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21. 发明申请

WO2012135638A1 FLUID TURBINE WITH VARIABLE PITCH SHROUD SEGMENTS 审中-公开
标题翻译：流体涡轮机与可变阀座SHROUD部分
公开(公告)号：WO2012135638A1
公开(公告)日：2012-10-04
申请号：PCT/US2012/031490
申请日：2012-03-30
申请人： FLODESIGN WIND TURBINE CORP. , PRESZ, Walter, M., Jr. , WERLE, Michael, J. , HJORT, Soren , RUBAK, Rune , LOVMAND, Bo , DALSGAARD, Soren
发明人： PRESZ, Walter, M., Jr. , WERLE, Michael, J. , HJORT, Soren , RUBAK, Rune , LOVMAND, Bo , DALSGAARD, Soren
IPC分类号： F03D1/04 , F03D7/02
CPC分类号： F01D11/22 , F03D1/04 , F03D7/02 , F03D7/028 , F03D9/25 , F05B2240/12 , F05B2240/122 , F05B2240/124 , F05B2250/41 , Y02E10/723
摘要： One or more variable pitch airfoils in fluid communication with a rotor of a fluid turbine can control the amount of energy directed to the rotor, and further control the amount of energy generated by the turbine. Varying the pitch of the airfoils may provide a means of controlling the power output of a fluid turbine without the need to control the pitch of the rotor blades, and may further provide a means of mitigating the effects of wind shear on the rotor. Variable pitch airfoils may also include a means of controlling the active power, reactive power and SCADA, of a group of fluid turbines.
摘要翻译：与流体涡轮机的转子流体连通的一个或多个可变桨距翼型件可以控制指向转子的能量的量，并进一步控制涡轮机产生的能量的量。改变翼型件的间距可以提供控制流体涡轮机的功率输出的手段，而不需要控制转子叶片的桨距，并且还可以提供减轻风切变对转子的影响的手段。可变桨距翼型件还可以包括控制一组流体涡轮机的有功功率，无功功率和SCADA的装置。

22. 发明申请

WO2011084118A1 CONTROLLED-UNAIDED SURGE AND PURGE SUPPRESSORS FOR FIREARM MUZZLES 审中-公开
标题翻译：用于灭火器的控制消除冲击和冲击抑制器
公开(公告)号：WO2011084118A1
公开(公告)日：2011-07-14
申请号：PCT/US2010/000036
申请日：2010-01-06
申请人： FLODESIGN, INC. , PRESZ, Walter, M. JR. , WERLE, Michael, J. , LIPKENS, Bart , GAWENCKI, Jason
发明人： PRESZ, Walter, M. JR. , WERLE, Michael, J. , LIPKENS, Bart , GAWENCKI, Jason
IPC分类号： F41A21/30 , F41A21/34
CPC分类号： F41A21/30 , F41A21/34
摘要： A Controlled Unaided Surge and Purge Suppressor (1000) 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, the blast surge is mitigated via a slotted mixer nozzle (1002); a first expansion chamber (1004); a generally "wagon-wheel" shaped blast baffle (1006) with a vent hole; a series of alternating baffles (1012A-F), with vent holes, strategically located along the suppressor's inner wall surface; a second expansion chamber (1014); and an exit opening (1016). This preferred embodiment contains no "outside" vent holes (i.e. throughbores) which extend through the suppressor's outer or longitudinal wall (1001). Instead of ingesting ambient air through such throughbores and mixing the air with the muzzle gases, the preferred embodiment ingests and mixes chamber gases and contaminants with the muzzle gases while allowing fluid flow through and out the suppressor (1000). It too though can control or eliminate the Mach disk.
摘要翻译：用于火器的受控无人值守浪涌和清除抑制器（1000）使用弹道排放过程固有的爆破和羽流特性，开发以先进搅拌器 - 喷射器概念为中心的新的两步控制浪涌和净化系统。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，通过开槽混合器喷嘴（1002）减轻冲击浪涌; 第一膨胀室（1004）; 具有通气孔的通常为“车轮”形的鼓风挡板（1006）; 一系列交替挡板（1012A-F），具有通风孔，沿着抑制器的内壁表面策略地定位; 第二膨胀室（1014）; 和出口（1016）。该优选实施例不包含延伸穿过抑制器的外壁或纵壁（1001）的“外”通气孔（即通孔）。代替通过这种通孔吸入环境空气并将空气与枪口气体混合，优选实施例将腔室气体和污染物与枪口气体混合，同时允许流体流过和流出抑制器（1000）。它也可以控制或消除马赫盘。

23. 发明申请

WO2009151428A2 CONTROLLED-UNAIDED SURGE AND PURGE SUPPRESSORS FOR FIREARM MUZZLES 审中-公开
标题翻译：用于灭火器的控制消除冲击和冲击抑制器
公开(公告)号：WO2009151428A2
公开(公告)日：2009-12-17
申请号：PCT/US2008/010806
申请日：2008-09-17
申请人： FLODESIGN, INC. , PRESZ, Walter, M., JR , WERLE, Michael, J. , LIPKENS, Bart
发明人： PRESZ, Walter, M., JR , WERLE, Michael, J. , LIPKENS, Bart
IPC分类号： F41A21/30
CPC分类号： F41A21/30 , F41A21/34
摘要： 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.
摘要翻译：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。

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