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1. 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。

2. 发明授权

US5597140A Infrared deicers for aircraft positioned on a taxiway and methods for using same 失效
标题翻译：位于滑行道上的飞机的红外线除冰器及其使用方法
公开(公告)号：US5597140A
公开(公告)日：1997-01-28
申请号：US372066
申请日：1995-01-12
申请人： Robert C. Madsen
发明人： Robert C. Madsen
IPC分类号： B64F5/00 , H05B3/00 , B64D15/00 , B64D15/12
CPC分类号： B64F5/0072 , Y02P70/585
摘要： An apparatus for deicing an aircraft is defined by an insulated shelter being a size capable of enclosing an aircraft. The shelter is positioned on a deicing surface that absorbs heat from means such as electrical filaments or heated pipes within the deicing surface or through the application of infrared radiation onto the deicing surface. In turn, the deicing surface radiates heat into the air within the shelter. Once an aircraft is enclosed within the shelter, infrared radiation is applied to a portion of the exterior surface of the aircraft. The combination of the infrared radiation and the heat radiating from the deicing surface rapidly deices and substantially dries the exterior surface of the aircraft. The exterior of the aircraft is subsequently heated to a sufficiently high temperature that ice will not reform on the aircraft prior to take off.
摘要翻译：用于除冰飞机的装置由能够封闭飞机的尺寸的绝缘防护罩限定。遮蔽物定位在除冰表面上，该除冰表面从除冰表面内的电线或加热管等装置吸收热量，或通过将红外辐射施加到除冰表面上。反过来，除冰表面将热量散发到避难所内的空气中。一旦飞机被封闭在避难所内，红外辐射被施加到飞行器外表面的一部分。红外线辐射和从除冰表面辐射的热量的组合迅速脱落并使飞机的外表面基本上变干。飞机的外部随后被加热到足够高的温度，使冰在起飞前不会在飞机上重新形成。

3. 发明授权

US5417389A 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：US5417389A
公开(公告)日：1995-05-23
申请号：US207883
申请日：1994-03-07
申请人： Charles J. Chew , Timothy P. Seel
发明人： Charles J. Chew , Timothy P. Seel
IPC分类号： B64F5/00 , B64D20060101 , B64D15/00 , F24C1/12
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); 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装置（11）包括主表面（35）; 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），使得由次表面发射的红外辐射将处于期望的波长并将被聚焦; 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。

4. 发明授权

US4900891A Laser ice removal system 失效
标题翻译：激光除冰系统
公开(公告)号：US4900891A
公开(公告)日：1990-02-13
申请号：US208453
申请日：1988-06-20
申请人： Roger Vega , Rose M. Vega
发明人： Roger Vega , Rose M. Vega
IPC分类号： B08B7/00 , B23K7/06 , B23K26/40 , B64F5/00
CPC分类号： B64F5/0072 , B08B7/0042 , B23K26/40 , B23K26/402 , B23K2203/36 , B23K2203/50 , B23K7/06
摘要： A system to remove ice formed on a surface, such as an airplane wing. Heat generative laser beam is directed upon a snow or ice-covered surface, thereby vaporizing the ice and snow formed thereupon. By translating the laser light generator along the frozen surface, vaporization of the snow and ice formed on the entire surface takes place.
摘要翻译：用于去除在诸如飞机机翼的表面上形成的冰的系统。发热激光束被引导到积雪或冰覆盖的表面上，从而蒸发在其上形成的冰和雪。通过沿着冷冻表面平移激光发生器，发生在整个表面上形成的积雪和冰的蒸发。

5. 发明授权

US6092765A Infrared deicing system for aircraft 失效
标题翻译：飞机红外除冰系统
公开(公告)号：US6092765A
公开(公告)日：2000-07-25
申请号：US84706
申请日：1998-05-26
申请人： Richard P. White
发明人： Richard P. White
IPC分类号： B64D15/00 , B64F5/00
CPC分类号： B64F5/0072 , B64D15/00
摘要： Flameless infrared catalytic heater units are mounted in a generally wing-shaped carrier for positioning above surfaces of an aircraft. The carrier is attached to a boom end extending from a truck or other suitable self-propelled ground equipment. A temperature sensor bounces an infrared signal off the aircraft surface and inputs the skin temperature into a micro-controller regulating the output of the infrared heater units. The micro controller maintains a desired safe skin temperature sufficient to melt ice and snow from the aircraft surfaces without blistering the paint or raising concern about temperatures within fuel tanks. The catalytic heater units use inexpensive natural gas or propane. Use of this system substitutes for expensive and hazardous ethylene glycol solutions heretofore sprayed over the aircraft.
摘要翻译：无焰红外线催化加热器单元安装在大体翼形的载体上，用于定位飞机表面上方。托架附接到从卡车或其他合适的自走式地面设备延伸的起重臂端部。温度传感器将红外信号从飞机表面反射并将皮肤温度输入到调节红外加热器单元输出的微控制器中。微型控制器保持所需的安全皮肤温度足以从飞行器表面融化冰雪，而不会使油漆起泡或引起对燃料箱内温度的担忧。催化加热器单元使用便宜的天然气或丙烷。使用该系统将昂贵且有害的乙二醇溶液替代到飞机上喷洒。

