公开(公告)号：WO2014199351A1

公开(公告)日：2014-12-18

申请号：PCT/IB2014/062209

申请日：2014-06-13

Applicant: NIMBUS S.R.L.

Inventor： BELLEZZA QUATER, Paolo ,  CAPUANI, Alfredo

IPC: B64C29/00 ,  B64C21/04

CPC classification number: B64C21/04 ,  B64C29/0066 ,  B64C39/12 ,  Y02T50/166

Abstract: Described herein is an aircraft (1; 1', 100) including : - a fuselage (2; 2'; 102); - a pair of wings (3, 4; 103, 104); - a propulsion apparatus (13; 13'; 113) configured for generating a propulsive thrust by processing a flow of fluid, in particular, air, and configured for varying the direction of said propulsive thrust by the Coanda effect; and - an equipment for generating lift (6, 7; 106, 107; 113, 113') arranged at a nose section (5; 5'; 105) in a substantially end position on said fuselage (2; 2'; 102).

Abstract translation: 本文描述的是飞机（1; 1'，100），包括： - 机身（2; 2'; 102）; - 一对翼（3,4; 103,104）; - 推进装置（13; 13'; 113），其构造成通过处理流体流，特别是空气来产生推进推力，并且被构造成通过柯安达效应改变所述推进推力的方向; 以及 - 设置在所述机身（2; 2'; 102）上的基本上位置的鼻部（5; 5'; 105）上的用于产生升降机（6,7; 106,107; 113,113'）的设备， 。

公开(公告)号：WO2007007353A1

公开(公告)日：2007-01-18

申请号：PCT/IT2005/000387

申请日：2005-07-07

Applicant: NIMBUS S.R.L. ,  CAPUANI, Alfredo

Inventor： CAPUANI, Alfredo

IPC: B64B1/02 ,  B64C31/032

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：EP1899220A1

公开(公告)日：2008-03-19

申请号：EP05769453.1

申请日：2005-07-07

Applicant: Nimbus S.R.L.

Inventor： CAPUANI, Alfredo

IPC: B64B1/02 ,  B64C31/032

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.

公开(公告)号：EP3007974A1

公开(公告)日：2016-04-20

申请号：EP14744161.2

申请日：2014-06-13

Applicant: NIMBUS S.r.l.

Inventor： BELLEZZA QUATER, Paolo ,  CAPUANI, Alfredo

IPC: B64C29/00 ,  B64C21/04

CPC classification number: B64C21/04 ,  B64C29/0066 ,  B64C39/12 ,  Y02T50/166

Abstract: Described herein is an aircraft (1; 1', 100) including : - a fuselage (2; 2'; 102); - a pair of wings (3, 4; 103, 104); - a propulsion apparatus (13; 13'; 113) configured for generating a propulsive thrust by processing a flow of fluid, in particular, air, and configured for varying the direction of said propulsive thrust by the Coanda effect; and - an equipment for generating lift (6, 7; 106, 107; 113, 113') arranged at a nose section (5; 5'; 105) in a substantially end position on said fuselage (2; 2'; 102).

公开(公告)号：EP1899220B1

公开(公告)日：2011-04-13

申请号：EP05769453.1

申请日：2005-07-07

Applicant: Nimbus S.R.L.

Inventor： CAPUANI, Alfredo

IPC: B64B1/02 ,  B64C31/032

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.