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1. 发明授权

US5222359A Nozzle system and method for supersonic jet engine 失效
标题翻译：用于超音速喷气发动机的喷嘴系统和方法
公开(公告)号：US5222359A
公开(公告)日：1993-06-29
申请号：US722944
申请日：1991-06-28
申请人： Garry W. Klees , Gary L. Lidstone , Mark L. Sloan
发明人： Garry W. Klees , Gary L. Lidstone , Mark L. Sloan
IPC分类号： F02C7/04 , F02K1/38 , F02K3/075
CPC分类号： F02C7/04 , F02K1/386 , F02K3/075 , B64D2033/026 , F05D2220/80
摘要： A supersonic jet engine for improved noise abatement and thrust augmentation. There is an intake section, an engine, a mixing section, an exhaust section, and a secondary air passageway. Ambient air is directed into the engine and into the secondary air passageway. Exhaust from the engine and the secondary air are directed into primary and secondary segments to mix in a stream direction as supersonic flow. Selectively controllable primary bypass passageways are provided at the primary passageway segments and are operated to bypass the primary flow through the primary segments at times when greater primary flow area is required.
摘要翻译：一种超音速喷气发动机，用于改善噪声消除和推力增大。有进气段，发动机，混合段，排气段和二次空气通道。环境空气被引导到发动机中并进入二次空气通道。来自发动机和二次空气的排气被引导到一级和二级段，以在流动方向上作为超音速流动混合。在主通道段处设置选择性可控的主旁通通路，并且在需要更大的主流动区域的时候，操作以旁通通过主段的主流。

2. 发明授权

US5129227A Low speed engine for supersonic and hypersonic vehicles 失效
标题翻译：用于超级和超级车辆的低速发动机
公开(公告)号：US5129227A
公开(公告)日：1992-07-14
申请号：US683350
申请日：1991-04-10
申请人： Garry W. Klees , Mark L. Sloan , Russel L. Thornock
发明人： Garry W. Klees , Mark L. Sloan , Russel L. Thornock
IPC分类号： F02K7/12
CPC分类号： F02K7/12 , Y02T50/671
摘要： A jet engine for use in a hypersonic aircraft. A fuel rich injectant is injected into the mixing zone of a duct at a substantial downstream angle to form an ejector. The temperature of the injectant is sufficiently low that spontaneous combustion of the injectant is delayed until the injectant reaches the combustion zone of the duct. In order to prevent combustion from propagating upstream from the combustion zone, the equivalence ratio of the mixture of injectant and ambient air flowing along the wall of the duct is maintained at a relatively high value, and the velocity profile of the flow along the wall of the duct is maintained at a relatively high value.

3. 发明授权

US4802629A Plug-type exhaust nozzle having a variable centerbody and translating shroud 失效
标题翻译：插头式排气喷嘴具有可变的中心体和平移护罩
公开(公告)号：US4802629A
公开(公告)日：1989-02-07
申请号：US436006
申请日：1982-10-22
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F02K1/08 , F02K1/09 , F02K1/62
CPC分类号： F02K1/625 , F02K1/085 , F02K1/09 , F05D2250/34 , Y02T50/671
摘要： A variable geometry gas turbine engine exhaust nozzle includes a variable circumference centerbody and a translating, annular shroud that cooperate to vary the throat area of the exhaust nozzle and the final area of the exhaust gas exiting the nozzle. The shroud includes a substantially constant inside diameter forward portion and a rear portion that has a continuously increasing inside diameter in the rearward direction. The centerbody is coaxially positioned within a circular cross section flow passage formed by the shroud and is configured with an upper and a lower shell that pivot between a retracted and an extended position. In the retracted position, the centerbody presents a circular profile to exhaust gases flowing through the exhaust nozzle. In the extended position, the centerbody presents an oval profile. By coordinating the centerbody shell position with the axial position of the shroud, the throat passage of the exhaust nozzle can be varied between an annular and a nonannular cross section. Additionally, since the shroud can be moved translationally independently of the configuration of the centerbody, the throat area of the exhaust nozzle and the final area of the exhaust gas can be varied independently of one another.
摘要翻译：可变几何形状燃气涡轮发动机排气喷嘴包括可变圆周中心体和平移的环形护罩，其协调以改变排气喷嘴的喉部区域和离开喷嘴的排气的最终区域。护罩包括基本上恒定的内径前部和在向后方向上具有连续增加的内径的后部。中心体同轴地定位在由护罩形成的圆形截面流动通道内，并且构造成具有在缩回位置和伸出位置之间枢转的上壳体和下壳体。在缩回位置，中心体具有圆形轮廓以排出流过排气喷嘴的废气。在延伸位置，中心体呈椭圆形。通过将中心体壳体位置与护罩的轴向位置协调，排气喷嘴的喉部通道可以在环形和非横截面之间变化。此外，由于护罩可以独立于中心体的构造而平移地移动，所以排气喷嘴的喉部区域和废气的最终区域可以彼此独立地变化。

