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1. 发明授权

US08411214B2 Variably transmittive, electronically-controlled eyewear 有权
标题翻译：可变透射电子控制眼镜
公开(公告)号：US08411214B2
公开(公告)日：2013-04-02
申请号：US12144937
申请日：2008-06-24
申请人： John J. Chapman , Louis J. Glaab , Timothy D. Schott , Charles T. Howell , Vincent J. Fleck
发明人： John J. Chapman , Louis J. Glaab , Timothy D. Schott , Charles T. Howell , Vincent J. Fleck
IPC分类号： G02F1/1335
CPC分类号： G09B9/36 , G09B9/30 , G09B9/307
摘要： A system and method for flight training and evaluation of pilots comprises electronically activated vision restriction glasses that detect the pilot's head position and automatically darken and restrict the pilot's ability to see through the front and side windscreens when the pilot-in-training attempts to see out the windscreen. Thus, the pilot-in-training sees only within the aircraft cockpit, forcing him or her to fly by instruments in the most restricted operational mode.
摘要翻译：飞行员的飞行训练和评估的系统和方法包括电子激活的视力限制眼镜，其检测飞行员的头部位置，并且当驾驶员在训练中试图看到时，自动变暗并且限制飞行员通过前侧挡风玻璃和侧面挡风玻璃的能力挡风玻璃。因此，驾驶员在训练中只能在飞机驾驶舱内看到，迫使他或她以最受限制的作战模式飞行。

2. 发明申请

US20090317773A1 Variably Transmittive, Electronically-Controlled Eyewear 有权
标题翻译：可变透明电子控制眼镜
公开(公告)号：US20090317773A1
公开(公告)日：2009-12-24
申请号：US12144937
申请日：2008-06-24
申请人： John J. Chapman , Louis J. Glaab , Timothy D. Schott , Charles T. Howell , Vincent J. Fleck
发明人： John J. Chapman , Louis J. Glaab , Timothy D. Schott , Charles T. Howell , Vincent J. Fleck
IPC分类号： G09B9/36 , G02F1/17 , G02F1/1335
CPC分类号： G09B9/36 , G09B9/30 , G09B9/307
摘要： A system and method for flight training and evaluation of pilots comprises electronically activated vision restriction glasses that detect the pilot's head position and automatically darken and restrict the pilot's ability to see through the front and side windscreens when the pilot-in-training attempts to see out the windscreen. Thus, the pilot-in-training sees only within the aircraft cockpit, forcing him or her to fly by instruments in the most restricted operational mode.
摘要翻译：飞行员的飞行训练和评估的系统和方法包括电子激活的视力限制眼镜，其检测飞行员的头部位置，并且当驾驶员在训练中试图看到时，自动变暗并且限制飞行员通过前侧挡风玻璃和侧面挡风玻璃的能力挡风玻璃。因此，驾驶员在训练中只能在飞机驾驶舱内看到，迫使他或她以最受限制的作战模式飞行。

3. 发明授权

US4767484A Method of attaching strain gauges to various materials 失效
标题翻译：将应变计连接到各种材料的方法
公开(公告)号：US4767484A
公开(公告)日：1988-08-30
申请号：US74792
申请日：1987-07-17
申请人： Timothy D. Schott , Robert L. Fox , John D. Buckley
发明人： Timothy D. Schott , Robert L. Fox , John D. Buckley
IPC分类号： B29C65/36 , G01L1/22 , H05B6/10 , B44C1/14 , B32B31/12 , B32B31/20 , B32B31/26
CPC分类号： G01L1/2287 , B29C65/3644 , B29C66/472 , B29C66/8322 , Y10T156/1158
摘要： A method is provided to bond strain gauges 6 to various materials. First, a tape 9 with an adhesive backing 10 is placed across the inside of fixture frame 8. Strain gauge 6 is flatly placed against adhesive backing 10 and coated with a thin, uniform layer of adhesive 5. Tape 9 is then removed from fixture frame 8 and placed, strain gauge side down, on the material to be tested. If the material is a high reluctance material 12, induction heating source 20 is placed upon tape 9. If the material is a low reluctance material 13, a plate 23 with a ferric side 21 and a rubber side 22 is placed, ferric side down, onto tape 9. Induction heating source 20 is then placed upon rubber side 22. If the material is an insulator material 14, a ferric plate 7 is placed on tape 9. Induction heating source 20 is then placed on ferric plate 7. Inductive heating source 20 then generates frequency from 60 to 70 kilocycles to inductively heat either low reluctance material 13, ferric side 21, or ferric plate 21 and provides incidental pressure of approximately five pounds per square inch to tape 9 for two minutes, thoroughly curing adhesive 5. Induction heating source 20, and, if necessary, plate 23 or ferric plate 7, are then removed from tape 9 after one minute. Tape 9 is then removed from bonded strain gauge 6.
摘要翻译：提供了一种将应变计6粘合到各种材料上的方法。首先，具有粘合剂背衬10的带9横跨固定框架8的内部放置。应变计6被平坦地放置在粘合剂背衬10上并涂覆有薄的均匀的粘合剂层5.然后将带9从夹具框架 8并将应变计侧面放置在要测试的材料上。如果材料是高磁阻材料12，则感应加热源20被放置在带9上。如果材料是低磁阻材料13，则将具有铁质侧面21和橡胶侧22的板23放置在铁面侧，然后将感应加热源20放置在橡胶侧22.如果材料是绝缘体材料14，则将铁板7放置在带9上。然后将感应加热源20放置在铁板7上。感应加热源 20然后产生60至70千圈的频率以感应加热低磁阻材料13，铁侧21或铁板21，并且向带9提供约5磅/平方英寸的附带压力2分钟，彻底固化粘合剂5.感应加热源20，如有需要，然后在一分钟之后从带9上取下板23或铁板7。然后将带9从结合的应变片6中取出。

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