FIELD: air transport not requiring runways. SUBSTANCE: flying vehicle has case 1 and engine 2 brought in communication with spherical rotors 3 and 4 by means of shaft 5 secured in center of intake 6 with rotor 3 and satellite gears 7 on axle 8 secured on case 1. Surface 9 of rotor 3 is located above outer surface 10 of rotor 4; it includes blades 13 adjoining surface 14 of shield 15 connected with case 1 and control lever 16. Payload is secured on suspension 18 mounted in hinge 19 located on geometrical axis 20. Surface 21 of rotor 3 is provided with blades 22 adjoining surface 23 of fairing 24 on which stator blades 25 and lines 26 of parachute 27 are secured. EFFECT: extended field of application of flying vehicle. 6 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRBORNE VEHICLE | 2013 |
|
RU2532443C2 |
KARPHIDOV ROTOR ENGINE | 2006 |
|
RU2333372C2 |
ROTARY ENGINE | 1998 |
|
RU2151312C1 |
ROTARY ENGINE | 2000 |
|
RU2189470C1 |
ROTARY ENGINE AND METHOD OF DELIVERING FUEL MIXTURES INTO ITS COMBUSTION CHAMBER | 1997 |
|
RU2133840C1 |
POSITIVE-DISPLACEMENT ROTOR MACHINE | 1994 |
|
RU2084640C1 |
POSITIVE-DISPLACEMENT ROTARY MACHINE | 1992 |
|
RU2041361C1 |
METHOD TO RECOVER HEAT IN ROTARY ENGINE FOR EXECUTING ADDITIONAL WORK | 2004 |
|
RU2277174C1 |
VOLUMETRIC NUTATION MACHINE | 2007 |
|
RU2374457C2 |
WIND TURBINE PLANT | 2023 |
|
RU2805549C1 |
Authors
Dates
2000-05-10—Published
1999-02-03—Filed