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41. 发明授权

US07594627B2 Method and apparatus for de-icing aircraft and other snow or ice covered surfaces 有权
标题翻译：飞机和其他积雪覆冰表面除冰的方法和装置
公开(公告)号：US07594627B2
公开(公告)日：2009-09-29
申请号：US11135245
申请日：2005-05-23
申请人： Pierre Bourgault
发明人： Pierre Bourgault
IPC分类号： B64D15/00
CPC分类号： E01H5/106 , B64F5/20 , B64F5/23
摘要： Methods and devices for deicing aircraft and other snow or ice covered surfaces. The invention is based on warm moisture-laden air or steam that can be released over the surface to be thawed. The device consists of three components: a hot water or steam boiler with an associated pump; a plenum for heating and humidifying air; and a delivery unit or head that brings the moisture-laden air or steam into contact with the surface to be de-iced or thawed. Various delivery heads are also described.
摘要翻译：用于除冰飞机和其他积雪或冰盖表面的方法和设备。本发明基于温暖的含湿空气或蒸汽，其可以在待融化的表面上释放。该装置由三个部件组成：一个热水或带相关泵的蒸汽锅炉; 用于加热和加湿空气的集气室; 以及将含水分的空气或蒸汽与要除冰或解冻的表面接触的输送单元或头部。还描述了各种输送头。

42. 发明申请

US20090095842A1 Power distribution architecture for an ice protection system 有权
标题翻译：防冰系统的配电架构
公开(公告)号：US20090095842A1
公开(公告)日：2009-04-16
申请号：US11974697
申请日：2007-10-15
申请人： James Robert Gaertner, II , Mark Douglas Glewwe , Eric D. Anderson
发明人： James Robert Gaertner, II , Mark Douglas Glewwe , Eric D. Anderson
IPC分类号： B64D15/12 , B64D15/00
CPC分类号： B64D15/12 , B64D2033/0233 , B64D2221/00
摘要： An ice protection system for a vehicle is disclosed which includes a plurality of de-ice power distribution units positioned proximate to a leading edge surface of the vehicle that is susceptible to ice accretion, at least two anti-ice power distribution units located within the vehicle, spaced from the de-ice power distribution units, and a point of power regulation located within the vehicle, spaced from the power distribution units, from which power is fed to the power distribution units through independent feeder wire bundles so as to distribute line current across the system in a manner that optimizes wire weight.
摘要翻译：公开了一种用于车辆的防冰系统，其包括位于车辆前缘表面附近易于积冰的多个除冰配电单元，位于车辆内的至少两个防冰配电单元与除冰配电单元间隔开的功率调节点和位于车辆内的功率调节点与配电单元间隔开，电力通过独立的馈电线束供电到配电单元，以便分配线路电流跨系统以优化线重量的方式。

43. 发明授权

US6089505A Mission adaptive inlet 失效
标题翻译：任务适应入口
公开(公告)号：US6089505A
公开(公告)日：2000-07-18
申请号：US898162
申请日：1997-07-22
申请人： Cynthia Ann Gruensfelder , Robert Henry Wille
发明人： Cynthia Ann Gruensfelder , Robert Henry Wille
IPC分类号： B64D33/02 , F02C7/042 , B64B1/24 , B64C1/38 , B64D15/00 , F02B27/00
CPC分类号： B64D33/02 , F02C7/042 , B64D2033/026 , B64D2033/0286 , Y02T50/672
摘要： A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position. A reinforced elastomer system (48) is connected the rigid lip panel and the inlet (42).
摘要翻译：用于飞行器（40）的任务自适应入口（42）具有枢转地附接到飞行器（40）的入口（42）的刚性唇板（56）。致动机构联接到刚性唇板（56）并使刚性唇板（56）从第一位置枢转到第二位置。加强弹性体系统（48）连接刚性唇板和入口（42）。

