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公开(公告)号：US6029934A
公开(公告)日：2000-02-29
申请号：US392524
申请日：1999-09-09
申请人： Clifton L. Foster
发明人： Clifton L. Foster
CPC分类号： B64F5/0054 , B60S3/002 , B64F5/0063
摘要： An apparatus for deicing aircraft includes a vehicle frame, such as part of a truck, and a boom having one end mounted on the vehicle frame and a free end. A compressor unit is supported by the boom and includes a motor having an output and a centrifugal compressor operatively connected to the motor output. A deicer air jet nozzle is located at the boom and operatively coupled to the air outlet of the centrifugal compressor for receiving air and discharging the air for a deicer application.
摘要翻译： 用于除冰飞机的装置包括诸如卡车的一部分的车架和具有安装在车架上的一端和自由端的吊杆。 压缩机单元由悬臂支撑并且包括具有可操作地连接到电动机输出的输出和离心式压缩机的电动机。 除冰空气喷嘴位于起重臂处并且可操作地联接到离心式压缩机的空气出口，用于接收空气并排出用于除冰机应用的空气。
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公开(公告)号：US5490646A
公开(公告)日：1996-02-13
申请号：US84857
申请日：1993-06-28
申请人： E. Craig Shaw , Marlee Payne-Shaw
发明人： E. Craig Shaw , Marlee Payne-Shaw
CPC分类号： B64F5/0054 , B25J5/005 , B64F5/0063
摘要： An aircraft maintenance robot (20) for maintaining aircraft surfaces is described, that includes a maintenance tool (228), for example a nozzle (78), conduits and a pump, which supply fluid to the maintenance tool, which sprays the fluid on aircraft surfaces; movable arm with rotatable hinges and wrists such that a manifold to which the maintenance tools are coupled may be positioned in response to control signals; and a processor which, after accounting for the position of the aircraft, the weather conditions, and the physical dimensions of the aircraft, generates the control signals used to position the maintenance tool such that, after positioning the aircraft, the maintenance operation may be performed without human intervention. The preferred embodiment of the present invention discloses the use of the maintenance robot (20) for deicing aircraft. A wide variety of interchangeable end effectors, however, may be used for a wide variety of applications. These may include various cleaning, painting, paint removing, and even firefighting applications.
摘要翻译： 描述了用于维持飞行器表面的飞行器维护机器人（20），其包括维护工具（228），例如喷嘴（78），导管和泵，其向维护工具供应流体，所述维护工具在飞机上喷射流体 表面 可移动臂具有可旋转的铰链和手腕，使得可以响应于控制信号来定位维修工具联接到的歧管; 以及处理器，在考虑到飞机的位置，天气状况和飞机的物理尺寸之后，生成用于定位维护工具的控制信号，使得在定位飞行器之后，可以执行维护操作 没有人为干预。 本发明的优选实施例公开了维护机器人（20）用于除冰飞机的应用。 然而，各种可互换的端部执行器可以用于各种各样的应用。 这些可能包括各种清洁，涂漆，除漆，甚至消防应用。
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公开(公告)号：US5330579A
公开(公告)日：1994-07-19
申请号：US923789
申请日：1992-09-21
CPC分类号： B64F5/0054 , B44D3/16 , B64F5/0063 , Y10S15/02
摘要： An apparatus and method are provided for use in removal of coatings from airplanes and the like wherein such removal requires the application of a solvent composition for dissolving the coating such as paint, the solvent having a sufficiently high vapor pressure to be present in both a liquid phase and a gaseous vapor phase at stripping temperatures with the solvent in the vapor phase being lighter than the liquid phase and heavier than air, and the apparatus including a portable carriage, positionable beneath the airplane, a receptacle having spaced side walls and carried by the carriage, the side walls extending vertically upwardly, the receptacle further defining a receptacle bottom portion, the receptacle receiving spent solvent in both the liquid and the vapor phases after application of the solvent to the airplane surfaces and dissolution of the paint therein, the side walls directing the received spent solvent in both phases to the receptacle bottom portion such that vapor phase is trapped above the heavier liquid phase by the lighter air thereover, and an exhaust port located above the receptacle bottom portion for removing the vapor phase.
