F5/23B64F5/20
    • A device for treating the outer sides of aircrafts, more particularly the wing and tail surfaces of aircrafts, mainly comprising two gantries (1) disposed on opposite sides of a parking guideline (2) on an aircraft parking place and movable towards one another in a direction transversely to said parking guideline, from a position in which the gantries are mutually spread corresponding to the wing span of an aircraft. Said gantries are each provided with an elongate support (4) that extends substantially parallel to said parking guideline and is provided with means for dispensing a treatment fluid (10), which means is formed by at least one spraying tube extending longitudinally of the longitudinal support, said tube being equipped with longitudinally spaced spraying nozzles, that cooperate with independently controllable valves.
    • 一种用于处理飞行器的外侧的装置,更具体地说是飞机的机翼和尾部表面,主要包括设置在飞行器停车位置上的停车指南(2)的相对侧上的两个机架(1),并且可相互朝向彼此移动 横向于所述停车指南的方向从与机架的机翼跨度对应的台架相互扩展的位置。 所述龙门架各自设置有基本上平行于所述停车指南延伸的细长支撑件(4),并且设置有用于分配治疗流体(10)的装置,所述装置由至少一个沿纵向支撑件纵向延伸的喷射管形成 所述管装备有纵向隔开的喷嘴,其与可独立控制的阀配合。
    • 3. 发明申请
    • METHOD OF TREATING AN OBJECT BY MEANS OF EQUIPEMENT HAVING AT LEAST ONE TREATMENT UNIT
    • 一种用于处理目的是通过其具有处理单元至少一个处理单元来
    • WO1995007217A1
    • 1995-03-16
    • PCT/EP1994002898
    • 1994-09-01
    • FRAUNHOFER-GESELLSCHAFT ZUR FÖRDERUNG DER ANGEWANDTEN FORSCHUNG E.V.WANNER, Martin-ChristophHERKOMMER, Thomas, Fred
    • FRAUNHOFER-GESELLSCHAFT ZUR FÖRDERUNG DER ANGEWANDTEN FORSCHUNG E.V.
    • B64F05/00
    • G05B19/4207B08B1/00B64F5/30G05B13/042
    • Described is a method of treating an object by means of equipment having at least one treatment unit, the equipment being positioned with respect to the object by scanning with a range sensor at least part of the surface of the object facing the sensor, comparing the scan pattern thus obtained with a stored reference model of the object and hence determining the distance and orientation of the equipment relative to the object. The invention calls for comparison of the scan pattern generated by the range sensor with the stored reference model of the object to be preceded by an additional operation in which the object is scanned by an at least range-resolving sensor, for the scan pattern of the object generated by this sensor to be compared with its reference model and the differences between the scan pattern and the stored reference model to be determined, and for at least part of the stored reference model of the object to be modified on the basis of the differences determined and the modified reference model thus generated to be used to determine the position of the equipment relative to the object.
    • 公开了一种用于通过具有处理设备的至少一个处理单元的装置,其中所述处理设备被定位在对象前面通过用距离传感器面向要被处理,扫描处理的对象的方法,至少一部分所述要被处理的物体的距离的传感器表面,一个从该扫描, 扫描与所述对象的所存储的参考模式相比获得将被处理,并且从这个距离和处理装置的取向相对于所述被处理物体被确定。 根据本发明,它提供了待加工与在从与对象的所存储的参考模型的距离传感器的扫描图案所产生的比较的至少距离分辨传感器扫描的物体被处理前面步骤,从所述对象的该传感器图案所产生的与它的参考模型被处理 比较,并且被扫描的图案和所存储的参考模型之间的差异被确定,并且该修改的对象的所存储的参考模型至少部分地对应于所述检测到的偏差,以及用于确定所述机械加工装置的相对位置,从而生成修改后的参考模型是verwendent。
    • 4. 发明申请
    • PROCESS FOR TREATING AN OBJECT, IN PARTICULAR AN AEROPLANE
    • 方法用于加工物体,特别是飞机
    • WO1995005310A1
    • 1995-02-23
    • PCT/EP1994002716
    • 1994-08-15
    • FRAUNHOFER-GESELLSCHAFT ZUR FÖRDERUNG DER ANGEWANDTEN FORSCHUNG E.V.WANNER, Martin-ChristophHERKOMMER, Thomas, Fred
    • FRAUNHOFER-GESELLSCHAFT ZUR FÖRDERUNG DER ANGEWANDTEN FORSCHUNG E.V.