44. 再颁专利

USRE36468E Method of, and apparatus for, de-icing an aircraft by infrared radiation 失效
标题翻译：用于通过红外辐射除冰飞机的方法和装置
公开(公告)号：USRE36468E
公开(公告)日：1999-12-28
申请号：US861478
申请日：1997-05-22
申请人： Charles J. Chew , Timothy P. Seel
发明人： Charles J. Chew , Timothy P. Seel
IPC分类号： B64F5/00 , B64D15/00
CPC分类号： B64F5/0072
摘要： An improved apparatus (11) for emitting infrared radiation of a desired wavelength includes a primary surface (.[.35.]. .Iadd.25.Iaddend.); a burner (24) for raising the temperature of the primary surface so as to cause the primary surface to emit infrared radiation of a first wavelength; a secondary surface (26) surrounding the primary surface in spaced relation thereto and arranged to be heated by infrared radiation emitted by the first surface and for emitting infrared radiation of a second wavelength toward the object; and an actuator (28) for selectively varying the spacing between the primary and secondary surfaces so that infrared radiation emitted by the secondary surface .[.will be at a desired wavelength and.]. will be focused; whereby the apparatus will emit infrared radiation of a desired wavelength toward the object. The improved apparatus may be used in a method of de-icing a portion of an aircraft, which includes the steps of: providing a structure (10) having an infrared heater (23); moving an aircraft relative to the structure to a position adjacent the heater; operating the heater so as to emit radiation toward the object; and controlling the wavelength of radiation emitted by the heater; thereby to melt snow and ice from the aircraft portion.
摘要翻译：用于发射所需波长的红外辐射的改进的装置（11）包括主表面（25）; 用于升高所述主表面的温度以使所述主表面发射第一波长的红外辐射的燃烧器（24）; 第二表面（26）围绕主表面与其间隔开并且被布置成被第一表面发射的红外辐射加热并且用于向物体发射第二波长的红外辐射; 以及用于选择性地改变主表面和次表面之间的间隔的致动器（28），使得由次表面[将处于期望的波长和]发射的红外辐射将被聚焦; 由此该装置将朝向物体发射所需波长的红外辐射。改进的装置可以用于除冰飞机的一部分的方法，其包括以下步骤：提供具有红外加热器（23）的结构（10）; 将飞机相对于结构移动到靠近加热器的位置; 操作加热器以朝向物体发射辐射; 并控制加热器发射的辐射波长; 从而从飞机部分融化雪和冰。

45. 发明授权

US5934617A De-ice and anti-ice system and method for aircraft surfaces 失效
标题翻译：防冰和防冰系统和飞机表面的方法
公开(公告)号：US5934617A
公开(公告)日：1999-08-10
申请号：US935165
申请日：1997-09-22
申请人： Robert B. Rutherford
发明人： Robert B. Rutherford
IPC分类号： B64D15/12 , B64D15/14 , B64D15/00 , B64C1/00
CPC分类号： B64D15/14
摘要： A thermal de-ice and anti-ice system for aircraft surfaces employs a laminate in which flexible expanded graphite foil is an electrical and heat conducting layer that is disposed below an outer heat conducting layer, with an electrically insulating layer below the graphite layer. The flexible expanded graphite layer requires about three times less wattage than known resistance heating pad thermal systems to achieve de-ice and/or anti-ice temperatures. The temperature of the surface is controlled by varying the power supplied to the flexible expanded graphite layer of the laminate in response to a real time temperature value transmitted to a power control.
摘要翻译：用于飞行器表面的热去冰和防冰系统采用层压板，其中柔性膨胀石墨箔是布置在外部导热层下方的电和导热层，在石墨层下方具有电绝缘层。柔性膨胀石墨层比已知的电阻加热垫热系统要求的功率要低三倍，以实现去冰和/或抗冰温度。响应于传输到功率控制器的实时温度值，改变提供给层压板的柔性膨胀石墨层的功率来控制表面的温度。

46. 发明授权

US5857646A Aircraft de-icing and recovery system 失效
标题翻译：飞机除冰和回收系统
公开(公告)号：US5857646A
公开(公告)日：1999-01-12
申请号：US634954
申请日：1996-04-19
申请人： Todd Taricco
发明人： Todd Taricco
IPC分类号： B64F5/00 , B64D15/00
CPC分类号： B64F5/0054 , B64F5/0063 , Y02P70/585
摘要： A system for collecting and recovering de-icing fluid that is sprayed onto an aircraft. The de-icing system includes a mat that is assembled onto the approaching ramp of a runway. The de-icing mat has a plurality of channels that collect and direct the de-icing fluid to the outer edges of the mat. The de-icing fluid is removed from the mat by a vacuum system. Coupled to the vacuum system is a filter system that separates the de-icing fluid from other fluids such as oil, water, etc., so that the de-icing fluid can be used again. The mat has a plurality of heating elements that prevent the de-icing fluid from freezing on the mat and provide heat to the underside of the aircraft.
摘要翻译：用于收集和回收喷射到飞行器上的除冰流体的系统。除冰系统包括组装到跑道接近坡道上的垫子。除冰垫具有多个通道，其收集并将除冰流体引导到垫的外边缘。除冰液体通过真空系统从垫中除去。耦合到真空系统的是将除冰流体与其它流体如油，水等分离的过滤系统，从而可以再次使用除冰液。垫具有多个加热元件，其防止除冰流体在垫上冻结并向飞行器的下侧提供热量。

47. 发明授权

US5845878A Skin for a deicer 失效
公开(公告)号：US5845878A
公开(公告)日：1998-12-08
申请号：US628363
申请日：1996-08-06
申请人： Richard Lawrence Rauckhorst, III , Kevin Lee Leffel
发明人： Richard Lawrence Rauckhorst, III , Kevin Lee Leffel
IPC分类号： B64D15/16 , B64D15/18 , B64D15/00
CPC分类号： B64D15/16 , B64D15/166
摘要： An aircraft deicing assembly 101 for attachment to an airfoil 99 includes a deflection shell 101 disposed over a deflection means 102. The deflection shell is comprised of a primary layer 116 comprised of a high strength fabric reinforced with a phenolic resin and a backing layer 115 comprised of a high strength fabric reinforced with an epoxy resin. The thickness of the backing layer is varied as a function of curvature of the airfoil and spanwise length of the airfoil.

