公开(公告)号：US20050174760A1

公开(公告)日：2005-08-11

申请号：US10470306

申请日：2003-01-17

申请人： Piero Perlo ,  Rosella Monferino ,  Anatolii Zezdine ,  Piermario Repetto ,  Nello Li Pira ,  Mazria Paderl ,  Vito Lambertini ,  Davide Capello ,  Cosimo Carvignese ,  Giovanni Brusco ,  Bartolo Pairetti

发明人： Piero Perlo ,  Rosella Monferino ,  Anatolii Zezdine ,  Piermario Repetto ,  Nello Li Pira ,  Mazria Paderl ,  Vito Lambertini ,  Davide Capello ,  Cosimo Carvignese ,  Giovanni Brusco ,  Bartolo Pairetti

IPC分类号： F21L19/00 ,  F21V9/04 ,  F23D11/32 ,  F23D14/18 ,  F23D14/28 ,  F23D99/00 ,  F23Q3/00

CPC分类号： F23D99/00 ,  F23D11/32 ,  F23D14/18 ,  F23D14/28

摘要： A lighting device has a light source, comprising a volume (11) inside which combustion of a fuel-comburent mixture is confined. A photonic crystal structure (16) is positioned inside the volume (11). The photonic crystal structure (16) operates to inhibit or limit emission from said passage of at least a part of infrared radiation and simultaneously allow emission of visible light radiation. (FIG. 1)

摘要翻译： 照明装置具有光源，其包括容积（11），燃料混合物的燃烧被限制在其内。 光子晶体结构（16）位于体积（11）内。 光子晶体结构（16）用于抑制或限制来自所述红外线辐射的至少一部分的通过的发射，同时允许发射可见光辐射。 （图。1 ）

公开(公告)号：US20050160737A1

公开(公告)日：2005-07-28

申请号：US11019317

申请日：2004-12-23

申请人： Pietro Perlo ,  Gianfranco Innocenti ,  Piermario Repetto ,  Mauro Sgroi ,  Gianluca Bollito ,  Bartolo Pairetti ,  Rossella Monferino ,  Roberto Finizio ,  Cosimo Carvignese

发明人： Pietro Perlo ,  Gianfranco Innocenti ,  Piermario Repetto ,  Mauro Sgroi ,  Gianluca Bollito ,  Bartolo Pairetti ,  Rossella Monferino ,  Roberto Finizio ,  Cosimo Carvignese

IPC分类号： B81B7/00 ,  F01D1/32 ,  F01D25/16 ,  F02C3/14 ,  F02C3/16 ,  F02K7/00 ,  F16C39/06 ,  F23C15/00 ,  F23R3/52 ,  F23R3/56 ,  H02K7/18

CPC分类号： H02K7/1823 ,  F01D1/32 ,  F02C3/16 ,  F02C3/165 ,  F02K7/005 ,  F16C32/0427 ,  F16C32/0429 ,  F16C39/063 ,  F23C15/00 ,  F23R3/52 ,  F23R3/56

摘要： The combustor comprises a stationary structure and at least one tubular rotor supported rotatably about an axis by the structure by means of contactless suspension devices there being formed within this rotor at least one combustion chamber having at least one orientated lateral outflow aperture for the ejection of the combustion gases. The rotor has a narrow circumferential slot through which there extend at least one controlled stationary injector of fuel and combustion agent and an associated igniter which is also stationary. A control unit operates the injector and the igniter according to predetermined procedures, in such a way as to generate a detonation wave which is propagated in the chamber, and to cause the rotor to rotate as a result of the thrust due to the combustion gases emitted through the lateral outflow aperture.

摘要翻译： 燃烧器包括固定结构和至少一个管状转子，其通过非接触式悬挂装置通过结构围绕轴线可旋转地支撑，在该转子内形成有至少一个燃烧室，该燃烧室具有至少一个定向的横向流出孔，用于喷射 燃烧气体。 转子具有窄的圆周槽，通过该狭槽周围狭槽延伸至少一个控制的燃料和燃烧剂的固定喷射器以及也是静止的相关联的点火器。 控制单元根据预定的过程操作喷射器和点火器，以便产生在室中传播的爆震波，并且由于由于排放的燃烧气体而引起的推力，导致转子旋转 通过侧向流出孔。

公开(公告)号：US20050082421A1

公开(公告)日：2005-04-21

申请号：US10901132

申请日：2004-07-29

申请人： Pietro Perlo ,  Denis Bollea ,  Bartolo Pairetti ,  Stefano Alacqua ,  Roberto Finizio ,  Cosimo Carvignese ,  Piermario Repetto ,  Gianfranco Innocenti

发明人： Pietro Perlo ,  Denis Bollea ,  Bartolo Pairetti ,  Stefano Alacqua ,  Roberto Finizio ,  Cosimo Carvignese ,  Piermario Repetto ,  Gianfranco Innocenti

IPC分类号： B64C29/00 ,  A63H27/127 ,  A63H29/22 ,  B64C27/20 ,  B64C39/02 ,  B64C15/00

CPC分类号： B64C39/024 ,  A63H27/12 ,  A63H29/22 ,  B64C27/20 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146

摘要： The flying machine includes a supporting structure including a central rotational support having a vertical axis connected to an essentially horizontal, preferably annular, peripheral support part, coaxial with the central support, at least one upper rotor including a central hub rotatable about the axis of the central support of the supporting structure, an outer channel-section ring supported by the peripheral part of the supporting structure by contactless suspension means, preferably magnetic suspension means, and a plurality of blades which extend from the hub to the channel-section ring and which are inclined with respect to the horizontal plane; and motor devices carried at least partially by the peripheral part of the supporting structure and operable to cause rotation of the rotor with respect to this structure in a predetermined direction.

摘要翻译： 飞行器包括支撑结构，其包括中心旋转支撑件，该中心旋转支撑件具有连接到基本上水平的，优选环形的外围支撑部分的垂直轴线，该中心旋转支撑件与中心支撑件同轴，至少一个上转子包括可围绕 支撑结构的中心支撑，通过非接触式悬挂装置，优选磁悬浮装置由支撑结构的周边部分支撑的外部通道截面环，以及从轮毂延伸到通道截面环的多个叶片， 相对于水平面倾斜; 以及至少部分地由支撑结构的周边部分承载的马达装置，并且可操作以使转子相对于该结构在预定方向上旋转。