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1. 外观设计

USD355899S Combined pointing device and coupling assembly 失效
公开(公告)号：USD355899S
公开(公告)日：1995-02-28
申请号：US974
申请日：1992-10-30
申请人： Mike M. Paull , Michael D. Nelson , Claire H. Beliard , Domenic S. Giuntoli , Robert C. Evans, III , William P. Stiles
设计人： Mike M. Paull , Michael D. Nelson , Claire H. Beliard , Domenic S. Giuntoli , Robert C. Evans, III , William P. Stiles

2. 发明授权

US5839219A Method of coating a fishing fly and a fishing fly coated thereby 失效
标题翻译：涂覆钓鱼蝇的方法和由此涂覆的钓鱼蝇
公开(公告)号：US5839219A
公开(公告)日：1998-11-24
申请号：US853020
申请日：1997-05-08
申请人： Charles P. Evans , Armand Moscovici , Robert C. Evans
发明人： Charles P. Evans , Armand Moscovici , Robert C. Evans
IPC分类号： A01K85/08 , A01N25/00
CPC分类号： A01K85/08
摘要： A method of coating a fishing fly to improve the durability and wetting character of the fly. The coating is applied using gas deposition, encapsulating the fly with a water barrier while preserving its micro-details. The typical coating is odorless and colorless, and increases the longevity of the fly. The wetting character imparted by the method results from the choice of gas deposited on the fly. In coating a dry-type fly, the method uses a gas that will make the fly hydrophobic so that it floats after a significantly greater number of immersions than an uncoated fly. In coating a wet-type fly, the method uses a gas that will make the fly hydrophilic so that it submerges in less time than an untreated fly.
摘要翻译：一种用于涂覆钓鱼蝇以提高飞行的耐久性和润湿特性的方法。使用气体沉积施加涂层，用防水屏障包封飞行物，同时保留其微细节。典型的涂层无臭无色，增加了飞行的寿命。该方法赋予的润湿特性来自于飞行中沉积的气体的选择。在涂覆干式飞行物时，该方法使用一种气体，其将使疏水性疏水，使得在比未涂布飞行物更多次的浸入之后漂浮。在涂覆湿式飞行物时，该方法使用将使飞行亲水的气体，使其在比未处理的飞行物更短的时间内淹没。

3. 发明授权

US4205813A Thrust vectoring apparatus for a VTOL aircraft 失效
标题翻译：用于垂直起降飞机的推力矢量装置
公开(公告)号：US4205813A
公开(公告)日：1980-06-03
申请号：US916627
申请日：1978-06-19
申请人： Robert C. Evans , Robert C. Ammer
发明人： Robert C. Evans , Robert C. Ammer
IPC分类号： F02K1/78 , B64C29/00 , B64D27/18 , F02K3/02 , B64C15/06
CPC分类号： B64C29/0066 , F02K3/025 , Y02T50/671
摘要： Cascades and associated blocker doors are provided in the lower section of a turbofan engine nacelle such that when the blocker doors are closed the bypass flow is diverted through the open cascades to produce vertical thrust. Vanes are provided in the cascades to assist in directing the diverted airflow in the downward direction. The upper section of the bypass duct is isolated from the lower cascade section by way of horizontal struts extending across the bypass duct. A pair of outer doors may be provided over the cascades such that, when opened, they act to provide side skirts to guide the downward flow of air.
摘要翻译：在涡轮风扇发动机舱的下部设置有级联和相关的阻塞门，使得当阻塞门关闭时，旁路流通过开放级联转向以产生垂直推力。叶片设置在级联中，以帮助将向下的方向引导转向的气流。旁路管道的上部通过横过旁通管道的水平支柱与下级联部分隔离。可以在级联上设置一对外门，使得当打开时，它们用于提供侧裙以引导向下的空气流。

4. 外观设计

USD361759S Pointing device and a coupling assembly 失效
公开(公告)号：USD361759S
公开(公告)日：1995-08-29
申请号：US973
申请日：1992-10-30
申请人： Mike M. Paull , Michael D. Nelson , Claire H. Beliard , Domenic S. Giuntoli , Robert C. Evans, III , William P. Stiles
设计人： Mike M. Paull , Michael D. Nelson , Claire H. Beliard , Domenic S. Giuntoli , Robert C. Evans, III , William P. Stiles

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