摘要翻译： PCT No.PCT / US90 / 01074 Sec。 371日期：1992年9月21日 102（e）日期1992年9月21日PCT提交1990年2月26日PCT公布。 公开号WO91 / 12906 1991年9月5日提供的装置和方法用于从飞机等中去除涂层，其中这种去除需要施加用于溶解涂层的溶剂组合物，例如涂料，溶剂具有足够高的蒸气压 在气相中的溶剂比液相轻且比空气重的存在于汽提温度下的液相和气态气相中，并且该装置包括可位于飞机下方的便携式支架，容器具有 间隔的侧壁并由托架承载，侧壁垂直向上延伸，容器还限定了容器底部部分，在将溶剂施加到飞机表面之后，该容器在液相和汽相中接收废溶剂， 其中的涂料，侧壁将接收到的废溶剂在两相中引导到容器底部部分 h，气相通过其上较轻的空气被捕获在较重的液相上方，以及位于容器底部部分上方的用于除去气相的排气口。
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公开(公告)号：US4723733A
公开(公告)日：1988-02-09
申请号：US853124
申请日：1986-04-17
申请人： William McClinchy
发明人： William McClinchy
CPC分类号： B64F5/0054 , B64F5/0063
摘要： A mobile aircraft deicer having a base unit, a boom connected to the base unit, a deicer nozzle connected to the free end of the boom, and a television camera connected to the deicer nozzle.
摘要翻译： 具有基座单元的移动式飞机除冰机，连接到基座的起重臂，连接到起重臂的自由端的除冰机喷嘴以及连接到除冰机喷嘴的电视摄像机。
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公开(公告)号：US4651927A
公开(公告)日：1987-03-24
申请号：US678556
申请日：1984-11-20
申请人： Godtfred Vestergaard
发明人： Godtfred Vestergaard
IPC分类号： B05B7/24 , B05B7/26 , B05B7/32 , B05B9/03 , B64D15/10 , B64F5/00 , B05B7/00 , A01G25/09 , A62C31/00 , A62C31/30
CPC分类号： B64F5/0054 , B05B12/1418 , B05B7/32 , B64F5/0063
摘要： A plant for de-icing especially surfaces of aeroplanes, comprising the use of at least two sources (10, 12) of liquid media that are different from each other and capable of being sprayed separately or as a mixture, comprising a number of positive liquid pumps (16, 22) corresponding to the number of media, which pumps all have the same capacity or a predetermined interrelated capacity ratio and terminate in a common spray pipe (24). The connection of the liquid pumps to the sources includes at least one of the sources to at least one of the liquid pumps. In a hydraulic system comprising hydraulic motors (56, 52) for driving the liquid pumps (16, 22) at least two of motors are connected to a common hydraulic pressure pump (32) controlled by way of pressure compensation (33) to work with at least two pressure stages subject to a ratio corresponding to that of the capacity of at least one liquid pump to the total capacity of both liquid pumps. In such a plant the compostion of the spray liquid to be dispensed is determined solely by the capacity of the liquid pumps, thereby eliminating any throttling effects which may cause the de-icing medium to coagulate.
摘要翻译： PCT No.PCT / DK84 / 00020 Sec。 1984日期1984年11月20日 102（e）1984年11月20日日期PCT提交1984年3月20日PCT公布。 公开号WO84 / 03644 日期：1984年9月27日。一种用于除冰，特别是飞机表面的设备，其包括使用彼此不同并能够单独喷射或作为混合物的至少两种液体介质源（10,12） 包括多个对应于介质数量的正液体泵（16,22），所述多个泵都具有相同的容量或预定的相互关联的容量比并且终止在共同的喷管（24）中。 液体泵与源的连接包括至少一个液体泵的源中的至少一个。 在包括用于驱动液体泵（16,22）的液压马达（56,52）的液压系统中，至少两个马达连接到通过压力补偿（33）控制的公共液压泵（32），以与 至少两个压力级受到与至少一个液体泵的容量相对应于两个液体泵的总容量的比率。 在这种植物中，要分配的喷雾液体的组合仅由液体泵的容量确定，从而消除可能导致除冰介质凝结的任何节流效应。
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公开(公告)号：US6038781A
公开(公告)日：2000-03-21
申请号：US268959
申请日：1999-03-16
CPC分类号： B64F5/0054 , B64F5/0063
摘要： The assembly includes a plurality of flexible and inflatable bags 43, 44, 45, 46, 47, 48, 56 and 58, each having a rectangular cross section with an open end for receiving air from various ducts 30, 32, 34, 36, 38, 40, 62 and 66, and extending vertically to a nozzle end 52. A plurality of first starboard bags 43 overlap a plurality of second starboard bags 44 in the horizontal direction and a plurality of first port bags 46 overlap a plurality of second port bags 47 in the horizontal direction. Also, the second starboard 44 and port 47 bags are spaced downstream from the first 43 starboard and port 46 bags. The nozzles 52 of the first starboard bags 43 are disposed in a first horizontal V.sub.a. -shape in relationship with the first port bags 46 to direct the emitting air in the emitting planes rearwardly and outwardly on each side of the aircraft 10 to move deicing material outwardly and rearwardly over the wings 12 and 14 and the nozzles 52 of the second starboard 44 and port 47 bags are disposed in a second horizontal V.sub.b -shape with each other to direct the emitting air in the emitting planes rearwardly and outwardly from the aircraft 10 to move deicing material outwardly and rearwardly over the wings from the first starboard 43 and port 46 bags. Three third starboard bags 45 are aligned horizontally with three third port bags 48 and downstream of the second starboard 44 and port 47 bags. A plurality of starboard 56 and port 58 are disposed close together for removing deicing material from the horizontal stabilizer of the aircraft.