    • B64F05/00
    • B63B59/06B08B1/04B25J9/06B25J9/1692B60S3/06B64F5/30G05B2219/33078G05B2219/37561G05B2219/37563G05B2219/39024G05B2219/40292G05B2219/40298G05B2219/45071G05B2219/49195
    • A process and arrangement are disclosed for cleaning the surface of aeroplanes (44). A large manipulator arranged on a truck (8) is moved towards the aeroplane (44) up to a predetermined position within its range of action and is parked in that position. A rotary brush-bearing head (18) is moved over the surface of the object by means of an articulated mast (13) arranged on the truck (10) and constituted of several extension arms (12, 12', 12", 12''', 14) that may swivel or slide with respect to each other at turning knuckles and/or prismatic joints and of a multiple joint (16) arranged at the last extension arm (14). In order to carry out a washing process in a reliable manner, without the risk of collisions even when the large manipulator is not accurately positioned in front of the aeroplane (44), the large manipulator is parked within a limited two-dimensional parking field (46) spaced apart from the aeroplane (44), while the joints (20 to 28) of the articulated mast (13) and/or the multiple joint (16) are controlled during the surface treatment according to a series of predetermined sets of joint co-ordinates associated to the actual position of the large manipulator within the parking field (46), and the brush-bearing head (18) is moved along a predetermined path of operation over the surface of the object.
    • 本发明涉及一种方法和用于飞机(44)的表面清洁的布置,在所述飞行器(44)的方法的范围内的预定位置,其中一个在底盘上(8),其设置大操纵器,并且停在那里,并在其中一个 旋转刷头(18)由多个旋转和/或滑动关节中的一个的装置可枢转相对于彼此或可移动的臂(12,12”,12”,12' ‘’,14),并且在最后一个臂布置成一个(14)铰接的臂(16) 现有布置(8)的底盘上铰接在物体表面上桅杆(13)移动。为了确保可靠的和无碰撞的洗涤过程中即使有大的机械手的大操纵器的飞机(44)前方的较不准确的定位是(有限二维停车场10内 驻扎在飞机(44)的距离),而关节(20至28)铰接门架(13)和/或Mul的的 术语伦克(16)根据大操纵器的具有预定关节坐标组的序列与刷子头(18)相关联的停车场(10)内的当前位置的一个表面处理沿预定加工路径上移动物体表面上,从而在控制。
    • 5. 发明申请
    • JET AIRCRAFT ENGINE SHIPPING STAND
    • 喷气机飞机发动机
    • WO1997019851A1
    • 1997-06-05
    • PCT/US1996019006
    • 1996-11-27
    • STANLEY AVIATION CORPORATIONLILJA, Gerald, D.FOWLER, FrankHATCH, Robert, F.
    • STANLEY AVIATION CORPORATION
    • B64F05/00
    • B64F5/50
    • The shipping stand includes a cradle assembly (224) mounted upon a frame assembly (211) to which a jet aircraft is securable. The frame assembly includes a plurality of wheels (218) for locomotive capability. A plurality of shock absorbers are operatively engaged between the cradle assembly and frame assembly to provide adequate shock protection to a loaded jet aircraft engine when the shipping stand is configured in a truck transport mode. A plurality of lifting mechanisms selectively raise the cradle assembly to a predetermined height creating gaps between upper transport flanges (254) and lower transport flanges. The gaps correspond to the height of spacers (261) positionable between the flanges in the truck transport mode. To place the shipping stand in an air transport mode, the lifting mechanisms are activated, the spacers are removed from between the flanges and the cradle assembly is lowered to eliminate the gaps between the flanges. Each spacer includes indicia which indicate in which mode the shipping stand is configured and further includes an air mode slot and a truck mode slot which cooperates with corresponding mode pins ensuring that the appropriate indicia are viewable when the shipping stand is configured in either the truck transport mode or the air transport mode.
    • 运输支架包括安装在框架组件(211)上的支架组件(224),喷气式飞机可保持在该框架组件上。 框架组件包括用于机车能力的多个轮子(218)。 多个减震器可操作地接合在支架组件和框架组件之间,以便在装载架被配置为卡车运输模式时,为加载的喷气式飞机发动机提供足够的冲击保护。 多个提升机构选择性地将托架组件升高到预定高度,从而在上传送凸缘(254)和下传送凸缘之间形成间隙。 间隙对应于在卡车运输模式中可在凸缘之间定位的间隔件(261)的高度。 为了将运输支架放置在空运模式中,升降机构被启动,间隔件从凸缘之间移除,并且托架组件被降低以消除凸缘之间的间隙。 每个间隔件包括标记,其指示在哪种模式下运输支架被配置并且进一步包括空气模式槽和卡车模式槽,其与相应的模式销相配合,确保当运输架配置在卡车运输中时可以看到适当的标记 模式或航空运输模式。
    • 6. 发明申请
    • ARRANGEMENT FOR SURFACE TREATMENT, ESPECIALLY THE CLEANING OF THE SURFACES OF LARGE OBJECTS
    • 安排进行表面处理,特别是对大型物体的表面处理
    • WO1995006587A1
    • 1995-03-09
    • PCT/EP1994002611
    • 1994-08-06
    • PUTZMEISTER-WERK MASCHINENFABRIK GMBHWANNER, MartinSCHLECHT, KarlFÜGEL, DietmarFRITZ, Stefan
    • PUTZMEISTER-WERK MASCHINENFABRIK GMBH
    • B64F05/00
    • G01S17/89B63B59/06B64F5/30Y10S15/02
    • The invention relates to an arrangement for cleaning the surfaces of aircraft with a large manipulator having a rotating brush head consisting of several extensions (12, 12', 12'', 14) pivotable on articulations (20, 22, 24, 28) by means of hydraulic drive systems (30) and fitted on a rotary bracket (11) of a motor-driven chassis (10) with its base extension (12) fitted on an angled mast to rotate about a main axis (11) and a multiple articulation (16) on the end extension (14) at the free end. To provide starting auxiliary for the chassis (10), the adaptation of the large manipulator to the aircraft and/or monitoring facilities for the cleaning process, there is an opto-electronic distance camera (40) and a computer-supported electronic evaluation system to which the output signals of the distance camera (40) are applied.
