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1. 发明授权

US06787782B1 Ultraviolet-light vehicle air cleaning system 有权
标题翻译：紫外线车辆空气净化系统
公开(公告)号：US06787782B1
公开(公告)日：2004-09-07
申请号：US10421296
申请日：2003-04-23
申请人： Mark D. Krosney , Joseph Baughman , Richard L. Rauckhorst, III , Michael G. Casto , Tolek Pawelko , Jennifer L. Gloisten , William E. Reisenauer
发明人： Mark D. Krosney , Joseph Baughman , Richard L. Rauckhorst, III , Michael G. Casto , Tolek Pawelko , Jennifer L. Gloisten , William E. Reisenauer
IPC分类号： G01N2101
CPC分类号： A61L9/20 , B60H3/06
摘要： A system for cleaning air in a vehicle by ultraviolet light includes an exposure chamber for exposure of air to ultraviolet light. An ultraviolet light source is mounted in the exposure chamber. A collection plenum chamber is connected to a first end of the exposure chamber. An air valve is connected to the collection plenum chamber. An expansion plenum chamber is connected to a second end of the exposure chamber including passages for distribution of air to the exposure chamber. An inlet conduit connected to the expansion plenum chamber directs air to the expansion plenum chamber. The system reliably cleans air and may be packaged so as to be integrated into existing vehicle structures, such as a passenger service unit of an airplane.
摘要翻译：用于通过紫外线清洁车辆中的空气的系统包括用于将空气暴露于紫外线的曝光室。紫外光源安装在曝光室中。收集室室连接到曝光室的第一端。空气阀连接到收集室室。膨胀增压室连接到曝光室的第二端，包括用于将空气分配到曝光室的通道。连接到膨胀增压室的入口导管将空气引导到膨胀增压室。该系统可靠地清洁空气并且可以被包装以便被集成到诸如飞机的乘客服务单元的现有的车辆结构中。

2. 发明授权

US5609314A Skin for a deicer 失效
标题翻译：皮肤为一个除冰机
公开(公告)号：US5609314A
公开(公告)日：1997-03-11
申请号：US485751
申请日：1995-06-07
申请人： Richard L. Rauckhorst, III , Kevin L. Leffel
发明人： Richard L. Rauckhorst, III , Kevin L. 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.
摘要翻译：用于附接到翼型件99的飞机除冰组件101包括设置在偏转装置102上的偏转壳体101.偏转壳体包括由用酚醛树脂增强的高强度织物和包含背衬层115的主层116组成的高强度织物用环氧树脂增强。背衬层的厚度作为翼型的曲率和翼型的翼展长度的函数而变化。

3. 发明授权

US5356096A Skin for a deicer 失效
标题翻译：皮肤为一个除冰机
公开(公告)号：US5356096A
公开(公告)日：1994-10-18
申请号：US998360
申请日：1992-12-30
申请人： Richard L. Rauckhorst, III , Kevin L. Leffel
发明人： Richard L. Rauckhorst, III , Kevin L. Leffel
IPC分类号： B64D15/16 , B64D15/18 , B64D15/00
CPC分类号： 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.
摘要翻译：用于附接到翼型件99的飞机除冰组件101包括设置在偏转装置102上的偏转壳体101.偏转壳体包括由用酚醛树脂增强的高强度织物和包含背衬层115的主层116组成的高强度织物用环氧树脂增强。背衬层的厚度作为翼型的曲率和翼型的翼展长度的函数而变化。

4. 发明授权

US06384611B1 Ice thickness detector 失效
标题翻译：冰厚探测器
公开(公告)号：US06384611B1
公开(公告)日：2002-05-07
申请号：US08971801
申请日：1997-11-17
申请人： Randall W. Wallace , Allen D. Reich , David B. Sweet , Richard L. Rauckhorst, III , Michael J. Terry , Marc E. Holyfield
发明人： Randall W. Wallace , Allen D. Reich , David B. Sweet , Richard L. Rauckhorst, III , Michael J. Terry , Marc E. Holyfield
IPC分类号： G01R2726
CPC分类号： B64D15/20
摘要： An ice detector includes a pair of electrodes connected by a pair of leads to a control unit which measures the admittance between leads to thereby sense and detect the presence of ice and other contaminants formed on top thereof utilizing a detection circuit. The electrodes are integrated into patch which can be placed at different locations on an aircraft.
摘要翻译：冰检测器包括通过一对引线连接到控制单元的一对电极，该控制单元测量引线之间的导纳，从而利用检测电路感测并检测在其顶部形成的冰和其它污染物的存在。电极被集成到可以放置在飞机上的不同位置的补片中。

