公开(公告)号：US20040079301A1

公开(公告)日：2004-04-29

申请号：US10429716

申请日：2003-05-06

Applicant: C.R.F. SOCIETA CONSORTILE PER AZIONI

Inventor： Piero Perlo ,  Gianfranco Innocenti ,  Gianluca Bollito ,  Bartolomeo Pairetti ,  Alessandro Zanella ,  Cosimo Carvignese

IPC: F02B071/00

CPC classification number: H02K7/1884 ,  F02B1/12 ,  F02B63/04 ,  F02B63/041 ,  F02B71/04 ,  F02B75/34 ,  H02K35/02

Abstract: Described herein is a microgenerator of electrical energy with a high power density, which uses an internal-combustion micromotor with two combustion chambers set opposite to one another, within which a piston is displaced with reciprocating motion. The piston is at least in part made of magnetic material and is wound with a coil, within which is generated an electric current by induction. The fuel, the oxidant, and preferably a catalyst, are injected into each of the two combustion chambers by means of injectors that are substantially of the same type as those used in ink-jet printer heads. The dimensions of the device are comparable to those of a 1.5-V NiCd battery of a traditional standard type.

Abstract translation: 这里描述的是具有高功率密度的电能的微发电机，其使用具有彼此相对设置的两个燃烧室的内燃微型马达，其中活塞以往复运动位移。 活塞至少部分由磁性材料制成，并用线圈缠绕，其中通过感应产生电流。 燃料，氧化剂，优选催化剂，通过喷射器注入到两个燃烧室的每一个中，所述喷射器基本上与喷墨打印头中使用的类型相同。 该装置的尺寸与传统标准类型的1.5V镍氢电池的尺寸相当。

公开(公告)号：US20040129833A1

公开(公告)日：2004-07-08

申请号：US10626697

申请日：2003-07-25

Applicant: C.R.F. SOCIETA CONSORTILE PER AZIONI

Inventor： Piero Perlo ,  Denis Bollea ,  Roberto Finizio ,  Cosimo Carvignese ,  Elena Balocco

IPC: B64C039/00

CPC classification number: B64C29/02 ,  B64C27/20 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165

Abstract: VTOL micro-aircraft comprising a first and a second ducted rotor mutually aligned and distanced according to a common axis and whose propellers are driven in rotation in mutually opposite directions. Between the two ducted rotors are positioned a fuselage and a wing system formed by wing profiles forming an X or an H configuration and provided with control flaps.

Abstract translation: VTOL微型飞机包括第一和第二导管转子，该第一和第二导管转子根据公共轴相互对准和间隔，并且其螺旋桨沿彼此相反的方向旋转驱动。 在两个管状转子之间设置有由机翼轮廓形成的机身和机翼系统，所述机翼轮廓形成X或H构造并设置有控制翼片。

公开(公告)号：US20040129827A1

公开(公告)日：2004-07-08

申请号：US10626704

申请日：2003-07-25

Applicant: C.R.F. SOCIETA CONSORTILE PER AZIONI

Inventor： Piero Perlo ,  Denis Bollea ,  Stefano Alacqua ,  Roberto Finizio ,  Cosimo Carvignese ,  Elena Balocco

IPC: B64C027/22

CPC classification number: B64C39/026 ,  B64C29/02

Abstract: VTOL aircraft comprising a first and a second ducted rotor positioned at the ends of a vertical fuselage and whose propellers are driven to rotate in mutually opposite directions. Control flaps for orientation and transverse flight are operatively associated at least to the lower ducted rotor.

Abstract translation: VTOL飞机包括位于垂直机身的端部的第一和第二导管转子，并且其螺旋桨被驱动以沿彼此相反的方向旋转。 用于定向和横向飞行的控制翼片至少可操作地连接到下部管道转子。