    • 本发明涉及一种装置,用于对具有大机械手,多个旋转接头中的一个(20,22,24,28)由液压驱动单元的装置(30)相互可转动的臂(12,12“ 12' ”,14飞机的表面清洁 )现有(及其Grundlausleger(12马达驱动起落架(10)的枢轴支承块11)上)(绕竖直轴线11“)铰接桅杆可旋转地安装并布置在一个(臂14)中的多个接头(16的自由端)设置旋转刷头 (18)。 为了允许牵引到机箱(10),相对于飞机和/或洗涤过程中的监控大操纵器的校准,是铰接桅杆一个靠在被加工面(44)对准的光电距离相机的枢轴支承块(11)(40 )和(随距离照相机40)的输出信号是在计算机化评价作用提供。
    • 8. 发明申请
    • DE-ICING DEVICE FOR AIRCRAFT
    • 飞机专用装置
    • WO1992013763A1
    • 1992-08-20
    • PCT/EP1992000214
    • 1992-01-31
    • DOLL FAHRZEUGBAU GMBH
    • DOLL FAHRZEUGBAU GMBHECKENFELS, Josef
    • B64F05/00
    • B64F5/23B64F5/20
    • De-icing devices for aircraft have so far taken the form of special lorries on commercial chassis or low-loaders stationed at the airfield concerned. The operator sprayed the aircraft from a separate cab generally fitted with a hydraulic raising and lowering system. It is necessary, especially for temporary airfields, e.g. those used for military purposes, and for de-icing on smaller permanent airfields, to have a de-icing device which is substantially smaller and lighter and can be easily taken to any point of use in the form of a container. To this end the de-icing device is fitted inside a self-supporting frame and has an internal combustion engine as its own power supply unit which drives both a generator to supply all the electrical units and a pump to supply the hydraulically operated components. In addition, all the pipes, threaded unions and cocks conveying the de-icing agent are designed without any sharp inner edges and with the largest possible internal radii.
    • 飞机除冰装置以前是作为专用货车安装在驻扎在各自机场的货车底盘或低装载机上。 操作员从可以移动到升高位置的单独的通常是液压工作篮子喷洒车辆。 优选地,对于临时机场,特别是在军事领域,并且为了在小型永久性机场上进行除冰,需要提供一种除冰装置,其重量更小且更轻,并且可以容易地运送到任何所需的地方 以容器的形式使用。 为此,除冰装置容纳在自支承框架内,并且具有内燃机作为其自身的电源单元,其一方面驱动用于供应所有电气单元的发电机,另一方面驱动一个 用于供应液压操作部件的泵。 此外,导电除冰剂,螺丝和阀门的所有管道均铺设没有尖锐的内部边缘,内部圆形部分尽可能大。
    • 9. 发明申请
    • METHOD AND ARRANGEMENT FOR DEICING AIRCRAFT
    • 用于检测飞机的方法和装置
    • WO1998001341A1
    • 1998-01-15
    • PCT/SE1997001109
    • 1997-06-23
    • ELFSTRÖM, BoROSÉN, Lars-Erik
    • B64F05/00
    • B64F5/23B64F5/20
    • A method and an arrangement for treating the surface (1) of an aircraft on which a layer of ice, frost or snow has formed, in order to remove such layer and possibly prevent re-freezing with e.g. glycol. According to the invention water vapour is supplied to a movable arrangement having a space (26) defined by a cloth (28) and having an opening (27) which is closed by the part of the aircraft surface being treated. The arrangement is moved along the surface of the aircraft while water vapour is supplied continuously to said space (26) via a pipe (35) so that the layer in the opening (27) melts.
    • 一种用于处理其上形成有一层冰,霜或雪的飞行器的表面(1)的方法和装置,以便去除这样的层并且可能防止例如冷冻, 乙二醇。 根据本发明,水蒸气被供应到具有由布(28)限定的空间(26)的可移动装置,并且具有由被处理的飞机表面的部分封闭的开口(27)。 该装置沿着飞行器的表面移动,同时水蒸汽经由管道35连续供应到所述空间(26),使得开口(27)中的层熔化。