5. 发明授权

US5813631A Pneumatic deicing system with drain valve 失效
标题翻译：带排水阀的气动除冰系统
公开(公告)号：US5813631A
公开(公告)日：1998-09-29
申请号：US804774
申请日：1997-02-24
申请人： Donald E. Butler , Richard L. Rauckhorst, III , Thomas A. Waples , Alan J. Fahrner
发明人： Donald E. Butler , Richard L. Rauckhorst, III , Thomas A. Waples , Alan J. Fahrner
IPC分类号： B64D15/16 , B64D15/18
CPC分类号： B64D15/166
摘要： A pneumatic deicing system includes a deicer assembly comprised of an outer layer, an inner ply, and a plurality of inflatable members provided therebetween. The deicer assembly is disposed directly on top of and bonded to an airfoil. The deicer assembly is inflated through an inflation port. Fluid is drained from the deicer assembly through a drain valve.
摘要翻译：气动除冰系统包括由外层，内层和设置在其间的多个可充气构件组成的除冰组件。除冰机组件直接设置在翼型件的顶部并结合到翼型件上。除冰机组件通过充气口充气。流体通过排水阀从除冰机组件中排出。

6. 发明授权

US5569850A Ice detector 失效
标题翻译：冰探测器
公开(公告)号：US5569850A
公开(公告)日：1996-10-29
申请号：US437004
申请日：1995-05-08
申请人： Richard L. Rauckhorst, III
发明人： Richard L. Rauckhorst, III
IPC分类号： B64D15/20 , G01N29/09 , G02N1/00
CPC分类号： G01N29/09 , B64D15/20 , G01N2291/018 , G01N2291/0251 , Y10T29/49082
摘要： An ice detector 110 includes a pair of electrodes 122, 124 connected by a pair of leads 116, 118 to a control unit 120 which measures the impedance (or other parameters) between leads 116 and 118 to thereby sense and detect ice or other contaminants formed on top thereof. Electrodes 122, 124 are integrated into patch 134 and comprised of a top layer 142 of conductive resin, a middle layer 144 of conductive cloth and a bottom layer 146 of conductive resin.
摘要翻译：冰检测器110包括由一对引线116,118连接到控制单元120的一对电极122,124，控制单元120测量引线116和118之间的阻抗（或其他参数），从而感测并检测形成的冰或其他污染物在其顶部。电极122,124集成在贴片134中，由导电树脂的顶层142，导电布的中间层144和导电树脂的底层146组成。

7. 发明授权

US5562265A Vibrating pneumatic deicing system 失效
标题翻译：振动气动除冰系统
公开(公告)号：US5562265A
公开(公告)日：1996-10-08
申请号：US322905
申请日：1994-10-13
申请人： Richard L. Rauckhorst, III
发明人： Richard L. Rauckhorst, III
IPC分类号： B64D15/16 , B64D15/00
CPC分类号： B64D15/166
摘要： A pneumatic deicing system includes a deicer assembly comprised of an outer layer having a low modulus of elasticity, an inner ply, and a plurality of inflatable members provided therebetween. The deicer assembly is disposed directly on top of and bonded to an airfoil. The inflatable members are inflated with an inflation apparatus that inflates in an inflation pattern comprised of a sequence of high frequency pressure pulses superimposed on a low frequency inflation pressure wave.
摘要翻译：气动除冰系统包括除霜组件，其由具有低弹性模量的外层，内层和设置在它们之间的多个可充气构件组成。除冰器组件直接设置在翼型件的顶部并结合到翼型件上。充气构件用膨胀装置充气，该膨胀装置以叠加在低频充气压力波上的一系列高频压力脉冲的膨胀模式膨胀。