6. 发明授权

US5823474A Aircraft ice detection and de-icing using lasers 失效
标题翻译：使用激光的飞机冰检测和除冰
公开(公告)号：US5823474A
公开(公告)日：1998-10-20
申请号：US706598
申请日：1996-09-05
申请人： William C. Nunnally
发明人： William C. Nunnally
IPC分类号： B64F5/00 , B64D15/00
CPC分类号： B64F5/0072
摘要： An aircraft ice detection and de-icing system is disclosed in which an aircraft is positioned remotely from a laser beam generator, a beam of radiant energy is reflected from a mirror so that the beam impinges upon and creates a footprint upon a surface of the aircraft and the mirror is manipulated to move the footprint about the aircraft surface. The beam has a wavelength that is preferentially reflected by the aircraft surface and absorbed by ice, snow and water, so the beam heats and removes ice, snow and water from aircraft surfaces as the beam's footprint is moved thereabouts. A remote thermal monitoring system may also be used to monitor temperatures at the aircraft surface for detecting regions experiencing temperature rises at relatively increased rates as the regions are treated with the beam, thereby indicating the presence of ice, snow or water. A visible light may also be used simultaneously to track and indicate movement of the footprint of the treating beam about the aircraft surface.
摘要翻译：公开了一种飞机冰检测和除冰系统，其中飞行器远离激光束发生器定位，辐射能束从反射镜反射，使得射束撞击并在飞行器的表面上产生占地面积并且操纵镜子以移动飞机表面周围的足迹。光束具有优先由飞机表面反射并被冰，雪和水吸收的波长，因此当光束的足迹移动到该处时，光束加热并从飞机表面去除冰，雪和水。远程热监测系统也可用于监测飞行器表面的温度，以便在用波束处理区域时，以相对增加的速率检测经历温度升高的区域，从而指示冰，雪或水的存在。也可以同时使用可见光来跟踪和指示处理束围绕飞机表面的足迹的移动。

7. 发明授权

US5558303A Method and apparatus for using hot fuels to de-ice aircraft 失效
标题翻译：使用热燃料去除飞机的方法和装置
公开(公告)号：US5558303A
公开(公告)日：1996-09-24
申请号：US364301
申请日：1994-12-27
申请人： Terence L. Koethe , Richard M. Wilson , Gary L. Reid
发明人： Terence L. Koethe , Richard M. Wilson , Gary L. Reid
IPC分类号： B64F5/00 , B64D15/02
CPC分类号： B64F5/0072 , Y10T137/6552
摘要： A method and apparatus are provided for de-icing an aircraft of the type having wings and fuel storage in the wings. Hot fuel is provided for fueling the aircraft. The hot fuel is at elevated temperatures which are sufficiently high enough to transfer heat from the fuel, through a fuel tank extending within the wings, and to the exterior of the wings to de-ice the aircraft. A storage tank stores the fuel, and a heater heats the fuel to elevated temperatures. An intermediate thermal transfer system having a secondary thermal fluid transfers heat from a primary power source to the fuel. Further, a substantial volume of the secondary thermal fuel may be maintained at elevated temperatures to provide a sufficient thermal reserve capacity for heating the fuel upon demand.
摘要翻译：提供一种方法和装置，用于使具有机翼和燃料储存在翼中的类型的飞机除冰。提供热燃料来加油飞机。热燃料处于升高的温度，这些高温足够高以从燃料传递热量，通过在翼内延伸的燃料箱以及机翼的外部来使飞机脱冰。储罐储存燃料，加热器将燃料加热到升高的温度。具有次级热流体的中间热传递系统将热量从主电源传递到燃料。此外，大量的二次热燃料可以保持在升高的温度下，以提供足够的热储备容量以根据需要加热燃料。

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