MD3510G2 - Aircraft-control gear - Google Patents
Aircraft-control gearInfo
- Publication number
- MD3510G2 MD3510G2 MDA20060036A MD20060036A MD3510G2 MD 3510 G2 MD3510 G2 MD 3510G2 MD A20060036 A MDA20060036 A MD A20060036A MD 20060036 A MD20060036 A MD 20060036A MD 3510 G2 MD3510 G2 MD 3510G2
- Authority
- MD
- Moldova
- Prior art keywords
- joined
- aircraft
- gear unit
- onto
- satellite gear
- Prior art date
Links
Landscapes
- Retarders (AREA)
- Non-Deflectable Wheels, Steering Of Trailers, Or Other Steering (AREA)
- Transmission Devices (AREA)
- Braking Arrangements (AREA)
Abstract
The invention relates to the aircraft designing and may be used in the aircraft control and braking systems.The aircraft-control gear includes two turntable sections (1) and (2), installed onto the backside of the wing. The turntable sections (1) and (2) are mounted onto a common axis (5), in the middle of which it is placed an electric motor (7) with two hollow output shafts (8) and (9), one of which (8) is rigidly joined with a hollow inclined shaft (10), onto which it is installed a toothed two-crown (12, 13) satellite gear unit (11), on one side of which there are placed two fixed gearwheels (14) and (15) with a different number of teeth, alternately joined with a lateral fixed cover (18) by means of two couplings (16) and (17). On the other side of the satellite gear unit (11) it is installed a movable gearwheel (20), joined by a hinge (3) with one of the turntable sections (1). The second hollow output shaft (9) is rigidly joined with the second hollow inclined shaft (21), onto which it is installed the second toothed two-crown (23, 24) satellite gear unit (22), on one side of which it is placed a fixed gearwheel (25), joined with the second lateral fixed cover (29) by means of another coupling (26). On the other side of the satellite gear unit (22) it is placed another movable gearwheel (31), joined by a hinge (4) with the second turntable section (2).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MDA20060036A MD3510G2 (en) | 2006-01-18 | 2006-01-18 | Aircraft-control gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MDA20060036A MD3510G2 (en) | 2006-01-18 | 2006-01-18 | Aircraft-control gear |
Publications (3)
Publication Number | Publication Date |
---|---|
MD20060036A MD20060036A (en) | 2007-08-31 |
MD3510F2 MD3510F2 (en) | 2008-02-29 |
MD3510G2 true MD3510G2 (en) | 2008-09-30 |
Family
ID=38477225
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MDA20060036A MD3510G2 (en) | 2006-01-18 | 2006-01-18 | Aircraft-control gear |
Country Status (1)
Country | Link |
---|---|
MD (1) | MD3510G2 (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2147544C1 (en) * | 1998-01-19 | 2000-04-20 | Нурмухаметов Искандер Рифович | Wing |
RU2184681C2 (en) * | 2000-08-04 | 2002-07-10 | Буданов Станислав Васильевич | Device for motion in air medium |
RU2186711C2 (en) * | 2000-05-11 | 2002-08-10 | Дудник Виталий Владимирович | Singler-rotor helicopter multi-functional tail unit |
RU2189334C2 (en) * | 2000-05-04 | 2002-09-20 | Буданов Станислав Васильевич | Vehicle for motion in air medium |
RU2002119450A (en) * | 2002-07-23 | 2004-04-27 | Закрытое акционерное общество "Отделение морских систем ОКБ им. П.О. Сухого" | AIR BRAKE |
SU1517264A1 (en) * | 1987-06-22 | 2005-04-10 | Н.С. Кирпичев | WHEEL DIRECTION OF THE AIRCRAFT AND THE METHOD OF ITS MANUFACTURE |
-
2006
- 2006-01-18 MD MDA20060036A patent/MD3510G2/en not_active IP Right Cessation
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU1517264A1 (en) * | 1987-06-22 | 2005-04-10 | Н.С. Кирпичев | WHEEL DIRECTION OF THE AIRCRAFT AND THE METHOD OF ITS MANUFACTURE |
RU2147544C1 (en) * | 1998-01-19 | 2000-04-20 | Нурмухаметов Искандер Рифович | Wing |
RU2189334C2 (en) * | 2000-05-04 | 2002-09-20 | Буданов Станислав Васильевич | Vehicle for motion in air medium |
RU2186711C2 (en) * | 2000-05-11 | 2002-08-10 | Дудник Виталий Владимирович | Singler-rotor helicopter multi-functional tail unit |
RU2184681C2 (en) * | 2000-08-04 | 2002-07-10 | Буданов Станислав Васильевич | Device for motion in air medium |
RU2002119450A (en) * | 2002-07-23 | 2004-04-27 | Закрытое акционерное общество "Отделение морских систем ОКБ им. П.О. Сухого" | AIR BRAKE |
Non-Patent Citations (1)
Title |
---|
Mecanism de dirijare a aparatului de zbor: www.buran.ru/htm/tail.htm [regăsită 2007.12.11] * |
Also Published As
Publication number | Publication date |
---|---|
MD20060036A (en) | 2007-08-31 |
MD3510F2 (en) | 2008-02-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
KA4A | Patent for invention lapsed due to non-payment of fees (with right of restoration) | ||
MM4A | Patent for invention definitely lapsed due to non-payment of fees |