RU2013115878A - METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER - Google Patents
METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER Download PDFInfo
- Publication number
- RU2013115878A RU2013115878A RU2013115878/11A RU2013115878A RU2013115878A RU 2013115878 A RU2013115878 A RU 2013115878A RU 2013115878/11 A RU2013115878/11 A RU 2013115878/11A RU 2013115878 A RU2013115878 A RU 2013115878A RU 2013115878 A RU2013115878 A RU 2013115878A
- Authority
- RU
- Russia
- Prior art keywords
- airship
- hull
- stabilizing
- autogyro
- traction
- Prior art date
Links
- 230000000087 stabilizing effect Effects 0.000 title claims 2
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
Способ управления, стабилизации и создания дополнительной подъемной силы дирижабля, имеющего корпус, хвостовое оперение, гондолу с полезным грузом, подвешенную к корпусу, отличающийся тем, что устойчивость и управляемость дирижабля для требуемых характеристик взлета, полета и посадки обеспечена путем использования на нем рационально скомпонованных и работающих в воздушном потоке одного, двух, трех, четырех и более автожирных винтов с управляемым вектором полной аэродинамической силы тяги, осуществляемым при помощи непосредственного наклона оси вращения каждого автожирного винта относительно продольного и поперечного направлений в присутствии отдельных маршевых силовых установок, выполняющих свои тяговые функции механически независимо от автожирных винтов.A method of controlling, stabilizing and creating additional lifting force of an airship having a hull, tail unit, a nacelle with a payload suspended from the hull, characterized in that the stability and controllability of the airship for the required take-off, flight and landing characteristics are ensured by using rationally arranged and working in the air stream of one, two, three, four or more gyroscrews with a controlled vector of full aerodynamic traction, carried out using direct Pull autogyro rotation axis of each screw relative to the longitudinal and transverse directions in the presence of a separate propulsion power units, perform their functions traction mechanically independently from autogyro screws.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013115878/11A RU2532448C1 (en) | 2013-04-10 | 2013-04-10 | Method of control, stabilisation and development of extra lift of airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013115878/11A RU2532448C1 (en) | 2013-04-10 | 2013-04-10 | Method of control, stabilisation and development of extra lift of airship |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2013115878A true RU2013115878A (en) | 2014-10-20 |
| RU2532448C1 RU2532448C1 (en) | 2014-11-10 |
Family
ID=53380046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2013115878/11A RU2532448C1 (en) | 2013-04-10 | 2013-04-10 | Method of control, stabilisation and development of extra lift of airship |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2532448C1 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2639377C2 (en) * | 2016-01-29 | 2017-12-21 | Акционерное общество "Долгопрудненское конструкторское бюро автоматики" | Helistat device with autogyro screw |
| RU2659716C1 (en) * | 2017-03-01 | 2018-07-03 | Владимир Александрович Ворогушин | Ultralight foldable gyroplane design |
| DK3659912T3 (en) * | 2018-11-30 | 2022-04-25 | Umiles Urban Air Mobility S L | Aircraft with decoupled degrees of freedom |
| CN112046724A (en) * | 2020-09-09 | 2020-12-08 | 重庆交通大学 | A self-rotating airship |
| WO2025170486A1 (en) * | 2024-02-07 | 2025-08-14 | Федеральное государственное бюджетное учреждение науки Институт теплофизики им. С.С. Кутателадзе Сибирского отделения Российской академии наук | Method of aerodynamically stabilizing an airship in an air flow |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4591112A (en) * | 1975-09-09 | 1986-05-27 | Piasecki Aircraft Corporation | Vectored thrust airship |
| US4269375A (en) * | 1979-10-31 | 1981-05-26 | Hickey John J | Hybrid annular airship |
| RU63770U1 (en) * | 2007-01-09 | 2007-06-10 | Федеральное государственное унитарное предприятие "Государственный ракетный центр "КБ им. академика В.П. Макеева" | VERTOSTAT |
-
2013
- 2013-04-10 RU RU2013115878/11A patent/RU2532448C1/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2532448C1 (en) | 2014-11-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP4306427A3 (en) | Vertical takeoff and landing aircraft | |
| WO2016028358A3 (en) | High Performance VTOL Aircraft | |
| EP4324740A3 (en) | Erodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowable rotor blades | |
| EA201491528A1 (en) | AERIAL VERTICAL TAKE-OFF AIRCRAFT AND LANDING WITH TWO WING DESIGNS | |
| WO2017131834A3 (en) | Pivoting wing system for vtol aircraft | |
| CA2947974A1 (en) | Vtol aircraft | |
| EA201800376A1 (en) | AIRCRAFT WITH VERTICAL TAKEOUT AND LANDING AND METHOD OF CONTROL OF THIS EQUIPMENT | |
| NZ706696A (en) | Vertical take-off and landing aircraft | |
| WO2014120331A3 (en) | Vertical takeoff and landing aircraft | |
| IL241201B (en) | Foldable wings for an unmanned air vehicle | |
| Wang et al. | Modeling and control of an agile tail-sitter aircraft | |
| WO2016109003A3 (en) | Delta fuselage for vertical take-off and landing (vtol) aircraft | |
| EA201300348A1 (en) | TRANSFORMABLE AIRCRAFT VERTICAL TAKEOFF AND LANDING WITH A TURNING WING | |
| WO2016060827A3 (en) | Translation thrust system engagement and disengagment for rotary wing aircraft | |
| ATE552171T1 (en) | FLYING WING PLANE | |
| EP4417510A3 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| RU2013141179A (en) | AIRCRAFT | |
| BR112013018863A2 (en) | aircraft | |
| WO2015133932A3 (en) | Rotary-wing aircraft with vertical take-off | |
| WO2015143098A3 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| WO2014058351A3 (en) | Aircraft | |
| RU2013115878A (en) | METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER | |
| NZ712963A (en) | Vertical take-off and landing aircraft | |
| WO2015094020A3 (en) | Convertiplane with reactive rotor drive, which is controlled by rotors by means of swash plates, via control levers, and which does not require additional control means | |
| RU2016110050A (en) | VERTICAL TAKEOFF AND LANDING FLIGHT AND ITS FLIGHT CONTROL METHOD |