4. 发明授权

US06685337B2 Combination flashlight and candle lantern 失效
标题翻译：组合手电筒和蜡烛灯
公开(公告)号：US06685337B2
公开(公告)日：2004-02-03
申请号：US10176630
申请日：2002-06-21
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F21S1900
CPC分类号： F21V35/00 , F21L4/005 , F21L19/00 , F21V23/0414 , F21Y2115/10
摘要： A combination flashlight/candle lantern with a modified lower base designed to be used with the standard, metallic cover on a candle lantern. The modified lower base has an upper neck designed to selectively attach to the metallic cover. The modified lower base also includes an upward extending cavity and a transversely aligned candle platform designed to receive a tube candle. Formed on the opposite side of the candle platform is a downward extending lower cavity designed to receive a low profile flashlight assembly. The flashlight assembly includes a cylindrical-shaped housing designed to partially extend into the lower base. Located centrally on the housing is a longitudinally extending LED electrically connected to two side-by-side watch batteries. Attached over the lower opening on the housing is a combination lens/switch which, when rotated, controls operation of the LED. The flashlight assembly may also include a bail located on the base member opposite the combination lens/switch. The bail may be disposed in a concealed manner when the flashlight assembly is attached to the lower base, or may allow the separated flashlight assembly to be independently supported from a hook or aimed on a flat surface.
摘要翻译：一个组合手电筒/蜡烛灯，具有改装的底座，设计用于标准的蜡烛灯笼上的金属盖。修改的下底座具有设计成选择性地附接到金属盖的上颈部。修改的下底座还包括向上延伸的腔和横向对准的烛台，设计成接收管蜡烛。形成在蜡烛台的相反一侧的是向下延伸的下腔，被设计成接收低轮廓的手电筒组件。手电筒组件包括设计成部分延伸到下底座的圆柱形壳体。位于壳体中央的是纵向延伸的LED，电连接到两个并排手表电池。连接在外壳上的下开口是组合透镜/开关，当旋转时控制LED的操作。手电筒组件还可以包括位于与组合透镜/开关相对的基部构件上的吊环。当手电筒组件附接到下基座时，吊环可以以隐蔽的方式设置，或者可以允许分离的手电筒组件从挂钩或针对平坦表面独立地支撑。

5. 外观设计

USD295401S Electronic circuit board housing 失效
公开(公告)号：USD295401S
公开(公告)日：1988-04-26
申请号：US710099
申请日：1985-03-11
申请人： Garry W. Klees
设计人： Garry W. Klees