摘要翻译： 组件包括多个柔性和可充气的袋子43,44,45,46,47,48,56和58，每个袋子具有矩形横截面，开口端用于从各种管道30,32,34,36,36接收空气， 38,40,62和66，并且垂直地延伸到喷嘴端52.多个第一右舷行李箱43在水平方向上与多个第二右舷行李箱44重叠，并且多个第一口袋46与多个第二端口 袋47在水平方向。 此外，第二右舷44和47口袋与第一个43右舷和46个行李箱的下游隔开。 第一右舷行李箱43的喷嘴52与第一端口袋46相关地设置成第一水平的Va.形状，以便在飞机10的每一侧向后和向外引导发射平面中的排放空气，以移动除冰材料 向上和向后在翼12和14之上，并且第二右舷44和端口47的喷嘴52袋彼此相邻地设置成第二水平的Vb形状，以将飞行器10的向后和向外的发射平面中的排出空气引导 以从第一右舷43和46口袋向外和向后移动除冰材料。 三个第三右舷行李箱45与三个第三口袋48水平对准，第二右舷44和47个袋子的下游。 多个右舷56和端口58靠近放置，用于从飞机的水平稳定器上除去除冰材料。
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公开(公告)号：US5354014A
公开(公告)日：1994-10-11
申请号：US54044
申请日：1993-04-27
申请人： Thomas M. Anderson
发明人： Thomas M. Anderson
CPC分类号： B64F5/0054 , B64F5/0063 , Y02P70/585
摘要： A system for de-icing aircraft in a de-icing area includes a first recessed storage area located substantially below ground level on a first side of the de-icing area. A first spraying boom, having at least one boom section, is used to apply de-icing solution to surfaces of aircraft. A first spray nozzle, for applying de-icing solution to surfaces of aircraft, is supported by the first spraying boom. The first spraying boom may be raised out of the first recessed storage area when an aircraft needs de-icing and lowered into the first recessed storage area for storage when aircraft de-icing is complete.
摘要翻译： 用于在除冰区域中除冰飞机的系统包括在除冰区域的第一侧上基本上位于地平面下方的第一凹陷存储区域。 使用具有至少一个悬臂部分的第一喷洒臂将除冰溶液应用于飞机的表面。 用于将除冰溶液施加到飞机表面的第一喷嘴由第一喷洒臂支撑。 当飞行器除冰完成时，当飞机需要除冰并且降低到第一凹进的存储区域中以存储时，第一喷洒臂可以从第一凹进的存储区域升出。
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公开(公告)号：US5222696A
公开(公告)日：1993-06-29
申请号：US837447
申请日：1992-02-14
申请人： William D. Brigham , Dinh D. Nguyen
发明人： William D. Brigham , Dinh D. Nguyen
CPC分类号： B64F5/0054 , B64F5/0063 , F02B3/06
摘要： A single nonfired heat source, such as a diesel engine, drives a hydraulic pump. The hydraulic pump in turn is coupled in a hydraulic circuit with a back-pressure valve which loads the hydraulic pump and hence the diesel engine. The engine also circulates a heat exchanging fluid, such as engine coolant through a second circuit. Water or engine coolant is circulated through the second circuit by means of a pump driven by the diesel engine. An exhaust gas heat exchanger coupled to the exhaust gases from the engine may also be included within the water coolant, the exhaust gases or both, and is then transferred to noncirculating deicing fluid in a storage tank. Heat developed within the hydraulic circuit which loads the engine is also transferred to the noncirculating fluid in the storage tank. The heated noncirculating fluid may be gently stirred to increase heat exchange efficiency and then either pumped directly to the utilization site from the storage tank or pumped in a single pass through a heat exchanger thermally coupled through the water coolant heat exchanger, hydraulic heat exchanger, or both, and thence to the utilization site.