8. 发明授权

US5489073A Side flex leading edge ice protector 失效
标题翻译：侧面前缘冰保护器
公开(公告)号：US5489073A
公开(公告)日：1996-02-06
申请号：US149873
申请日：1993-11-10
申请人： Kevin L. Leffel , Richard L. Rauckhorst, III
发明人： Kevin L. Leffel , Richard L. Rauckhorst, III
IPC分类号： B64D15/16 , B64D15/00
CPC分类号： B64D15/166
摘要： An airfoil deicing system includes an airfoil substructure having an apex corresponding to the portion of the airfoil where the radius of curvature of the airfoil is smallest, the airfoil and the apex being bisected by a centerline, a deflectable shell disposed over the airfoil substructure for meeting and breaking an impinging airstream, a deflection means disposed between the airfoil substructure and the deflectable shell at the apex for deflecting the deflectable shell in the area of the apex away from the airfoil substructure and, at least one compressible zones provided beneath the deflectable shell adjacent the apex on either side of the centerline, the compressible zones facilitating deflection of the deflectable shell overlying the compressible zones toward the airfoil substructure when the deflection means deflects the deflectable shell.
摘要翻译：机翼除冰系统包括翼型底座，其具有对应于翼型部分的翼部的顶点，其中翼型的曲率半径最小，翼型和顶点由中心线平分，位于翼型子结构上方的可偏转壳，以满足并且破坏冲击的气流，偏转装置设置在所述翼型底座结构和所述顶点处的所述可偏转壳体之间，用于使所述顶点区域中的所述可偏转壳体偏离所述翼型件底部结构，以及设置在所述可偏转壳体下方的至少一个可压缩区域中心线两侧的顶点，当偏转装置偏转可偏转的壳体时，可压缩区域有助于偏转可压缩的壳体覆盖可压缩区域朝向翼型件子结构的偏转。

9. 发明授权

US5553814A Skin for a deicer 失效
标题翻译：皮肤为一个除冰机
公开(公告)号：US5553814A
公开(公告)日：1996-09-10
申请号：US253027
申请日：1994-06-02
申请人： Richard L. Rauckhorst, III , Kevin L. Leffel
发明人： Richard L. Rauckhorst, III , Kevin L. Leffel
IPC分类号： B64D15/16 , B64D15/18 , B64D15/00
CPC分类号： 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.
摘要翻译：用于附接到翼型件99的飞机除冰组件101包括设置在偏转装置102上的偏转壳体101.偏转壳体包括由用酚醛树脂增强的高强度织物和包含背衬层115的主层116组成的高强度织物用环氧树脂增强。背衬层的厚度作为翼型的曲率和翼型的翼展长度的函数而变化。

10. 发明授权

US5427332A Modular ice protection assembly 失效
标题翻译：模块化防冰组件
公开(公告)号：US5427332A
公开(公告)日：1995-06-27
申请号：US149875
申请日：1993-11-10
申请人： Richard L. Rauckhorst, III , Kevin L. Leffel
发明人： Richard L. Rauckhorst, III , Kevin L. Leffel
IPC分类号： B64D15/16 , B64D15/18 , B64C1/34
CPC分类号： B64D15/16
摘要： A modular ice protection system for an airfoil includes a deflection assembly attached to the airfoil and a removable outer shell having a modulus of elasticity of at least 40,000 kPa impermanently disposed over the deflection assembly, wherein the deflection assembly causes distortion of the separable outer shell during de-icing. The deflection assembly may likewise be removable from an underlying substructure which is attached to the airfoil.
摘要翻译：用于翼型件的模块化防冰系统包括附接到翼型件的偏转组件和经常设置在偏转组件上方的具有至少40,000kPa的弹性模量的可移除外壳，其中偏转组件引起可分离的外壳在除冰偏转组件同样可以从附接到翼型件的底部子结构移除。

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