6. 发明授权

US4448019A Turbine bypass turbojet with mid-turbine reingestion and method of operating the same 失效
标题翻译：涡轮旁路涡轮喷气发动机具有中等涡轮机再燃料及其运行方法
公开(公告)号：US4448019A
公开(公告)日：1984-05-15
申请号：US306652
申请日：1981-09-29
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F02C9/18 , F02K3/02 , F02F3/02
CPC分类号： F02C9/18 , F02K3/02 , F05D2220/80
摘要： A supersonic two spool turbojet engine capable not only of developing sufficient power to accelerate up to supersonic cruise and maintain efficient operation at supersonic cruise, but also arranged to cruise at subsonic velocities with a relatively low specific fuel consumption. The engine is provided with a variable bypass passageway downstream of the compressor. Flow into the bypass passageway is controlled so that during low power setting the bypass passageway is closed so that all the gaseous flow is directed through the turbine. During higher power settings, the bypass passageway is opened to the extent that a selected portion of the gaseous flow is directed through the bypass passageway to bypass the first stage of the turbine section so that the corrected flow to the first turbine stage remains substantially constant for high and low power setting of the engine. The bypass flow is then directed into the area between the first and second turbine to combine with the gaseous flow passing through the first turbine and pass through the second turbine.
摘要翻译：一种超音速双卷轴涡轮喷气发动机，不仅能够发展足够的功率加速到超音速巡航，并且在超音速巡航中保持有效的运行，而且还可以以相对较低的比燃料消耗在亚音速下巡航。发动机在压缩机的下游设有可变旁路通道。控制流入旁路通道的流动，使得在低功率设定期间，旁路通道关闭，使得所有的气流被引导通过涡轮机。在较高功率设置期间，旁路通道被打开至一定程度，气流的选定部分被引导通过旁通通道以绕过涡轮部分的第一级，使得到第一涡轮级的校正流保持基本恒定发动机的高低功率设定。然后将旁路流引导到第一和第二涡轮机之间的区域中，以与通过第一涡轮并通过第二涡轮机的气流相结合。

7. 发明授权

US4291782A Simplified method and apparatus for hot-shield jet noise suppression 失效
标题翻译：用于热屏蔽喷射噪声抑制的简化方法和装置
公开(公告)号：US4291782A
公开(公告)日：1981-09-29
申请号：US89693
申请日：1979-10-30
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F02K1/34 , F02K1/44 , F02K1/00
CPC分类号： F02K1/44 , F02K1/34 , B64D2033/024 , Y02T50/671
摘要： A method and apparatus for selectively generating a noise suppressing hot gas shield are described. A portion of the jet engine exhaust flow is selectively directed to a nozzle which at least partially surrounds the circumference of the jet engine exhaust. Prior to exiting the nozzle the flow is passed through a pressure, and therefore density, loss producing device to provide a shield flow of optimum noise suppression properties.
摘要翻译：描述用于选择性地产生噪声抑制热气体屏蔽的方法和装置。喷气发动机排气流的一部分被选择性地导向至少部分地围绕喷气发动机排气的圆周的喷嘴。在离开喷嘴之前，流动通过压力，因此通过密度损失产生装置，以提供最佳噪声抑制特性的屏蔽流。

8. 发明授权

US3938328A Multicycle engine 失效
标题翻译：多缸发动机
公开(公告)号：US3938328A
公开(公告)日：1976-02-17
申请号：US425586
申请日：1973-12-17
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F02K3/04 , F02K3/075 , F02K3/077 , F02K3/105 , F02K7/16 , F02K3/06
CPC分类号： F02K3/105 , F02K3/04 , F02K3/075 , F02K3/077 , F02K7/16 , F05D2220/80
摘要： Air breathing gas turbine engine design concepts, and methods and apparatus for providing variable engine cycles are disclosed. The preferred engine embodiments involve two flow control valve systems for internal management of air, each of which have the capacity to cross-over or invert adjacent annular flow patterns, and at least one of which is capable of switching from inverted to straight through flow.
摘要翻译：公开了空气呼吸燃气涡轮发动机设计概念以及用于提供可变发动机循环的方法和装置。优选的发动机实施例涉及用于内部管理空气的两个流量控制阀系统，每个流量控制阀具有交叉或反转相邻环形流动模式的能力，并且其中的至少一个能够通过流从倒流切换到直流。