48. 发明授权

US5634800A Sliding contact for a propeller ice protection system 失效
标题翻译：螺旋桨防冰系统的滑动接触
公开(公告)号：US5634800A
公开(公告)日：1997-06-03
申请号：US235828
申请日：1994-04-29
申请人： Michael J. Giamati
发明人： Michael J. Giamati
IPC分类号： B64D15/00 , H01R39/10 , H01R39/22
CPC分类号： B64D15/00 , H01R39/10 , H01R39/22
摘要： An improved sliding contact for use with a propeller ice protection system is provided. According to an aspect of the invention, a silver graphite brush forms a sliding contact with a hardened copper alloy slip ring. A sliding contact according to the invention demonstrates improved performance in an oil contaminated environment.
摘要翻译：提供了一种与螺旋桨防冰系统一起使用的改进的滑动接触。根据本发明的一个方面，银石墨刷与硬化的铜合金滑环形成滑动接触。根据本发明的滑动接触显示出在油污染的环境中改进的性能。

49. 发明授权

US5575441A Fuel liquid/vapor vent containment/recovery system 失效
标题翻译：燃油液/蒸气泄压收集/回收系统
公开(公告)号：US5575441A
公开(公告)日：1996-11-19
申请号：US345182
申请日：1994-11-28
申请人： James R. Gervais , Walter S. Lambert
发明人： James R. Gervais , Walter S. Lambert
IPC分类号： B64D37/14 , B64D15/00
CPC分类号： B64D37/14
摘要： The present invention provides a device for preventing the venting of fuel vapor to the atmosphere and liquid fuel spillage on military aircraft having vent/dump outlets thereon. On the F-15 fighter aircraft, for example, a dump mast is located on the trailing edge of a wing. The dump mast, externally, consists of a oblong walled outlet which is slanted consistent with the trailing edge. An adaptor is placed over the walled outlet and may be held in place by straps or clips. The adaptor has a reducer further attached thereon for the purpose of connecting to a standard hose. The hose therefrom may be returned to the fuel truck for collection of vapor or dumped fuel.
摘要翻译：本发明提供一种用于防止燃料蒸气排放到大气中并在其上具有通风/排放出口的军用飞机上的液体燃料溢出的装置。例如，在F-15战机上，倾倒式桅杆位于机翼的后缘。倾倒式桅杆在外部包括一个与后缘一致倾斜的长方形墙壁出口。适配器放置在有壁的出口上，并可通过带子或夹子保持在适当位置。适配器具有进一步连接到其上的减速器，用于连接到标准软管。其中的软管可以返回到燃料车辆以收集蒸气或倾倒的燃料。

50. 发明授权

US5575440A Procedure and devices to determine the severity of icing conditions for an aircraft 失效
标题翻译：确定飞机结冰条件严重程度的程序和设备
公开(公告)号：US5575440A
公开(公告)日：1996-11-19
申请号：US348086
申请日：1994-11-25
申请人： Henri LeBlond , Joel Choisnet , Gregoire Dodel
发明人： Henri LeBlond , Joel Choisnet , Gregoire Dodel
IPC分类号： B64D15/20 , B64D15/00
CPC分类号： B64D15/20
摘要： A method and apparatus for determining the severity of icing conditions for an aircraft in flight. A mobile probe projecting from a surface of the aircraft is heated to a predetermined range of temperatures, and the total power required for the heating is measured. The measured total power is divided into a basic power corresponding to the thermal exchange in dry air having the same flow parameters as those measured and a complimentary power corresponding to the evaporating of drops of water contained in the actual air. A parameter representative of the speed at which the thickness of ice increases at the surface of the aircraft is computed from the complementary power.
摘要翻译：一种用于确定飞行中的飞行器的结冰条件的严重性的方法和装置。将从飞行器表面突出的移动探针加热到预定的温度范围，并测量加热所需的总功率。测量的总功率被分为与干空气中的热交换相对应的基本功率，其具有与测量的相同的流量参数，以及对应于包含在实际空气中的水滴蒸发的互补功率。从互补功率计算表示在飞机表面处冰的厚度增加的速度的参数。

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