RU2379215C2 - Aircraft - Google Patents
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- Publication number
- RU2379215C2 RU2379215C2 RU2008139991/11A RU2008139991A RU2379215C2 RU 2379215 C2 RU2379215 C2 RU 2379215C2 RU 2008139991/11 A RU2008139991/11 A RU 2008139991/11A RU 2008139991 A RU2008139991 A RU 2008139991A RU 2379215 C2 RU2379215 C2 RU 2379215C2
- Authority
- RU
- Russia
- Prior art keywords
- aircraft
- airframe
- cab
- horizontal plane
- cockpit
- Prior art date
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- Body Structure For Vehicles (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Изобретение относится к космонавтике и служит для планирования на других планетах.The invention relates to astronautics and is used for planning on other planets.
Известна конструкция летающего аппарата, состоящая из корпуса и кабины (см. журнал «Техника молодежи» №12. 2000, с.33).A known design of a flying apparatus, consisting of a hull and a cockpit (see the journal "Technique of Youth" No. 12, 2000, p. 33).
Данная конструкция не эффективна.This design is not effective.
Изобретение направлено на устранение указанного недостатка.The invention is aimed at eliminating this drawback.
Достигается это тем, что корпус и кабина симметричны и сдвигаются относительно горизонтальной плоскости.This is achieved by the fact that the body and the cabin are symmetrical and move relative to the horizontal plane.
На фиг.1 показан летающий аппарат; на фиг.2 - вид сверху; на фиг.3 - летающий аппарат при его раздвижении; на фиг.4 - вид сверху.Figure 1 shows a flying machine; figure 2 is a top view; figure 3 - flying apparatus when it is extended; figure 4 is a top view.
Конструкция включает корпуса 1 и 2, к которым крепятся кабины 3 и 4.The design includes buildings 1 and 2, to which cabs 3 and 4 are attached.
Устройство работает следующим образом:The device operates as follows:
При приземлении корпус 2 и кабина 4 смещаются относительно горизонтальной плоскости, тем самым увеличивая планерность конструкции.When landing, the housing 2 and the cabin 4 are displaced relative to the horizontal plane, thereby increasing the glider structure.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008139991/11A RU2379215C2 (en) | 2008-10-08 | 2008-10-08 | Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008139991/11A RU2379215C2 (en) | 2008-10-08 | 2008-10-08 | Aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2008139991A RU2008139991A (en) | 2009-01-27 |
RU2379215C2 true RU2379215C2 (en) | 2010-01-20 |
Family
ID=41647079
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008139991/11A RU2379215C2 (en) | 2008-10-08 | 2008-10-08 | Aircraft |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2379215C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2451624C1 (en) * | 2011-02-25 | 2012-05-27 | Сергей Владимирович Михайлов | Disc-like aircraft |
-
2008
- 2008-10-08 RU RU2008139991/11A patent/RU2379215C2/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2451624C1 (en) * | 2011-02-25 | 2012-05-27 | Сергей Владимирович Михайлов | Disc-like aircraft |
Also Published As
Publication number | Publication date |
---|---|
RU2008139991A (en) | 2009-01-27 |
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