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    • 3. 发明申请
    • WIND TURBINE WITH MIXERS AND EJECTORS
    • 具有搅拌机和喷射器的风力涡轮机
    • WO2009120176A8
    • 2010-03-04
    • PCT/US2008011015
    • 2008-09-23
    • FLODESIGN WIND TURBINE CORPPRESZ WALTER M JRWERLE MICHAEL J
    • PRESZ WALTER M JRWERLE MICHAEL J
    • F03D1/04
    • F03D1/04F05B2240/13F05B2240/133F05B2260/96Y02B10/30Y02E10/721
    • A method is disclosed for improving the operational effectiveness and efficiency of wind turbines. Applicants' preferred method comprises: generating a level of power over the Betz limit for an axial flow wind turbine, of the type having a turbine shroud with a flared inlet and an impeller downstream having a ring of impeller blades, by receiving and directing a primary air stream of ambient air into the flared inlet and through the turbine shroud; rotating the impeller inside the shroud by the primary air stream, whereby the primary air stream transfers energy to the impeller; entraining and mixing a secondary flow stream of ambient air exclusively with the primary air stream, which has passed through the impeller, via a mixer and an ejector sequentially downstream of the impeller. Unlike gas turbine mixers and ejectors which also mix with hot core exhaust gases, Applicants' preferred method entrains and mixes ambient air (i.e., wind) exclusively with lower energy air (i.e., partially spent air) which has passed through a turbine shroud and rotor. Applicant's method further comprises harnessing the power of the primary air stream to produce mechanical energy while exceeding the Betz limit for operational efficiency of the axial flow wind turbine over a non-anomalous period.
    • 公开了一种用于提高风力涡轮机的运行效率和效率的方法。 申请人的首选方法包括:为轴流式风力涡轮机产生超过Betz限制的功率级别,该轴流式风力涡轮机的类型具有涡轮机罩,其具有扩口入口和具有叶轮叶片环的叶轮,通过接收和引导初级 空气流进入扩口入口并通过涡轮罩; 通过一次空气流使护罩内的叶轮旋转,由此一次空气流将能量传递到叶轮; 通过混合器和依次在叶轮下游的喷射器将环境空气的二次流流与仅通过叶轮的一次空气流混合并混合。 不同于也与热芯废气混合的燃气轮机混合器和喷射器,申请人的首选方法仅将环境空气(即风)与通过涡轮机罩和转子的较低能量空气(即部分废气)混合 。 申请人的方法还包括利用一次空气流的功率产生机械能,同时超过在非异常时期的轴流式风力涡轮机的运行效率的Betz限制。
    • 6. 发明申请
    • CONTROLLED-UNAIDED SURGE AND PURGE SUPPRESSORS FOR FIREARM MUZZLES
    • 用于灭火器的控制消除冲击和冲击抑制器
    • WO2009151428A3
    • 2010-02-18
    • PCT/US2008010806
    • 2008-09-17
    • FLODESIGN INCPRESZ WALTER M JRWERLE MICHAEL JLIPKENS BART
    • PRESZ WALTER M JRWERLE MICHAEL JLIPKENS BART
    • F41A21/30F41A21/34
    • F41A21/30F41A21/34
    • A noise and flash suppressor for firearms uses the blast and plume characteristics inherent to the ballistic discharge process to develop a new two-step controlled surge and purge system centered around advanced mixer-ejector concepts. The blast surge noise is reduced by controlling the flow expansion, and the flash effects are reduced by controlling inflow and outflow gas purges. In the preferred embodiment, suppressor vent holes are convergently contoured to better reduce the blast surge. Preferably a two-stage supersonic mixer/ejector system, in combination with adjacent vent holes in the suppressor housing and a divergent entrance nozzle, is used to control or eliminate the external Mach disk, while rapidly mixing and diluting the propellant with purged gases. A diffuser downstream of the mixer/ejector system further increases ejector performance and pumping. The pumped gases are used to self-clean and cool the suppressor.
    • 用于火器的噪音和闪光抑制器使用弹道放电过程固有的爆炸和羽流特性,开发出以先进的混合器 - 喷射器概念为中心的新的两步控制的浪涌和净化系统。 通过控制流量膨胀来减少爆炸浪涌噪声,并通过控制流入和流出气体清除来减少闪光效应。 在优选实施例中,抑制器通气孔趋于一致的轮廓以更好地减少鼓风浪涌。 优选地,两级超音速混合器/喷射器系统与抑制器壳体中的相邻通气孔和扩散入口喷嘴组合用于控制或消除外部马赫盘,同时用吹扫气体快速混合和稀释推进剂。 混合器/喷射器系统下游的扩散器进一步增加喷射器性能和泵送。 泵送的气体用于自我清洁和冷却抑制器。
    • 7. 发明申请
    • CONTROLLED-UNAIDED SURGE AND PURGE SUPPRESSORS FOR FIREARM MUZZLES
    • 用于灭火器的控制消除冲击和冲击抑制器
    • WO2009151428A2
    • 2009-12-17
    • PCT/US2008/010806
    • 2008-09-17
    • FLODESIGN, INC.PRESZ, Walter, M., JRWERLE, Michael, J.LIPKENS, Bart
    • PRESZ, Walter, M., JRWERLE, Michael, J.LIPKENS, Bart
    • F41A21/30
    • F41A21/30F41A21/34
    • A Controlled Unaided Surge and Purge (CUSPS) suppressor for firearms uses the blast and plume characteristics inherent to the ballistic discharge process to develop a new two-step controlled surge and purge system centered around advanced mixer-ejector concepts. The blast surge noise is reduced by controlling the flow expansion, and the flash effects are reduced by controlling inflow and outflow gas purges. In the preferred embodiment, suppressor vent holes are convergently contoured to better reduce the blast surge. Preferably a two-stage supersonic mixer/ejector system, in combination with adjacent vent holes in the suppressor housing and a divergent entrance nozzle, is used to control or eliminate the external Mach disk, while rapidly mixing and diluting the propellant with purged gases. A diffuser downstream of the mixer/ejector system further increases ejector performance and pumping. The pumped gases are used to self-clean and cool the CUSPS suppressor.
    • 用于枪支的受控的无人值守浪涌和清除(CUSPS)抑制器使用弹道放电过程固有的爆炸和羽流特性,开发以先进的混合器 - 喷射器概念为中心的新的两步控制的浪涌和净化系统。 通过控制流量膨胀来减少爆炸浪涌噪声,并通过控制流入和流出气体清除来减少闪光效应。 在优选实施例中,抑制器通气孔趋于一致的轮廓以更好地减少鼓风浪涌。 优选地,两级超音速混合器/喷射器系统与抑制器壳体中的相邻通气孔和扩散入口喷嘴组合用于控制或消除外部马赫盘,同时用吹扫气体快速混合和稀释推进剂。 混合器/喷射器系统下游的扩散器进一步增加喷射器性能和泵送。 抽吸气体用于自我清洁和冷却CUSPS抑制剂。