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
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- RU
- Russia
- Prior art keywords
- airship
- hull
- stabilizing
- autogyro
- traction
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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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 (4)
| 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 | Self-rotating rotor type airship |
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 |
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2013
- 2013-04-10 RU RU2013115878/11A patent/RU2532448C1/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2532448C1 (en) | 2014-11-10 |
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