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1. 发明授权

US4534293A Coiled curvilinear solid propellant grain 失效
标题翻译：卷曲曲线固体推进剂颗粒
公开(公告)号：US4534293A
公开(公告)日：1985-08-13
申请号：US667315
申请日：1984-11-01
申请人： Ben F. Wilson
发明人： Ben F. Wilson
IPC分类号： F02K9/22 , C06D5/06
CPC分类号： F02K9/22
摘要： A curvilinear solid propellant gas generator which includes a housing thatas a diameter or width that is larger than the length of the gas generator and with a curvilinear solid propellant grain mounted therein to provide a long burning time propellant with a short length housing.
摘要翻译：曲线式固体推进剂气体发生器，其包括壳体，该壳体的直径或宽度大于气体发生器的长度，并且具有安装在其中的曲线固体推进剂颗粒，以提供具有短长度壳体的长燃烧时间推进剂。

2. 依法登记的发明

USH553H Pressurized piston expulsion system 失效
标题翻译：加压活塞排出系统
公开(公告)号：USH553H
公开(公告)日：1988-12-06
申请号：US138903
申请日：1987-12-28
申请人： Ben F. Wilson
发明人： Ben F. Wilson
IPC分类号： F02K9/50 , F02K9/60
CPC分类号： F02K9/605 , F02K9/50
摘要： A pressurized piston expulsion system in which an inner and smaller tank isn the form of a piston and mounted inside a larger tank by being sealably and slidably mounted therein to define two chambers in the larger tank and the smaller tank including high pressure stored gas therein with valving means for controlling flow of the gas to one side of the smaller tank and piston to cause fuel on an opposite side of the smaller tank and piston to be dispensed to a point of use.

3. 发明授权

US5622046A Multiple impinging stream vortex injector 失效
标题翻译：多冲击流涡流喷射器
公开(公告)号：US5622046A
公开(公告)日：1997-04-22
申请号：US521381
申请日：1995-08-28
申请人： Robert S. Michaels , Ben F. Wilson
发明人： Robert S. Michaels , Ben F. Wilson
IPC分类号： F02K9/52 , F02K9/00
CPC分类号： F02K9/52
摘要： Current state-of-the art injection methodologies for bipropellant engines ly on either impingement or turbulence to mix the fuel and oxidizer streams. The multiple impinging stream vortex injector combines both mixing schemes into a single injector. Both first stage mixing at point of impingement and second stage mixing or turbulent vortex mixing is accomplished by impinging momentum balanced, tangentially injected propellant streams onto one another. The impingement angles are calculated to yield a resultant stream vector that consists of only a tangential velocity component. The two stages of mixing results in increased engine performance and combustion efficiency.
摘要翻译：双组元推动剂发动机的现有技术注入方法依靠冲击或湍流来混合燃料和氧化剂流。多冲击流涡流喷射器将两种混合方案组合成单个喷射器。在撞击点和第二阶段混合或湍流涡流混合时的第一阶段混合都是通过将动量平衡的切向注入的推进剂流彼此冲击来实现的。计算冲击角以产生仅由切向速度分量组成的合成流向量。混合的两个阶段导致发动机性能和燃烧效率的提高。

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