9. 发明授权

US5688040A Portable, tub candle lantern 失效
标题翻译：便携式，浴缸蜡烛灯笼
公开(公告)号：US5688040A
公开(公告)日：1997-11-18
申请号：US587922
申请日：1996-01-17
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F21L19/00 , F21V35/00
CPC分类号： F21V35/00 , F21L19/00
摘要： A portable candle lantern with safety features designed to be used with a tub candle. The candle lantern includes an upper cover that selectively attaches to a lower base. The lower base has a plurality of feet with enable it to be supported in an elevated position on a support surface. Located inside the lower base is a candle holding assembly which removably holds a tub candle in an elevated, longitudinally aligned position therein. Formed inside the lower base is a centrally located, longitudinally aligned, upward extending, air delivery tube which delivers cool air directly against the sides of the tub candle and the candle holding assembly. By delivering cool air in this manner, the temperature inside the candle lantern is reduced thereby preventing a "flash" condition from occurring. Also, a collection cavity is formed between the air delivery tube and the sides of the lower base in which spilled wax from the tub candle is collected.
摘要翻译：一个便携式蜡烛灯，安全功能设计用于浴缸蜡烛。蜡烛灯包括选择性地附接到下底座的上盖。下底座具有多个脚，使其能够支撑在支撑表面上的升高位置。位于下基座内的是烛座保持组件，其可拆卸地将浴缸蜡烛保持在升高的纵向对准位置。形成在下底座内的是位于中心的纵向排列的向上延伸的空气输送管，其将冷空气直接传递到浴缸蜡烛和蜡烛保持组件的侧面。通过以这种方式输出冷空气，烛灯内部的温度降低，从而防止发生“闪光”状况。此外，在空气输送管和下底座的侧面之间形成收集腔，其中收集来自浴缸蜡烛的溢出的蜡。

10. 发明授权

US5463866A Supersonic jet engine installation and method with sound suppressing nozzle 失效
标题翻译：超音速喷气发动机安装方法与声音抑制喷嘴
公开(公告)号：US5463866A
公开(公告)日：1995-11-07
申请号：US175965
申请日：1993-12-30
申请人： Garry W. Klees
发明人： Garry W. Klees
IPC分类号： F02K1/38 , F02K1/46 , F02K3/02
CPC分类号： F02K1/46 , F02K1/383 , F05D2220/80
摘要： A supersonic jet engine having a nozzle section into which ambient air can be selectively introduced for a noise suppressing mode of operation, with this ambient air being intermixed with engine exhaust flow, through passageway segments. Flow modulating plugs or vanes are positioned at the exhaust end of engine exhaust outlet segments in a mixing section, and these are operated during noise suppression mode to match engine requirements. There is a final nozzle section which during the noise suppressing mode is opened to present a relatively large cross sectional flow area to accommodate the mixed flow.During the non-noise suppressing mode, the final nozzle has a convergent/divergent configuration to control flow, and the plug or vane flow modulating means are positioned to permit unrestricted flow from the engine exhaust outlet segments.
摘要翻译：一种具有喷嘴部分的超音速喷气发动机，其中可以选择性地引入环境空气用于噪声抑制操作模式，这种环境空气通过通道段与发动机排气流混合。流量调节塞子或叶片位于混合部分的发动机排气出口段的排气端，这些在噪声抑制模式下运行以匹配发动机的要求。存在最终喷嘴部分，其在噪声抑制模式被打开以呈现相对大的横截面流动面积以适应混合流动。在非噪声抑制模式期间，最终喷嘴具有收敛/发散配置以控制流量，并且插头或叶片流量调节装置被定位成允许来自发动机排气出口段的不受限制的流动。

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