摘要翻译： 单个非燃烧热源，例如柴油发动机，驱动液压泵。 液压泵依次与液压回路连接，其中背压阀装载液压泵并因此装载柴油发动机。 发动机还通过第二回路使诸如发动机冷却剂的热交换流体循环。 水或发动机冷却液通过由柴油发动机驱动的泵循环通过第二回路。 与来自发动机的废气相连的排气热交换器也可以包括在水冷却剂，废气或两者内，然后被转移到储罐中的非循环除冰流体中。 在装载发动机的液压回路内产生的热量也转移到储罐中的非循环流体。 加热的非循环流体可以被轻轻搅拌以提高热交换效率，然后直接从储罐泵送到利用部位，或者单次泵送通过热交换器，热交换器通过水冷却剂热交换器，液压热交换器或 两者，然后到使用场所。
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公开(公告)号：US5190249A
公开(公告)日：1993-03-02
申请号：US414628
申请日：1989-09-25
IPC分类号： B64F5/00
CPC分类号： B64F5/0054 , B64F5/0063
摘要： The invention is a system for heating aircraft deicing fluid. The system is an aircraft deicer such as shown in FIG. 2 which includes an engine 210. The deicer systems comprises a tank 270 for holding deicing fluid. First pump means 250,252 and 254 are driven by engine 210 and pump deicing fluid from tank 270 through piping or conduit 266,264,230. Backpressure valve means 251,253,255 is positioned the outlet of the first pump means 250,252,254 respectively, to continuously, substantially and directly heat deicing fluid to a temperature sufficient to deice the aircraft.The system further comprises second pump means 212, 232 for directing deicing fluid through engine 210 to pick up heat rejected by engine 210. Once the deicing fluid has been pumped through engine 210, piping or a conduit means 216,222,228,230,266,264 connects the output of the second pump means 212,232 to the inlet of the first pump means 250,252 and 254.
摘要翻译： 本发明是用于加热飞机除冰液的系统。 该系统是如图1所示的飞机除冰机。 除冰机系统包括用于保持除冰流体的罐270。 第一泵装置250,252和254由发动机210驱动，并且通过管道或导管266,264,230从罐270驱动泵除冰流体。 背压阀装置251,253,255分别定位在第一泵装置250,252,254的出口处，以将除冰流体连续地，基本上和直接加热到足以使飞机发射的温度。 该系统还包括第二泵装置212,232，用于引导除冰流体通过发动机210以拾取由发动机210排出的热量。一旦除冰液被泵送通过发动机210，管道或导管装置216,222,228,230,266,264将第二泵的输出 指向第一泵装置250,252和254的入口的装置212,232。
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10.发明授权Apparatus and method for de-icing and anti-icing (and/or cleaning and rinsing) aircraft 失效用于除冰和防冰（和/或清洁和冲洗）飞机的装置和方法
公开(公告)号：US5104068A
公开(公告)日：1992-04-14
申请号：US565963
申请日：1990-08-10
IPC分类号： B64F5/00
CPC分类号： B64F5/0054 , B64F5/0063 , Y02P70/585
摘要： An apparatus for both de-icing and anti-icing an aircraft in one "pass". A pair of units are positioned above and below the aircraft. Each unit has respective nozzles oriented in one direction for dispensing de-icing fluid/air onto the aircraft as it approaches the units. Each unit further has respective nozzles oriented in an opposite direction for dispensing anti-icing fluid/air onto the aircraft as the aircraft moves away from the units. The apparatus is bi-directional so that the aircraft may approach the apparatus from either of two opposite directions. Means are provided for collecting and recycling the run-off of the de-icing and anti-icing fluids, respectively.
摘要翻译： 一种用于在一个“通行证”中对飞机进行除冰和防冰的装置。 一对单元位于飞机上方和下方。 每个单元具有在一个方向上定向的各个喷嘴，用于当飞机接近单元时将除冰流体/空气分配到飞行器上。 每个单元进一步具有相反的方向的喷嘴，用于当飞机从单元移开时将防冰流体/空气分配到飞行器上。 该装置是双向的，使得飞行器可以从两个相反方向中的任一个接近设备。 提供了用于分别收集和回收除冰和防冰流体的流出物的装置。
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