公开(公告)号：US20090108126A1

公开(公告)日：2009-04-30

申请号：US11922506

申请日：2005-07-07

Applicant: Alfredo Capuani

Inventor： Alfredo Capuani

IPC: B64B1/02

CPC classification number: B64C31/032 ,  B64B1/02 ,  B64B2201/00

Abstract: The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tubular branches (12, 14) joined to form a V-shaped profile, with an aerodinamic-lift surface (22, 24) extending therebetween.

Abstract translation: 飞行器（10）包括设置有推进装置和方向控制平面的细长框架（26）。 该框架联接到适于填充轻于空气气体的气动室（16），并且包括两个连接以形成V形轮廓的管状分支（12,14），其具有气动提升表面（22， 24）。

公开(公告)号：US08113459B2

公开(公告)日：2012-02-14

申请号：US11922506

申请日：2005-07-07

Applicant: Alfredo Capuani

Inventor： Alfredo Capuani

IPC: B64C3/30

CPC classification number: B64C31/032 ,  B64B1/02 ,  B64B2201/00

Abstract: An aircraft comprising an elongated framework provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber suited to be filled with lighter-than-air gas and comprising two tubular branches joined to form a V-shaped profile, with an aerodinamic-lift surface extending therebetween.

Abstract translation: 一种飞机，其包括具有推进装置和方向控制平面的细长框架。 该框架联接到适于填充有轻于空气气体的气动室，并且包括连接以形成V形轮廓的两个管状分支，其间延伸有气动提升表面。