公开(公告)号：WO1997016342A1

公开(公告)日：1997-05-09

申请号：PCT/RU1996000284

申请日：1996-10-07

Applicant: FILIMONOV, Alexandr Iosifovich

IPC: B64B01/12

CPC classification number: B64C29/00 ,  B60V3/08 ,  B64B1/00 ,  B64B1/005 ,  B64B1/12 ,  B64C15/14 ,  B64C29/0025

Abstract: The hybrid dirigible craft belongs to the category of flying vehicles which use an air cushion and take off and land at any type of airfield. The aim of the invention is to design an improved dirigible craft capable of taking off from and landing on water and low-load bearing surfaces. To that end the hybrid dirigible craft comprises the following elements: a discoid body (1) with a central passage (2) in which is mounted a flow-permitting body (5) with a rotor (6) on its upper part and secured to the walls by radial partitions (7) which have an aerodynamic profile; the pilot-passenger and cargo compartments (9 and 10 respectively); a propulsion unit with propellers (8), units for landing on an air cushion in the form of an inflatable toroidal bag (11) and wheel-skid supports (12, 13) mounted on the lower surfaces; rotating flaps (3) mounted at the inlet into the central passage (2); control and stabilising elements (4) mounted at the outlet of the central passage (2); outer wing units (14) and a tail assembly with stabiliser (19) and two or more fins (17) mounted on the rear part of the hull; airflow flaps (21) on the rear flaps of the outer wing elements and hull (22); and airflow control surfaces (20) on the stabiliser and outer wing elements. The dirigible craft also has elevons (22) on the stabiliser and a flexible guard element (23) mounted on and underneath the forward part of the toroidal bag (11). It also has gear for taking off from water in the form of gliding surfaces (28) underneath the compartment (9).

Abstract translation: 混合动力飞艇属于使用气垫起飞和着陆于任何类型机场的飞行器类别。 本发明的目的是设计一种能够在水和低负载表面上起降的改进的可拆卸工具。 为此，混合动力工具包括以下元件：具有中心通道（2）的圆盘体（1），其中在其上部安装有具有转子（6）的流动允许体（5）并固定到 具有空气动力学特征的径向隔板（7）的壁; 飞行员和货舱（分别为9和10）; 具有螺旋桨（8）的推进单元，用于以可充气环形袋（11）的形式在气垫上着陆的单元和安装在下表面上的轮滑支撑件（12,13）; 安装在入口处的中心通道（2）中的旋转翼片（3）; 控制和稳定元件（4），安装在中央通道（2）的出口处; 外翼单元（14）和具有稳定器（19）的尾部组件和安装在船体后部的两个或更多个翼片（17） 外翼元件的后翼板上的气流翼片（21）和船体（22）; 和稳定器和外翼元件上的气流控制表面（20）。 稳定器上还具有升降器（22），安装在环形袋（11）前部和下方的柔性保护元件（23）。 它还具有用于从隔室（9）下方的滑动表面（28）的形式从水中取出的装置。