公开(公告)号：US06467724B2

公开(公告)日：2002-10-22

申请号：US09903782

申请日：2001-07-11

Applicant: Hermann Kuenkler

Inventor： Hermann Kuenkler

IPC: B64C2752

CPC classification number: B64C29/0033 ,  B63H5/125 ,  B64B1/32 ,  B64B2201/00 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64D35/00

Abstract: An aircraft has a fuselage designed essentially as an aerostatic lift body and combined lift and propulsion devices which are articulated on the fuselage, are provided with propellers and form propulsion units and which in each case are tiltable between a lift position, in which the respective propeller rotation plane is essentially horizontal and the output shaft of the associated drive, said output shaft acting on the respective propeller shaft, is essentially vertical, and a propulsion position, in which the respective propeller rotation plane is essentially vertical and the output shaft of the associated drive, said output shaft acting on the respective propeller shaft, is essentially horizontal. The propeller rotation plane has all-round inclinability relative to the output shaft of the associated drive, said output shaft acting on the propeller shaft.

Abstract translation: 飞机具有基本上被设计为空气静力升降机体的机身，并且在机身上铰接的组合的升降机和推进装置设置有螺旋桨和形式推进单元，并且在每种情况下都能够在提升位置之间倾斜， 旋转平面基本上是水平的，并且相关联的驱动器的输出轴（所述输出轴作用在相应的传动轴上）基本上是垂直的，以及推进位置，其中相应的螺旋桨旋转平面基本上垂直并且相关联的输出轴 驱动，所述输出轴作用在相应的传动轴上，基本上是水平的。 螺旋桨旋转平面相对于相关驱动器的输出轴具有全方位的倾斜性，所述输出轴作用在传动轴上。

公开(公告)号：US06286783B1

公开(公告)日：2001-09-11

申请号：US09341162

申请日：1999-11-01

Applicant: Hermann Kuenkler

Inventor： Hermann Kuenkler

IPC: B64B102

CPC classification number: B64C29/0033 ,  B63H5/125 ,  B64B1/32 ,  B64B2201/00 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64D35/00

Abstract: An aircraft has a fuselage designed essentially as an aerostatic lift body. Combined lift and propulsion devices are articulated on the fuselage, are provided with propellers and form propulsion units and which in each case can tilt between a lift position, in which the respective propeller rotation plane is essentially horizontal and a propulsion position, in which the respective propeller rotation plane is essentially vertical. Additionally the propeller rotation plane has all-round inclination relative to the output shaft of the associated drive device.

Abstract translation: 飞机有一个基本上设计为空气静力升降机身的机身。 组合的升降机和推进装置在机身上铰接，具有螺旋桨和形式推进单元，并且在每种情况下都可以在各自的螺旋桨旋转平面基本上水平的提升位置与推进位置之间倾斜， 螺旋桨旋转平面基本上是垂直的。 此外，螺旋桨旋转平面相对于相关联的驱动装置的输出轴具有全方位的倾斜。

公开(公告)号：IL146915A

公开(公告)日：2004-06-01

申请号：IL14691598

申请日：1998-01-02

Applicant: HERMANN KUENKLER

IPC: B64B20060101 ,  B64C27/52

公开(公告)号：BR9806838A

公开(公告)日：2000-03-14

申请号：BR9806838

申请日：1998-01-02

Applicant: HERMANN KUENKLER

Inventor： KUENKLER HERMANN

IPC: B64B1/06 ,  B63H5/125 ,  B64B1/30 ,  B64B1/32 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64C29/00 ,  B64D35/00

Abstract: The airship has a fuselage (1) built as an aerostatic buoyant body, having propellers (11,12,13,14) with respective shafts (121) and drive units (7,8,9,10). The respective propeller shaft (121) rotation plane (113) can be tilted all round relative to a drive shaft (104) of the allocated propeller drive, and the hull also does duty as aerodynamic float in a ship devoid of activatable aerodynamic steering system. The hull can be circular or elliptical to give an elliptical section whose upper shell is more steeply curved than the flatter bottom shell. The hull is fitted with a stiffener ring in its equatorial belt with the ring also of elliptical section in its exterior.